US2522596A - Altitude switch - Google Patents
Altitude switch Download PDFInfo
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- US2522596A US2522596A US664718A US66471846A US2522596A US 2522596 A US2522596 A US 2522596A US 664718 A US664718 A US 664718A US 66471846 A US66471846 A US 66471846A US 2522596 A US2522596 A US 2522596A
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- Prior art keywords
- pressure
- solenoid
- contacts
- spring
- aneroid
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H35/00—Switches operated by change of a physical condition
- H01H35/24—Switches operated by change of fluid pressure, by fluid pressure waves, or by change of fluid flow
- H01H35/26—Details
- H01H35/30—Means for transmitting pressure to pressure-responsive operating part, e.g. by capsule and capillary tube
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
- B60R16/005—Electro-mechanical devices, e.g. switched
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H35/00—Switches operated by change of a physical condition
- H01H35/24—Switches operated by change of fluid pressure, by fluid pressure waves, or by change of fluid flow
Definitions
- This invention relates to an altitude switch. and more particularly to an altitude switch which is closed and then opened at dverent predetermined values of absolute pressure.
- An object of my present invention is to provide an altitude switch in which an aneroid will actuate a circuit making device when barometric pressure reaches a predetermined value, and which will restore said device to its initial condition when the absolute pressure returns to a second predetermined value.
- Another object of my invention is to provide an altitude switch of the character described in which the absolute pressure values at which the circuit making device will be actuated by the aneroid, and at which said device is restored to its initial condition are readily adjustable.
- a further object of my invention is to provide an altitude switch of the character described in which the expansion and contraction of the aneroid is ail'ected by the actuation of the circuit making device to vary the absolute pressure at which said device ls restored to its initial condition by said aneroid.
- Still a further object of the present invention is to provide an altitude switch of the character described in which immediate recycling is prevented upon restoration of the circuit making device to initial condition in the event the absolute pressure varies a small amount.
- Still another object of the invention is to provide a highly compact and rugged altitude switch of the character described which shall be automatic and positive in its operation, relatively inexpensive to manufacture, which shall4 have a large variety of applications and yet be practical and efllcient to a high degree in use.
- Figure l is a side view of an altitude switch, portions of which have been broken away, the working parts of said switch being shown in elevation and cross section, while,
- Figure 2 is a wiring diagram showing the electric connections for said altitude switch.
- the altitude switch herein provided comprises an aneroid and a solenoid mounted in a, sealed casing, ambient pressures being applied to the interior of said casing through a suitable inlet.
- the aneroid carries a pilot contact which is adapted upon expansion of the aneroid to engage a stationary contact to complete an energizing circuit for the solenoid. Energization of the sclenoid will cause the core ythereof to be retracted, the movement of the core being used to open and close the controlled circuit.
- Two springs are associated with the solenoid of the herein described altitude switch.
- One of said springs is a return spring normally provided in solenoid construction for the return of the core to its initial condition upon de-energization of the solenoid.
- the second spring is interposed between the core and the aneroid.
- the return spring of the solenoid causes pressure to be exerted uponthe aneroid due to the bias of the second spring. ,'Ihus, the normal expansion of the aneroid is retarded by the increased pressure thereon by the aforesaid spring.
- the pilot contacts Upon sumcient expansion of the aneroid against the bias of the spring, the pilot contacts will close to energize the solenoid. 'I'he energization of the solenoid will cause the core to retract, releasing the pressure of the aneroid spring to permit the aneroid to expand normally. The expansion of the aneroid upon release of the spring pressure will cause the pilot contacts to remain closed until the absolute pressure is reduced in value to a lesser value than that at which the pilot contacts were iirst closed. The disengagement of the pilot contacts will open the energizing circuit of the solenoid permitting the solenoid spring to return the core to its initial position causing the aneroid spring to compress the aneroid in the manner previously described. The pilot contacts are thus opened a greater amount which will prevent immediate recycling in the event that the absolute pressure is decreased a small amount.
- the shell I4 is formed with a threaded openi A.3.. ing 28 to which a pressure line (not shown) may be connected.
- a pressure line (not shown) may be connected.
- a supporting wall 2I provided with a series of ports 22. Fixed to the center of said wall and concentric with opening 28, as by screw 28, is the pressure responsive member I3.
- the member I 8 is thus ilxed within a sealed casing into which the controlling pressures may be conducted by way of opening 28 and the ports 22.
- the shell I4 is further provided with a transverse opening 24, concentric with a threaded opening in a block 28 fixed within the shell. Threaded in the opening 25 is a screw 21, the purpose ⁇ oi' which will be hereinafter apparent.
- the interior end 28 of said screw is beveled, while the cap or slotted end 28 extends exteriorly to said casing.
- the shank 38 of the screw is sealed against pressure leaks by bushings 3l.
