US20140157939A1 - Release mechanism - Google Patents
Release mechanism Download PDFInfo
- Publication number
- US20140157939A1 US20140157939A1 US14/183,038 US201414183038A US2014157939A1 US 20140157939 A1 US20140157939 A1 US 20140157939A1 US 201414183038 A US201414183038 A US 201414183038A US 2014157939 A1 US2014157939 A1 US 2014157939A1
- Authority
- US
- United States
- Prior art keywords
- rotor
- housing
- release mechanism
- spring
- coil spring
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
- B60N2/22—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable
- B60N2/235—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable by gear-pawl type mechanisms
- B60N2/2356—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable the back-rest being adjustable by gear-pawl type mechanisms with internal pawls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/02—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles the seat or part thereof being movable, e.g. adjustable
- B60N2/0296—Central command actuator to selectively switch on or engage one of several special purpose circuits or mechanisms
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/90—Details or parts not otherwise provided for
- B60N2/919—Positioning and locking mechanisms
- B60N2/933—Positioning and locking mechanisms rotatable
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C1/00—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
- F16C1/10—Means for transmitting linear movement in a flexible sheathing, e.g. "Bowden-mechanisms"
- F16C1/12—Arrangements for transmitting movement to or from the flexible member
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/20—Control lever and linkage systems
- Y10T74/20396—Hand operated
- Y10T74/20402—Flexible transmitter [e.g., Bowden cable]
- Y10T74/2042—Flexible transmitter [e.g., Bowden cable] and hand operator
- Y10T74/20438—Single rotatable lever [e.g., for bicycle brake or derailleur]
Definitions
- Seats for motor vehicles and the like may include one or more adjustment features such as a seat back tilt mechanism that selectively retains the seat back in a position selected by a user.
- the seat may include additional adjustment features such as fore-aft sliding of the seat relative to the vehicle floor, and other such adjustment features.
- Various types of mechanisms have been developed to retain the seat components in a desired position. Such mechanisms may be actuated by a cable that is connected to a manually-operated release mechanism by an elongated cable. Also, elongated cables may be utilized to operably interconnect a lever or other release member located inside a vehicle to a component such as a hood release latch.
- Various mechanisms for manual user input have been developed. However, known mechanisms may suffer from various drawbacks.
- the release mechanism includes a housing defining a pivot element, and a rotor disposed within the housing and pivotably engaging the pivot element for rotation about an axis.
- the rotor is adapted to be manually rotated by a user, and the rotor includes a connecting feature that provides for connecting an end of an elongated flexible cable to the rotor, such that rotation of the rotor shifts the elongated flexible cable.
- the release mechanism also includes a helical coil spring having a first end connected to the housing, and a second end connected to the rotor. The coil spring is rotationally deformed to rotationally bias the rotor for rotation in a first direction about the axis, and the coil spring is also compressed, and biases the rotor axially away from the housing along the axis.
- the housing may include a separate cover that snaps onto a main portion of the housing during assembly.
- the housing and rotor can be utilized in either a “left hand” or “right hand” orientation.
- the housing and rotor may be symmetrical about a center plane, and the direction of the rotational bias of the rotor can be changed by selecting a helical coil that generates either a clockwise or counter clockwise torque on the rotor.
- the housing may include connecting features whereby a cable can be interconnected to the housing of the release mechanism at either of two opposite side faces of the housing.
- the release mechanism may include a rotation-limiting feature such as a boss on the rotor and corresponding arcuate slot on the housing to limit rotation of the rotor relative to the housing.
- a rotation-limiting feature such as a boss on the rotor and corresponding arcuate slot on the housing to limit rotation of the rotor relative to the housing.
- FIG. 1 is a partially fragmentary side elevational view of a motor vehicle seat or the like including an adjustment mechanism and a release mechanism that is interconnected to the adjustment mechanism by an elongated cable;
- FIG. 2 is a top plan view of a release mechanism according to one aspect of the present invention.
- FIG. 3 is a front elevational view of the release mechanism of FIG. 2 ;
- FIG. 4 is an exploded isometric view of the release mechanism of FIG. 2 ;
- FIG. 4A is an exploded isometric view of the release mechanism of FIG. 2 showing the spring in an uncompressed state
- FIG. 5 is a partially exploded isometric view of the release mechanism of FIG. 2 ;
- FIG. 6 is a partially fragmentary enlarged, isometric view of a portion of a release mechanism according to one aspect of the present invention.
- FIG. 7 is a partially fragmentary, enlarged isometric view of a portion of a rotor of a release mechanism according to one aspect of the present invention.
- FIG. 8 shows a coil spring according to one aspect of the present invention in an uncompressed state
- FIG. 9 shows the spring of FIG. 8 ;
- FIG. 10 is an end view of the spring of FIG. 8 ;
- FIG. 11 is an enlarged, fragmentary view of a portion of the spring of FIG. 10 .
- the terms “upper,” “lower,” “right,” “left,” “rear,” “front,” “vertical,” “horizontal,” and derivatives thereof shall relate to the invention as oriented in FIG. 1 .
- the invention may assume various alternative orientations, except where expressly specified to the contrary.
- the specific devices and processes illustrated in the attached drawings, and described in the following specification are simply exemplary embodiments of the inventive concepts defined in the appended claims. Hence, specific dimensions and other physical characteristics relating to the embodiments disclosed herein are not to be considered as limiting, unless the claims expressly state otherwise.
- a seat assembly 1 includes a seat portion 2 and a back portion 3 that is pivotally interconnected to the seat portion for fore-aft tilting movement as indicated by the arrow “A.”
- a releasable adjustment mechanism 4 selectively retains the back portion 3 at various positions B, B 1 , B 2 etc.
- An adjustment mechanism 4 may be positioned on both the left and right sides of the seat 1 .
- a support structure 5 interconnects the seat assembly 1 with a vehicle floor 6 .
- the support structure 5 may include slides or the like (not shown) that permit movement of the seat assembly 1 in a fore-aft direction relative to the floor 6 of a vehicle as indicated by the arrow “C.”
- the seat portion 2 , back portion 3 , adjustment mechanism 4 , and support structure 5 may comprise conventional, known components such that these parts will not be described in detail herein
- a release mechanism 10 is operably interconnected to the adjustment mechanism 4 by an elongated cable 11 .
- the release mechanism 10 includes a movable input member such as a handle 12 that is movable as indicated by the arrow “R” by a user to selectively release adjustment mechanism 4 to permit tilting of the seat back 3 .
- mechanism 10 includes a housing having a first portion 14 and a second portion or cover 16 that together form an interior space 18 .
- a rotor 20 When assembled, a rotor 20 is rotatably interconnected with a boss or protrusion 22 of housing 14 for rotation about an axis “A 1 ” ( FIG. 4 ).
- a spring 25 includes a first end 26 that is interconnected to housing 14 , and a second end 28 that is interconnected with rotor 20 to rotationally bias the rotor 20 relative to housing 14 for rotation about an axis “A 1 .”
- Rotor 20 includes an arm 34 having an end portion 36 that includes first and second connecting features 30 A and 30 B (cavities) that interconnect with a fitting 32 of cable 11 whereby rotation of rotor 20 longitudinally shifts the cable 11 and releases adjustment mechanism 4 .
- the arm 34 is substantially symmetrical such that either connecting feature 30 A or connecting feature 30 B can be utilized to connect with a cable end fitting 32 .
- the end fitting 32 is received in connector 30 A to thereby pull on cable 11 upon rotation of rotor 20 in the direction of the arrow “R 1 .”
- An end portion 11 A of cable 11 wraps around curved end surface 37 of arm 34 .
- End surface 37 may include a relatively flat central portion 37 A having a reduced radius about axis Al to provide increased force on cable 11 as it wraps around central portion 37 A.
- Cable end fitting 32 may be received in connecting feature 30 B such that rotation of rotor 20 in a direction opposite the arrow “R 1 ” pulls on cable 11 to actuate adjustment mechanism 4 .
- the direction of rotational bias provided by spring 25 may be reversed if connecting feature 30 B is utilized to thereby provide the proper rotational bias for a particular application.
- a bushing or fitting 38 includes an annular groove 39 that engages a selected one of the openings 40 A- 40 D of sidewall 41 A or 41 B of housing 14 to slidably support cable 11 where it enters housing 14 .
- Rotor 20 includes a generally cylindrical extension 42 having a plurality of teeth or splines 44 that engage corresponding teeth or splines 46 on an interior portion of extension 47 of handle 12 in a known manner to interconnect rotor 20 and handle 12 .
- a pair of transverse slots 48 receive a clip or other retainer (not shown) to retain handle 12 to rotor 20 in a conventional manner.
- Housing 14 includes a plurality of wedges 52 that protrude from sidewalls 41 C, 41 D, and 41 E. Wedges 52 are received in openings 53 formed in transverse flaps or extensions 54 (see also FIGS. 2 and 3 ). The wedges 52 and corresponding connectors 53 - 54 retain cover 16 on housing 14 prior to installation of the release mechanism 10 on a seat assembly 1 . Threaded fasteners 56 ( FIG. 3 ) are received in openings 57 in housing 14 and cover 16 ( FIGS. 2 and 3 ) and engage threaded openings in the seat structure to secure the release mechanism 10 to the seat assembly 1 . Fasteners 56 also ensure that housing 14 and cover 16 remain assembled together when mechanism 10 is attached to the seat assembly 1 .
- arm 34 of rotor 20 includes cylindrical extension 64 .
- Housing 14 includes a ridge or sidewall 60 that protrudes from inner surface 58 of sidewall 59 of housing 14 .
- extension 64 When assembled, extension 64 is received in arcuate slot 62 , and spring 25 rotatably biases extension 64 towards end surface 66 or end surface 68 of arcuate slot 62 .
- Spring 25 may be configured to rotatably bias rotor 20 in a first direction R 1 , or a second direction that is opposite R 1 , depending upon which direction handle 12 is required to rotate when release mechanism 10 is installed on a seat or other structure. For example, in FIG.
- mechanism 10 is mounted on a left side of a seat 2 , and handle 12 rotates upwardly when the handle 12 is pulled by a user.
- mechanism 10 may also be installed on a seat at a lower right side edge whereby the mechanism 10 is rotated 180 degrees about a horizontal axis relative to the orientation shown in FIG. 1 .
- the spring 25 is configured to provide a bias in the opposite rotational direction, and cable 11 will be configured to extend out of an opposite sidewall of housing 14 .
- the mechanism 10 is substantially symmetrical (other than spring 25 ) about a center plane “P” ( FIG. 2 ) Cable 11 is oriented in either the configuration shown in FIG. 2 in solid lines, or in the configuration shown in dashed lines 11 A as also shown in FIG. 2 .
- housing 14 includes an annular wall 70 protruding from inner side surface 58 of sidewall 59 of housing 14 .
- An inner side of sidewall 70 includes a plurality of raised portions or pads 72 having cylindrical end surface portions 73 .
- a ring-like annular space 76 is formed between boss 22 and cylindrical sidewall 70 .
- a plurality of protrusions 74 project into annular space 76 from sidewall 59 .
- a plurality of grooves 77 are formed between protrusions 74 . Grooves 77 extend radially away from boss 22 .
- the protrusions 74 also define convex cylindrical outer surfaces 78 that face the concave cylindrical surfaces 73 of pads 72 of cylindrical sidewall 70 .
- End portion 80 of rotor 20 includes a cylindrical inner side surface 81 that defines a cylindrical cavity or space 83 .
- End portion 20 also includes a cylindrical outer surface 82 .
- end 28 (see also FIG. 4 ) of spring 25 is received in a selected one of a plurality of openings 85 in inner base surface 84 of cavity 83 .
- An opening 86 in rotor 20 has a hexagonal shape to receive a hexagonal tool (not shown) during assembly of rotor 20 and housing 14 to control the rotational position of rotor 20 relative to housing 14 .
- end 26 of spring 25 ( FIGS. 4 and 4A ) is positioned in a selected slot 77 ( FIG. 6 ) of housing 14 , with a portion of spring 25 being disposed between cylindrical sidewall 70 and boss 22 of housing 14 .
- Spring 25 is initially in an uncompressed or “free” state wherein the individual coils of spring 25 are spaced apart as shown in FIGS. 4A , 8 and 9 .
- Rotor 20 is then moved to a position adjacent housing 14 , such that end 28 of spring 25 is received in a selected one of the openings 85 of rotor 20 .
- Rotor 20 is then rotated relative to housing 14 using a hexagonal tool (not shown), such that spring 25 generates a torsional bias or force between housing 14 and rotor 20 .
- Rotor 20 is then shifted axially along axis Al ( FIG. 4 ) to position end portion 80 of rotor 20 on the boss 22 of housing 14 .
- End portion 80 of rotor 20 is received in the space 76 ( FIG. 6 ) between surfaces 73 of pads 72 and the end surfaces 78 of protrusions 74 .
- protrusion 64 ( FIG. 5 ) of rotor 20 is positioned in arcuate slot 62 of housing 14 .
- extension 64 After the extension 64 is positioned in arcuate slot 62 , the torsional force acting on rotor 20 by the hexagonal tool is removed, and the torsional force caused by spring 25 causes extension 64 on arm 34 of rotor 20 to move into engagement with end 66 (or end 68 ) of arcuate slot 62 .
- spring 25 As rotor 20 is moved into position relative to housing 14 , spring 25 is compressed in addition to being rotationally deformed. This causes spring 25 to generate an axial force tending to push rotor 20 away from housing 14 .
- friction between extension 64 and end 66 (or 68 ) of arcuate slot 62 is sufficient to prevent the axial bias from shifting rotor 20 relative to housing 14 .
- the coils of spring 25 When compressed, the coils of spring 25 are in contact with one another or directly adjacent one another as shown in FIG. 4 .
- spring 25 shifts rotor 20 towards cover 16 slightly, such that annular bearing surface 90 of extension 42 of rotor 20 slidably engages an annular bearing surface 88 formed around opening 89 of cover 16 .
- the engagement of bearing surfaces 88 and 90 prevents rattling of rotor 20 when installed to a seat, yet permits some variation in the sizing of the components.
- outer surface 82 ( FIG. 4 ) of end 80 of rotor 20 slidably engages surface 73 ( FIG. 6 ) of housing 14
- outer surface 92 of extension 42 of rotor 20 slidably engages surfaces or pads 94 ( FIG. 4 ) of opening 90 in cover 16 .
- handle 12 is positioned on extension 42 of rotor 20 , and a clip or other retainer (not shown) is positioned in engagement with transverse slots 48 of extension 42 to thereby retain the handle 12 .
- rotor 20 can be temporarily assembled with housing 14 , rotor 20 does not need to be retained in position relative to housing 14 by a fixture or the like while cover 16 is installed. Thus, assembly of release mechanism 10 is simplified. Also, as discussed above, the axial bias of spring 25 ensures that the bearing surface 90 of rotor 20 remains in sliding engagement with the corresponding bearing surface 88 of cover 16 .
- the bearing surfaces 88 and 90 may comprise low friction materials, such that very little frictional resistance is generated. This permits spring 25 to have a relatively low torsional stiffness to return handle 12 to the rest position.
- spring 25 may comprise a helical coil spring having a wire diameter of 1.14 mm with 10 coils.
- the coils may have a right hand or left hand wind direction as required to provide a right or left hand version of mechanism 10 .
- the spring 25 has a free or unstressed length “L 1 ” of 28.5 mm.
- the length L 1 may be about 23.0 mm to about 33.0 mm.
- lengths L 1 outside this range may also be utilized if required for a particular application.
- an axial force “F” is applied to the spring 25 as described in more detail above. This results in a compression of spring 25 to an installed length “L 2 ” of 14.65 mm.
- the deflection of spring 25 when installed is about 13.85 mm.
- the overall length “L 3 ” of spring 25 in an unstressed or free state is 34.34 mm as shown in FIG. 8 .
- the inner radius “R” is 1.40 mm
- the outer diameter “D 2 ” ( FIG. 10 ) is 11.15 mm.
- the spring 25 may include straight portions 26 A and 28 A directly adjacent the ends 26 and 28 , respectively.
- the inner dimension “D 1 ” ( FIG. 10 ) is 8.72 mm, and the outside diameter “D 2 ” is 11.15 mm.
- the angle “ ⁇ 2 ” is 142.4°. Ends 26 and 28 extend at an angle “ ⁇ 1 ” of 90°.
- Spring 25 is preferably made of spring steel or other suitable material such as music wire (ASTM A228), and the spring 25 has a maximum solid height of 12.65 mm.
- the specific dimensions given above are an example of one possible configuration for spring 25 .
- the specific dimensions, shapes, materials, and other characteristics of spring 25 may vary as required for a particular application.
- mechanism 10 may be utilized in connection with different types of seats requiring different force characteristics to release adjustment mechanism 4 ( FIG. 1 ) or other such mechanism. It will be understood that the specific dimensions of the mechanism and spring 25 may vary as required, and the release mechanism 10 of the present application is not limited to any specific application.
- the installed length L 2 of spring 25 is greater than the solid height or length of spring 25 . Accordingly, when spring 25 is installed in mechanism 10 spring 25 is in a compressed state. When spring 25 is in the compressed (installed) state, the spacing between the individual coils of spring 25 is reduced, and spring 25 generates a biasing force tending to expand the length of spring 25 . As discussed above, this biasing force insures that bearing surface 90 of rotor 20 remains in sliding engagement with corresponding bearing surface 88 of cover 16 .
- mechanism 10 may be assembled by temporarily assembling rotor 20 with housing 14 , with friction between extensions 64 and end 66 (or end 68 ) of arcuate slot 62 to generate friction sufficient to prevent axial bias of spring 25 from shifting rotor 20 relative to housing 14 .
- mechanism 10 may also be assembled as follows. First, housing 14 may be positioned in a fixture (not shown) or otherwise retained in a generally horizontal orientation with interior space 18 ( FIG. 4 ) facing upwardly. Spring 25 is then positioned over boss 22 , and shifted (if required) to cause end 26 of spring 25 to engage one of the grooves 77 ( FIG. 6 ) of housing 14 .
- the rotor 20 is then positioned on spring 25 such that spring 25 is received within cylindrical cavity or space 83 of rotor 20 ( FIGS. 5 and 7 ), and end 28 of spring 25 is engaged with one of the openings 85 ( FIG. 7 ) of rotor 20 .
- the arm 34 of rotor 20 is initially oriented as shown in solid lines in FIG. 4A . This initial position is rotated 180° relative to the assembled orientation of arm 34 shown in dashed lines in FIG. 4A . The assembled orientation of arm 34 is also shown in solid lines in FIG. 4 .
- cover 16 is positioned on rotor 20 with extension 42 of rotor 20 extending through opening 89 of cover 16 .
- a hex tool (not shown) is positioned in hex opening 86 ( FIG. 7 ) of rotor 20 , and the rotor 20 is then rotated 180° until it is in the assembled rotational orientation ( FIG. 4 ).
- Rotor 20 may be rotationally constrained due to engagement of extension 64 on arm 34 of rotor with end 66 or 68 of arcuate slot 62 .
- rotor 20 may be configured to temporarily engage cover 16 to prevent rotation of rotor 20 during the assembly process. After the cover 16 is positioned over rotor 20 and rotor 20 is rotated to its assembled angular orientation, the housing 14 and cover 16 are pushed together and interconnected utilizing wedges 52 and openings 53 as described in more detail above.
- spring 25 Due to the axial compression (deflection), spring 25 generates about 24 N of axial force when assembled. This axial force biases rotor 20 away from housing 14 , and into engagement with cover 16 . Also, when assembled the rotational deflection or deformation of spring 25 causes the spring 25 to be preloaded such that it generates a torsional force of about 250 N-mm. Thus, when assembled spring 25 simultaneously generates a substantial axial biasing force and a substantial torsional biasing force.
- spring 25 has a longer length than conventional torsion springs utilized in prior mechanisms. The longer length allows spring 25 to have a lower torsional spring constant, thereby reducing the spring biasing force acting on the handle 12 ( FIG. 1 ) for a given spring displacement.
- the total force required by a user in moving (rotating) handle 12 includes force required to overcome the torsion of spring 25 and the force required to actuate adjustment mechanism 4 .
- reducing the torsional force generated by spring 25 reduces the total force a user must apply to handle 12 to actuate adjustment mechanism 4 .
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Seats For Vehicles (AREA)
Abstract
A release mechanism generates a force on a cable to operate an adjustment mechanism or the like in a seat or other device. The release mechanism includes a rotor, a housing, a spring, and a cover that attaches to the housing. The spring generates a torque, and the spring also axially biases the rotor into engagement with the cover to prevent rattling.
Description
- This application is a Continuation-In-Part of U.S. patent application Ser. No. 13/315,797, filed Dec. 9, 2011, and entitled “RELEASE MECHANISM,” the entire disclosure of which is incorporated herein by reference.
- Seats for motor vehicles and the like may include one or more adjustment features such as a seat back tilt mechanism that selectively retains the seat back in a position selected by a user. The seat may include additional adjustment features such as fore-aft sliding of the seat relative to the vehicle floor, and other such adjustment features. Various types of mechanisms have been developed to retain the seat components in a desired position. Such mechanisms may be actuated by a cable that is connected to a manually-operated release mechanism by an elongated cable. Also, elongated cables may be utilized to operably interconnect a lever or other release member located inside a vehicle to a component such as a hood release latch. Various mechanisms for manual user input have been developed. However, known mechanisms may suffer from various drawbacks.
- One aspect of the present invention is a release mechanism of the type utilized to shift an elongated connector to selectively release an adjustment mechanism. The release mechanism includes a housing defining a pivot element, and a rotor disposed within the housing and pivotably engaging the pivot element for rotation about an axis. The rotor is adapted to be manually rotated by a user, and the rotor includes a connecting feature that provides for connecting an end of an elongated flexible cable to the rotor, such that rotation of the rotor shifts the elongated flexible cable. The release mechanism also includes a helical coil spring having a first end connected to the housing, and a second end connected to the rotor. The coil spring is rotationally deformed to rotationally bias the rotor for rotation in a first direction about the axis, and the coil spring is also compressed, and biases the rotor axially away from the housing along the axis.
- The housing may include a separate cover that snaps onto a main portion of the housing during assembly. The housing and rotor can be utilized in either a “left hand” or “right hand” orientation. The housing and rotor may be symmetrical about a center plane, and the direction of the rotational bias of the rotor can be changed by selecting a helical coil that generates either a clockwise or counter clockwise torque on the rotor. Also, the housing may include connecting features whereby a cable can be interconnected to the housing of the release mechanism at either of two opposite side faces of the housing.
- The release mechanism may include a rotation-limiting feature such as a boss on the rotor and corresponding arcuate slot on the housing to limit rotation of the rotor relative to the housing. During assembly, the rotor is rotated against the spring bias relative to the main portion of the housing, and the rotor is shifted axially to move the boss into the arcuate slot. Friction between the boss and a side surface of the arcuate slot prevents shifting of the rotor that could otherwise occur due to the axial bias of the helical coil spring.
- These and other features, advantages, and objects of the present invention will be further understood and appreciated by those skilled in the art by reference to the following specification, claims, and appended drawings.
-
FIG. 1 is a partially fragmentary side elevational view of a motor vehicle seat or the like including an adjustment mechanism and a release mechanism that is interconnected to the adjustment mechanism by an elongated cable; -
FIG. 2 is a top plan view of a release mechanism according to one aspect of the present invention; -
FIG. 3 is a front elevational view of the release mechanism ofFIG. 2 ; -
FIG. 4 is an exploded isometric view of the release mechanism ofFIG. 2 ; -
FIG. 4A is an exploded isometric view of the release mechanism ofFIG. 2 showing the spring in an uncompressed state; -
FIG. 5 is a partially exploded isometric view of the release mechanism ofFIG. 2 ; -
FIG. 6 is a partially fragmentary enlarged, isometric view of a portion of a release mechanism according to one aspect of the present invention; -
FIG. 7 is a partially fragmentary, enlarged isometric view of a portion of a rotor of a release mechanism according to one aspect of the present invention; -
FIG. 8 shows a coil spring according to one aspect of the present invention in an uncompressed state; -
FIG. 9 shows the spring ofFIG. 8 ; -
FIG. 10 is an end view of the spring ofFIG. 8 ; and -
FIG. 11 is an enlarged, fragmentary view of a portion of the spring ofFIG. 10 . - For purposes of description herein, the terms “upper,” “lower,” “right,” “left,” “rear,” “front,” “vertical,” “horizontal,” and derivatives thereof shall relate to the invention as oriented in
FIG. 1 . However, it is to be understood that the invention may assume various alternative orientations, except where expressly specified to the contrary. It is also to be understood that the specific devices and processes illustrated in the attached drawings, and described in the following specification are simply exemplary embodiments of the inventive concepts defined in the appended claims. Hence, specific dimensions and other physical characteristics relating to the embodiments disclosed herein are not to be considered as limiting, unless the claims expressly state otherwise. - With reference to
FIG. 1 , a seat assembly 1 includes aseat portion 2 and aback portion 3 that is pivotally interconnected to the seat portion for fore-aft tilting movement as indicated by the arrow “A.” Areleasable adjustment mechanism 4 selectively retains theback portion 3 at various positions B, B1, B2 etc. Anadjustment mechanism 4 may be positioned on both the left and right sides of the seat 1. Asupport structure 5 interconnects the seat assembly 1 with avehicle floor 6. Thesupport structure 5 may include slides or the like (not shown) that permit movement of the seat assembly 1 in a fore-aft direction relative to thefloor 6 of a vehicle as indicated by the arrow “C.” Theseat portion 2,back portion 3,adjustment mechanism 4, andsupport structure 5 may comprise conventional, known components such that these parts will not be described in detail herein - A
release mechanism 10 is operably interconnected to theadjustment mechanism 4 by anelongated cable 11. Therelease mechanism 10 includes a movable input member such as ahandle 12 that is movable as indicated by the arrow “R” by a user to selectively releaseadjustment mechanism 4 to permit tilting of theseat back 3. - With further reference to
FIGS. 2-4 and 4A,mechanism 10 includes a housing having afirst portion 14 and a second portion orcover 16 that together form aninterior space 18. When assembled, arotor 20 is rotatably interconnected with a boss orprotrusion 22 ofhousing 14 for rotation about an axis “A1” (FIG. 4 ). As discussed in more detail below, aspring 25 includes afirst end 26 that is interconnected tohousing 14, and asecond end 28 that is interconnected withrotor 20 to rotationally bias therotor 20 relative tohousing 14 for rotation about an axis “A1.”Rotor 20 includes anarm 34 having anend portion 36 that includes first and second connectingfeatures fitting 32 ofcable 11 whereby rotation ofrotor 20 longitudinally shifts thecable 11 and releasesadjustment mechanism 4. Thearm 34 is substantially symmetrical such that either connectingfeature 30A or connectingfeature 30B can be utilized to connect with a cable end fitting 32. In the illustrated example, theend fitting 32 is received inconnector 30A to thereby pull oncable 11 upon rotation ofrotor 20 in the direction of the arrow “R1.” Anend portion 11A ofcable 11 wraps aroundcurved end surface 37 ofarm 34.End surface 37 may include a relatively flatcentral portion 37A having a reduced radius about axis Al to provide increased force oncable 11 as it wraps aroundcentral portion 37A.Cable end fitting 32 may be received in connectingfeature 30B such that rotation ofrotor 20 in a direction opposite the arrow “R1” pulls oncable 11 to actuateadjustment mechanism 4. The direction of rotational bias provided byspring 25 may be reversed if connectingfeature 30B is utilized to thereby provide the proper rotational bias for a particular application. A bushing orfitting 38 includes anannular groove 39 that engages a selected one of theopenings 40A-40D ofsidewall housing 14 to slidably supportcable 11 where it entershousing 14. -
Rotor 20 includes a generallycylindrical extension 42 having a plurality of teeth orsplines 44 that engage corresponding teeth orsplines 46 on an interior portion ofextension 47 ofhandle 12 in a known manner to interconnectrotor 20 and handle 12. A pair oftransverse slots 48 receive a clip or other retainer (not shown) to retainhandle 12 torotor 20 in a conventional manner. -
Housing 14 includes a plurality ofwedges 52 that protrude fromsidewalls Wedges 52 are received inopenings 53 formed in transverse flaps or extensions 54 (see alsoFIGS. 2 and 3 ). Thewedges 52 and corresponding connectors 53-54retain cover 16 onhousing 14 prior to installation of therelease mechanism 10 on a seat assembly 1. Threaded fasteners 56 (FIG. 3 ) are received inopenings 57 inhousing 14 and cover 16 (FIGS. 2 and 3 ) and engage threaded openings in the seat structure to secure therelease mechanism 10 to the seat assembly 1.Fasteners 56 also ensure thathousing 14 and cover 16 remain assembled together whenmechanism 10 is attached to the seat assembly 1. - With further reference to
FIG. 5 ,arm 34 ofrotor 20 includescylindrical extension 64.Housing 14 includes a ridge orsidewall 60 that protrudes frominner surface 58 ofsidewall 59 ofhousing 14. When assembled,extension 64 is received inarcuate slot 62, andspring 25rotatably biases extension 64 towardsend surface 66 orend surface 68 ofarcuate slot 62.Spring 25 may be configured to rotatablybias rotor 20 in a first direction R1, or a second direction that is opposite R1, depending upon which direction handle 12 is required to rotate whenrelease mechanism 10 is installed on a seat or other structure. For example, inFIG. 1 mechanism 10 is mounted on a left side of aseat 2, and handle 12 rotates upwardly when thehandle 12 is pulled by a user. However,mechanism 10 may also be installed on a seat at a lower right side edge whereby themechanism 10 is rotated 180 degrees about a horizontal axis relative to the orientation shown inFIG. 1 . Ifmechanism 10 is configured for use on a right side edge of a seat, thespring 25 is configured to provide a bias in the opposite rotational direction, andcable 11 will be configured to extend out of an opposite sidewall ofhousing 14. Because themechanism 10 is substantially symmetrical (other than spring 25) about a center plane “P” (FIG. 2 )Cable 11 is oriented in either the configuration shown inFIG. 2 in solid lines, or in the configuration shown in dashedlines 11A as also shown inFIG. 2 . - With further reference to
FIG. 6 ,housing 14 includes anannular wall 70 protruding frominner side surface 58 ofsidewall 59 ofhousing 14. An inner side ofsidewall 70 includes a plurality of raised portions orpads 72 having cylindricalend surface portions 73. A ring-likeannular space 76 is formed betweenboss 22 andcylindrical sidewall 70. A plurality ofprotrusions 74 project intoannular space 76 fromsidewall 59. A plurality ofgrooves 77 are formed betweenprotrusions 74.Grooves 77 extend radially away fromboss 22. When assembled, end 26 (see alsoFIG. 5 ) ofspring 25 is received in a selected one of thegrooves 77 to thereby rotationally retain thespring 25 relative tohousing 14. - The
protrusions 74 also define convex cylindricalouter surfaces 78 that face the concavecylindrical surfaces 73 ofpads 72 ofcylindrical sidewall 70. When assembled, the space betweensurfaces FIG. 7 ) ofrotor 20.End portion 80 ofrotor 20 includes a cylindricalinner side surface 81 that defines a cylindrical cavity orspace 83.End portion 20 also includes a cylindricalouter surface 82. Whenmechanism 10 is assembled, end 28 (see alsoFIG. 4 ) ofspring 25 is received in a selected one of a plurality ofopenings 85 ininner base surface 84 ofcavity 83. Anopening 86 inrotor 20 has a hexagonal shape to receive a hexagonal tool (not shown) during assembly ofrotor 20 andhousing 14 to control the rotational position ofrotor 20 relative tohousing 14. - During assembly, end 26 of spring 25 (
FIGS. 4 and 4A ) is positioned in a selected slot 77 (FIG. 6 ) ofhousing 14, with a portion ofspring 25 being disposed betweencylindrical sidewall 70 andboss 22 ofhousing 14.Spring 25 is initially in an uncompressed or “free” state wherein the individual coils ofspring 25 are spaced apart as shown inFIGS. 4A , 8 and 9.Rotor 20 is then moved to a positionadjacent housing 14, such thatend 28 ofspring 25 is received in a selected one of theopenings 85 ofrotor 20.Rotor 20 is then rotated relative tohousing 14 using a hexagonal tool (not shown), such thatspring 25 generates a torsional bias or force betweenhousing 14 androtor 20.Rotor 20 is then shifted axially along axis Al (FIG. 4 ) to positionend portion 80 ofrotor 20 on theboss 22 ofhousing 14.End portion 80 ofrotor 20 is received in the space 76 (FIG. 6 ) betweensurfaces 73 ofpads 72 and the end surfaces 78 ofprotrusions 74. As therotor 20 is moved into position relative tohousing 14, protrusion 64 (FIG. 5 ) ofrotor 20 is positioned inarcuate slot 62 ofhousing 14. After theextension 64 is positioned inarcuate slot 62, the torsional force acting onrotor 20 by the hexagonal tool is removed, and the torsional force caused byspring 25causes extension 64 onarm 34 ofrotor 20 to move into engagement with end 66 (or end 68) ofarcuate slot 62. Asrotor 20 is moved into position relative tohousing 14,spring 25 is compressed in addition to being rotationally deformed. This causesspring 25 to generate an axial force tending to pushrotor 20 away fromhousing 14. However, friction betweenextension 64 and end 66 (or 68) ofarcuate slot 62 is sufficient to prevent the axial bias from shiftingrotor 20 relative tohousing 14. When compressed, the coils ofspring 25 are in contact with one another or directly adjacent one another as shown inFIG. 4 . - After the temporary subassembly of
housing 14 androtor 20 is formed.Bushings 38 are assembled withhousing 14, and end fitting 32 ofcable 11 is positioned inconnector 30A orconnector 30B ofarm 34 ofrotor 20. It will be understood that these operations may be performed either beforerotor 20 is installed inhousing 14, or afterrotor 20 is installed inhousing 14.Cover 16 is then snapped ontohousing 14 and retained thereon bywedges 52 andopenings 53. - Referring back to FIG. 4., After the
cover 16 andhousing 14 are assembled,spring 25shifts rotor 20 towardscover 16 slightly, such thatannular bearing surface 90 ofextension 42 ofrotor 20 slidably engages anannular bearing surface 88 formed around opening 89 ofcover 16. The engagement of bearingsurfaces rotor 20 when installed to a seat, yet permits some variation in the sizing of the components. - When assembled, outer surface 82 (
FIG. 4 ) ofend 80 ofrotor 20 slidably engages surface 73 (FIG. 6 ) ofhousing 14, andouter surface 92 ofextension 42 ofrotor 20 slidably engages surfaces or pads 94 (FIG. 4 ) of opening 90 incover 16. - During assembly, handle 12 is positioned on
extension 42 ofrotor 20, and a clip or other retainer (not shown) is positioned in engagement withtransverse slots 48 ofextension 42 to thereby retain thehandle 12. - Because the
rotor 20 can be temporarily assembled withhousing 14,rotor 20 does not need to be retained in position relative tohousing 14 by a fixture or the like whilecover 16 is installed. Thus, assembly ofrelease mechanism 10 is simplified. Also, as discussed above, the axial bias ofspring 25 ensures that the bearingsurface 90 ofrotor 20 remains in sliding engagement with the corresponding bearingsurface 88 ofcover 16. The bearing surfaces 88 and 90 may comprise low friction materials, such that very little frictional resistance is generated. This permitsspring 25 to have a relatively low torsional stiffness to returnhandle 12 to the rest position. - With further reference to
FIGS. 8-11 ,spring 25 may comprise a helical coil spring having a wire diameter of 1.14 mm with 10 coils. The coils may have a right hand or left hand wind direction as required to provide a right or left hand version ofmechanism 10. Thespring 25 has a free or unstressed length “L1” of 28.5 mm. In general, the length L1 may be about 23.0 mm to about 33.0 mm. However, lengths L1 outside this range may also be utilized if required for a particular application. During assembly, an axial force “F” is applied to thespring 25 as described in more detail above. This results in a compression ofspring 25 to an installed length “L2” of 14.65 mm. Thus, the deflection ofspring 25 when installed is about 13.85 mm. - The overall length “L3” of
spring 25 in an unstressed or free state is 34.34 mm as shown inFIG. 8 . The inner radius “R” is 1.40 mm, and the outer diameter “D2” (FIG. 10 ) is 11.15 mm. Thespring 25 may includestraight portions ends FIG. 10 ) is 8.72 mm, and the outside diameter “D2” is 11.15 mm. With reference toFIG. 11 , the angle “θ2” is 142.4°. Ends 26 and 28 extend at an angle “θ1” of 90°.Spring 25 is preferably made of spring steel or other suitable material such as music wire (ASTM A228), and thespring 25 has a maximum solid height of 12.65 mm. The specific dimensions given above are an example of one possible configuration forspring 25. However, the specific dimensions, shapes, materials, and other characteristics ofspring 25 may vary as required for a particular application. For example,mechanism 10 may be utilized in connection with different types of seats requiring different force characteristics to release adjustment mechanism 4 (FIG. 1 ) or other such mechanism. It will be understood that the specific dimensions of the mechanism andspring 25 may vary as required, and therelease mechanism 10 of the present application is not limited to any specific application. - As discussed above, the installed length L2 of
spring 25 is greater than the solid height or length ofspring 25. Accordingly, whenspring 25 is installed inmechanism 10spring 25 is in a compressed state. Whenspring 25 is in the compressed (installed) state, the spacing between the individual coils ofspring 25 is reduced, andspring 25 generates a biasing force tending to expand the length ofspring 25. As discussed above, this biasing force insures that bearingsurface 90 ofrotor 20 remains in sliding engagement with corresponding bearingsurface 88 ofcover 16. - As also discussed above,
mechanism 10 may be assembled by temporarily assemblingrotor 20 withhousing 14, with friction betweenextensions 64 and end 66 (or end 68) ofarcuate slot 62 to generate friction sufficient to prevent axial bias ofspring 25 from shiftingrotor 20 relative tohousing 14. Alternatively,mechanism 10 may also be assembled as follows. First,housing 14 may be positioned in a fixture (not shown) or otherwise retained in a generally horizontal orientation with interior space 18 (FIG. 4 ) facing upwardly.Spring 25 is then positioned overboss 22, and shifted (if required) to causeend 26 ofspring 25 to engage one of the grooves 77 (FIG. 6 ) ofhousing 14. Therotor 20 is then positioned onspring 25 such thatspring 25 is received within cylindrical cavity orspace 83 of rotor 20 (FIGS. 5 and 7 ), and end 28 ofspring 25 is engaged with one of the openings 85 (FIG. 7 ) ofrotor 20. Thearm 34 ofrotor 20 is initially oriented as shown in solid lines inFIG. 4A . This initial position is rotated 180° relative to the assembled orientation ofarm 34 shown in dashed lines inFIG. 4A . The assembled orientation ofarm 34 is also shown in solid lines inFIG. 4 . After placing therotor 20 onto thespring 25, cover 16 is positioned onrotor 20 withextension 42 ofrotor 20 extending through opening 89 ofcover 16. A hex tool (not shown) is positioned in hex opening 86 (FIG. 7 ) ofrotor 20, and therotor 20 is then rotated 180° until it is in the assembled rotational orientation (FIG. 4 ).Rotor 20 may be rotationally constrained due to engagement ofextension 64 onarm 34 of rotor withend arcuate slot 62. Alternatively,rotor 20 may be configured to temporarily engagecover 16 to prevent rotation ofrotor 20 during the assembly process. After thecover 16 is positioned overrotor 20 androtor 20 is rotated to its assembled angular orientation, thehousing 14 and cover 16 are pushed together and interconnected utilizingwedges 52 andopenings 53 as described in more detail above. - Due to the axial compression (deflection),
spring 25 generates about 24N of axial force when assembled. This axialforce biases rotor 20 away fromhousing 14, and into engagement withcover 16. Also, when assembled the rotational deflection or deformation ofspring 25 causes thespring 25 to be preloaded such that it generates a torsional force of about 250 N-mm. Thus, when assembledspring 25 simultaneously generates a substantial axial biasing force and a substantial torsional biasing force. - The axial force/bias acting on
rotor 20 ensures that the rotor does not rattle, and substantially eliminates noises from vibrations or the like. Furthermore,spring 25 has a longer length than conventional torsion springs utilized in prior mechanisms. The longer length allowsspring 25 to have a lower torsional spring constant, thereby reducing the spring biasing force acting on the handle 12 (FIG. 1 ) for a given spring displacement. The total force required by a user in moving (rotating) handle 12 includes force required to overcome the torsion ofspring 25 and the force required to actuateadjustment mechanism 4. Thus, reducing the torsional force generated byspring 25 reduces the total force a user must apply to handle 12 to actuateadjustment mechanism 4. - It is to be understood that variations and modifications can be made on the aforementioned structure without departing from the concepts of the present invention, and further it is to be understood that such concepts are intended to be covered by the following claims unless these claims by their language expressly state otherwise.
Claims (21)
1. A release mechanism of the type that shifts an elongated connector to selectively release an adjustment mechanism, the release mechanism comprising:
a housing defining a pivot element;
a rotor pivotably engaging the pivot element for rotation about an axis, wherein the rotor is adapted to be manually rotated by a user; and wherein the rotor includes a connecting feature that provides for connecting an end of an elongated flexible cable to the rotor such that rotation of the rotor shifts the elongated flexible cable; and
a helical coil spring having a first end connected to the housing, and a second end connected to the rotor, the coil spring being simultaneously compressed and rotationally deformed and simultaneously axially biasing the rotor axially away from the housing along the axis and rotationally biasing the rotor for rotation in a first direction about the axis.
2. The release mechanism of claim 1 , wherein:
the rotor includes a cavity;
the pivot element comprises a boss that is received in the cavity to rotatably interconnect the rotor and the housing; and
the helical coil spring is disposed inside the cavity of the rotor.
3. The release mechanism of claim 2 , wherein:
the housing includes a first spring-connecting structure, and the rotor includes a second spring-connecting structure; and
the coil spring comprises a helical wire coil having a plurality of coils that are disposed around the boss, and includes a first end engaging the housing and a second end engaging the rotor and generating a rotational bias.
4. The release mechanism of claim 2 , wherein:
the rotor includes a central portion having a cylindrical inner surface defining the cavity;
the boss includes a cylindrical outer surface that is spaced apart from the cylindrical inner surface to define an annular gap therebetween; and
the coil spring is disposed in the annular gap.
5. The release mechanism of claim 1 , wherein:
the housing includes first and second portions that are spaced apart to define a gap, and wherein the rotor defines a central portion disposed in the gap, and wherein the spring biases the central portion of the rotor away from the first portion of the housing towards the second portion of the housing, and wherein the rotor slidably engages the second portion of the housing.
6. The release mechanism of claim 5 , wherein:
the housing comprises a first sidewall and an outer sidewall extending transversely from the first sidewall to define a cavity having an open side, and wherein the second portion of the housing comprises a cover closing off at least a portion of the cavity.
7. The release mechanism of claim 6 , wherein:
the cover includes an opening therethrough, and wherein the rotor includes an internal portion disposed in the cavity and an elongated extension extend from the internal portion outwardly through the opening to define an external portion.
8. The release mechanism of claim 7 , wherein:
the external portion includes a handle extending in a direction that is transverse to the axis.
9. The release mechanism of claim 8 , wherein:
the external portion comprises a plurality of outwardly facing teeth, and wherein the handle comprises a separate component having a plurality of inwardly extending teeth engaging the outwardly facing teeth.
10. The release mechanism of claim 7 , wherein:
the housing includes a generally annular groove extending around the boss, and the rotor includes an end portion movably disposed in the groove.
11. The release mechanism of claim 1 , wherein:
the housing includes a first retaining feature;
the rotor includes a second retaining feature; and
the first retaining feature engages the second retaining feature such that the rotor does not shift axially out of engagement with the housing due to the bias of the coil spring unless an external force is applied to the rotor to axially shift the rotor to disengage the first and second retaining features.
12. The release mechanism of claim 11 , wherein:
the rotor is axially movable relative to the housing between first and second axial positions, and wherein axial movement of the rotor relative to the housing from the first position to the second position disengages the first and second retaining features such that the first and second retaining features do not restrict rotation of the rotor relative to the housing when the rotor is in the second position relative to the housing.
13. The release mechanism of claim 12 , wherein:
the rotational bias of the coil spring causes the second stop surface to be biased into contact with the first stop surface.
14. The release mechanism of claim 13 , wherein:
the first stop surface comprises an end surface of an arcuate slot of the housing; and
the second stop surface comprises an extension of the rotor that is disposed in the arcuate slot when the rotor is in the first axial position, and wherein the extension is disposed outside of the arcuate slot when the rotor is in the second axial position.
15. A release mechanism of the type that shifts an elongated connector to selectively release an adjustment mechanism, the release mechanism comprising:
a housing;
a rotor pivotably engaging the housing for rotation about an axis, the rotor having a generally hollow central portion defining a cavity, and wherein the rotor includes a connecting feature that provides for connecting an end of an elongated flexible cable to the rotor such that rotation of the rotor shifts the elongated flexible cable; and
a coil spring having a first end connected to the housing, and a second end connected to the rotor, wherein a plurality of coils of the coil spring are disposed within the cavity of the rotor, and wherein the spring is rotationally deformed to rotationally bias the rotor for rotation in a first direction about the axis.
16. The release mechanism of claim 15 , wherein:
the housing includes a boss that is received in the cavity to rotatably interconnect the rotor and the housing.
17. The release mechanism of claim 16 , wherein:
the hollow central portion includes a generally cylindrical inner surface defining the cavity.
18. The release mechanism of claim 17 , wherein:
the boss comprises a generally cylindrical outer surface that is spaced apart from the cylindrical inner surface of the rotor to define an annular space therebetween, and wherein the spring comprises a helical coil spring that is disposed in the annular space.
19. The release mechanism of claim 15 , wherein:
the housing defines first and second side portions and a space between the first and second side portions, and wherein at least a portion of the rotor is disposed in the space;
the coil spring is compressed and generates an axial force biasing the rotor away from the first side portion of the housing towards the second side portion of the housing.
20. A release mechanism, comprising:
a housing having first and second portions;
a rotor pivotably engaging the housing for rotation about an axis; and
a spring defining a first length when the spring is in a free state wherein the spring is not compressed or stretched, and wherein the spring is in a compressed state when assembled in the release mechanism to define a second length that is substantially shorter than the first length, the spring biasing the rotor axially along the axis away from the first portion of the housing towards the second portion of the housing.
21. The release mechanism of claim 20 , wherein:
the spring comprises a coil spring that torsionally biases the rotor in addition to axially biasing the rotor.
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US14/183,038 US20140157939A1 (en) | 2011-12-09 | 2014-02-18 | Release mechanism |
US15/226,663 US10675997B2 (en) | 2011-12-09 | 2016-08-02 | Method of assembling a release mechanism |
US16/883,172 US11052792B2 (en) | 2011-12-09 | 2020-05-26 | Release mechanism |
Applications Claiming Priority (2)
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US13/315,797 US20140144278A1 (en) | 2011-12-09 | 2011-12-09 | Release mechanism |
US14/183,038 US20140157939A1 (en) | 2011-12-09 | 2014-02-18 | Release mechanism |
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US13/315,797 Continuation-In-Part US20140144278A1 (en) | 2011-12-09 | 2011-12-09 | Release mechanism |
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US15/226,663 Division US10675997B2 (en) | 2011-12-09 | 2016-08-02 | Method of assembling a release mechanism |
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US20140157939A1 true US20140157939A1 (en) | 2014-06-12 |
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US16/883,172 Active US11052792B2 (en) | 2011-12-09 | 2020-05-26 | Release mechanism |
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US15/226,663 Active 2032-09-10 US10675997B2 (en) | 2011-12-09 | 2016-08-02 | Method of assembling a release mechanism |
US16/883,172 Active US11052792B2 (en) | 2011-12-09 | 2020-05-26 | Release mechanism |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10150388B2 (en) * | 2014-10-15 | 2018-12-11 | Adient Luxembourg Holding S.à.r.l. | Actuating device, in particular for a vehicle seat, and vehicle seat |
US10493873B2 (en) * | 2015-03-13 | 2019-12-03 | Adient Luxembourg Holding S.à.r.l. | Hardware system for a vehicle seat |
US11052792B2 (en) | 2011-12-09 | 2021-07-06 | CTC Acquisition Company LLC | Release mechanism |
DE102015207425B4 (en) | 2014-04-25 | 2022-08-11 | Toyota Boshoku Kabushiki Kaisha | vehicle seat |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA3235284A1 (en) | 2021-11-12 | 2023-05-19 | Magna Seating Inc. | Remote handle assembly with modular pulley arrangement |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3958828A (en) * | 1973-02-14 | 1976-05-25 | Fuji Kiko Kabushiki Kaisha | Reclining seat device for motor car |
US6006627A (en) * | 1997-06-27 | 1999-12-28 | Honda Giken Kogyo Kabushiki Kaisha | Operation lever unit for engine-powered working machine |
US20060163924A1 (en) * | 2005-01-25 | 2006-07-27 | Schukra Of North America, Ltd. | Multiple turn mechanism for manual lumbar support adjustment |
US20070232129A1 (en) * | 2006-03-29 | 2007-10-04 | Wescon Products Company | Self locking cable control apparatus |
US20080148889A1 (en) * | 2006-12-22 | 2008-06-26 | Andrew James Elliot | Actuator |
US20080276748A1 (en) * | 2007-05-08 | 2008-11-13 | Bo-Cheng Chen | Gear Shifter |
US20090026825A1 (en) * | 2006-01-27 | 2009-01-29 | Takahiro Ishijima | Seat |
US20100109406A1 (en) * | 2006-01-27 | 2010-05-06 | Katsuya Ueda | Seat |
Family Cites Families (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4384744A (en) | 1981-03-16 | 1983-05-24 | Uop Inc. | Seat reclining mechanism |
US4765681A (en) | 1987-04-03 | 1988-08-23 | Keiper Recaro Incorporated | Seat back recliner with cable release |
DE8801833U1 (en) | 1988-02-12 | 1988-03-31 | Keiper Recaro GmbH & Co, 5630 Remscheid | Backrest for a vehicle seat |
KR100321587B1 (en) | 1993-06-04 | 2002-06-20 | 이토유타카 | Seat level adjusting device for car seat |
US5681005A (en) | 1995-08-11 | 1997-10-28 | Ligon Brothers Manufacturing Company | Lever actuator |
JP2003506883A (en) | 1999-08-10 | 2003-02-18 | シリコン ジェネシス コーポレイション | Cleavage process for manufacturing multi-layer substrates with low implant dose |
US6842959B2 (en) | 2001-01-25 | 2005-01-18 | Dahti, Inc. | Load bearing fabric attachment and associated method |
CA2525902A1 (en) | 2001-01-25 | 2002-07-25 | Jsj Seating Company Texas, L.P. | Office chair |
US6688443B2 (en) | 2001-11-07 | 2004-02-10 | L & P Property Management Company | Apparatus and method for double clutch actuator |
US6691851B2 (en) | 2001-10-03 | 2004-02-17 | L & P Property Management Company | Apparatus and method for ratchet actuator |
US6637575B2 (en) | 2001-10-03 | 2003-10-28 | L & P Property Management Company | Apparatus and method for thin profile ratchet actuator |
EP1432594B1 (en) | 2001-10-03 | 2006-07-26 | L & P Property Management Company | Apparatus and method for return actuator |
US6877597B2 (en) | 2003-02-18 | 2005-04-12 | Grand Rapids Controls, Inc. | Clutch mechanism |
JP4064331B2 (en) | 2003-10-14 | 2008-03-19 | 本田技研工業株式会社 | Seat adjuster device |
US6997847B2 (en) * | 2004-01-27 | 2006-02-14 | L&P Property Management Company | Planetary gear actuator apparatus and method |
US7451958B2 (en) | 2005-07-28 | 2008-11-18 | Brunswick Corporation | Cable operated seat mount locks for rotatable vehicle seats |
US7530638B2 (en) | 2005-09-01 | 2009-05-12 | Toyota Motor Engineering & Manufacturing North America, Inc. | Dual action seat release mechanism |
JP4185935B2 (en) | 2006-01-27 | 2008-11-26 | トヨタ自動車株式会社 | Sheet |
US20070203439A1 (en) * | 2006-02-24 | 2007-08-30 | Water Pik, Inc. | Water jet unit and handle |
US7556315B2 (en) | 2006-03-31 | 2009-07-07 | Lear Corporation | Latch actuator system |
US8011269B2 (en) | 2006-04-07 | 2011-09-06 | Capro Ltd. | Actuator |
JP4936361B2 (en) * | 2006-06-14 | 2012-05-23 | テイ・エス テック株式会社 | Operation device with lock for vehicle seat, etc. |
US7631938B2 (en) * | 2006-08-22 | 2009-12-15 | Grand Rapids Controls Company, Llc | Stored energy control mechanism |
DE102011106285B4 (en) * | 2011-07-04 | 2013-08-22 | Keiper Gmbh & Co. Kg | Fitting system for a vehicle seat and vehicle seat |
US20140157939A1 (en) | 2011-12-09 | 2014-06-12 | Grand Rapids Controls Company, Llc | Release mechanism |
US20140144278A1 (en) * | 2011-12-09 | 2014-05-29 | Mark G. Tomandl | Release mechanism |
DE102012010402B3 (en) * | 2012-05-22 | 2013-10-17 | Keiper Gmbh & Co. Kg | Fitting for a vehicle seat and vehicle seat |
DE102014207363A1 (en) * | 2014-01-31 | 2015-08-06 | Johnson Controls Components Gmbh & Co. Kg | Backrest adjuster and vehicle seat with a backrest adjuster |
JP6237325B2 (en) * | 2014-02-24 | 2017-11-29 | アイシン精機株式会社 | Seat reclining device |
US10385955B2 (en) * | 2014-11-07 | 2019-08-20 | Kongsberg Automotive Ab | Actuating device for actuating a cable |
US9889774B2 (en) * | 2015-08-07 | 2018-02-13 | Fisher & Company, Incorporated | Release mechanism for seat recliner assembly |
US20180326882A1 (en) | 2017-05-12 | 2018-11-15 | CTC Acquisition Company LLC | Cable assembly for vehicle seat headrest |
FR3074516B1 (en) * | 2017-12-01 | 2019-11-22 | Somfy Activites Sa | ELECTROMECHANICAL ACTUATOR AND DOMOTIC INSTALLATION COMPRISING SUCH ACTUATOR |
-
2014
- 2014-02-18 US US14/183,038 patent/US20140157939A1/en not_active Abandoned
-
2016
- 2016-08-02 US US15/226,663 patent/US10675997B2/en active Active
-
2020
- 2020-05-26 US US16/883,172 patent/US11052792B2/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3958828A (en) * | 1973-02-14 | 1976-05-25 | Fuji Kiko Kabushiki Kaisha | Reclining seat device for motor car |
US6006627A (en) * | 1997-06-27 | 1999-12-28 | Honda Giken Kogyo Kabushiki Kaisha | Operation lever unit for engine-powered working machine |
US20060163924A1 (en) * | 2005-01-25 | 2006-07-27 | Schukra Of North America, Ltd. | Multiple turn mechanism for manual lumbar support adjustment |
US20090026825A1 (en) * | 2006-01-27 | 2009-01-29 | Takahiro Ishijima | Seat |
US20100109406A1 (en) * | 2006-01-27 | 2010-05-06 | Katsuya Ueda | Seat |
US20070232129A1 (en) * | 2006-03-29 | 2007-10-04 | Wescon Products Company | Self locking cable control apparatus |
US7938039B2 (en) * | 2006-03-29 | 2011-05-10 | Wescon Products Company | Self locking cable control apparatus |
US20080148889A1 (en) * | 2006-12-22 | 2008-06-26 | Andrew James Elliot | Actuator |
US20080276748A1 (en) * | 2007-05-08 | 2008-11-13 | Bo-Cheng Chen | Gear Shifter |
Non-Patent Citations (2)
Title |
---|
Define helical coil spring, Google.com.search, 1/24/16. * |
Images for define helical coil spring, Google.com.search, 1/24/16. * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11052792B2 (en) | 2011-12-09 | 2021-07-06 | CTC Acquisition Company LLC | Release mechanism |
DE102015207425B4 (en) | 2014-04-25 | 2022-08-11 | Toyota Boshoku Kabushiki Kaisha | vehicle seat |
US10150388B2 (en) * | 2014-10-15 | 2018-12-11 | Adient Luxembourg Holding S.à.r.l. | Actuating device, in particular for a vehicle seat, and vehicle seat |
US10493873B2 (en) * | 2015-03-13 | 2019-12-03 | Adient Luxembourg Holding S.à.r.l. | Hardware system for a vehicle seat |
Also Published As
Publication number | Publication date |
---|---|
US10675997B2 (en) | 2020-06-09 |
US11052792B2 (en) | 2021-07-06 |
US20180229630A9 (en) | 2018-08-16 |
US20160339811A1 (en) | 2016-11-24 |
US20200282876A1 (en) | 2020-09-10 |
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Owner name: GRAND RAPIDS CONTROLS COMPANY, LLC, MICHIGAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:TOMANDL, MARK G.;REEL/FRAME:032628/0128 Effective date: 20140408 |
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Owner name: CTC ACQUISITION COMPANY LLC, MICHIGAN Free format text: CHANGE OF NAME;ASSIGNOR:GRAND RAPIDS CONTROLS COMPANY, LLC;REEL/FRAME:052607/0616 Effective date: 20120118 |