- the shell I5 of the casing is provided with an electrical socket connector 85 (broken away) to which the various wires hereinafter described are soldered. Connection of the altitude switch into the controlled circuit or circuits is made by a plug connector (not shown) fitted into the socket connector.
- the solenoid I2 is ilxed within the casing II by screws 36 (one shown) passing through a .ange 31 on said solenoid and threaded into a Vby suitable means, and insulated therefrom, a
- contact arm 5I adapted to engage the contacts 48 when the solenoid is energized, as indicated in the gures, and to engage the contacts 42 when said solenoid is de-energized.
- the solenoid core 41 is formed with a threaded end portion 52. Threaded thereon is a shouldered member 53 and a locknut 54. Abutting the shoulder of member 53 is a coil spring 55, the other end of which abuts a shouldered plate 58 fixed on the aneroid I3. The tension of spring 55 may be adjusted by means of shouldered member and the locknut.
- the spring is weaker than the solenoid return spring 48 previously described. Thus, when the solenoid is de-energized, the return spring 48 will return the core to its initial condition in which contacts 42 are engaged by contactor 5I, to compress the spring 55.
- Means is now provided to energize the solenoid I2 when a predetermined pressure ail'ects the member I3, and to de-energize ⁇ the solenoid when a second predetermined pressure affects said member.
- the load resistors 51 and 88 illustrated herein may be any type of electrical equipment, such as electrically driven air pumps for superchargers, control mechanism for pulling a plane out of a dive, retracting mechanism for ilap or landing gears on airplanes when predetermined pressure due to airspeed is reached, etc.
- the pressure at which the aneroid will close the contacts 88. 28 is determined by the distance traveled by contact 88 upon the expansion of the aneroid. The distance may be varied by turning the screw 21 to increase or decrease the diameter of contact 28 in the line of travel of the contact 88.
- the pressure at which the solenoid is energized may be readily changed from the outside of the casing II. This is also true of the pressure at which the solenoid is deenergized, since the pressure on the contacts 88, 28 upon energization of the solenoid will be increased or decreased, as the case may be, by the increase or decrease of the diameter of contact 28.
- De-energization of the solenoid will be affected upon the disengagement of the contacts 88, 28. Since the expansion oi the aneroid was retarded by the compression of spring 55 by the solenoid, the pressure value at which the contacts were closed is lower than that at which the contacts would close were there no added spring pressure added thereto. Upon energization of the solenoid the pressure of spring 55 on member ⁇ I3 is relieved permitting the member to expand. Thus upon an increase in ambient pressure, the aneroid will contract until a pressure is reached where the aneroid is suillciently contracted to move the contact 88 away from contact 28. The pressure at which the contacts are opened will be higher than that at which the contacts first were closed since the pressure of spring 55 is not aiding in contracting the aneroid.
- the pressure responsive member I3 instead of being an evacuated capsule as described, actuated by the pressure within the casing II; could be used to operate the herein described switch upon a predetermined pressure diifferential affecting the same.
- the interior of member I3 would be connected to the exterior of the casing II by a suitable line to which a second pressure line could be fastened in the manner herein described for the threaded opening 28.
- the Pitot tube pressures could be used to expand and contract the member I3; the dynamic pressure delivered to the interior of member i3, and the static pressure to the interior of casing il, or vice versa.
- predetermined pressure will include a predetermined pressure within the casing H, and a predetermined pressure diil'erential of the pressure within member I3 and of the pressure within casing Il.
- an altitude switch adapted to be used in an airplane to control many different types of electrical equipment at or between predetermined altitudes (pressure).
- a pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said member at a predetermined pressure, and a circuit making device actuated upon actuation of said contacts, said device including resilient means for applying pressure on said member which is relieved upon actuation of said device permitting said contacts to be returned to initial condition by said member when a second predetermined pressure affects said member.
- a pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said member at a predetermined pressure, a circuit making device actuated upon actuation of said contacts, said device including resilient l means for applying pressure on said member which is relieved upon actuation of said device permitting said contacts to be returned to initial condition by said member when ⁇ a second predetermined pressure affects said member, and means for varying the values of the predetermined pressures at which said contacts are actuated and at which they are restored to initial condition.
- a pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said member at a predetermined pressure, a solenoid energized upon actuation of said contacts, and a resilient member associated with said solenoid for applying pressure on said member, said pressure being relieved upon energization of said solenoid permitting said contacts to be restored to initial condition by said member when a second predetermined pressure aects said member.
- 4A pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said .member at a predetermined pressure, a solenoid energized upon actuation of said contacts, a resilient member associated with said solenoid for applying pressure on said member, said pressure being relieved upon energization of said solenoid-'permitting said contacts to be restored to initial condition by said member when a second predetermined pressure ailects said member, and means for varying the bias of said resilient member to adjust the pressures at which said member will actuate said contacts and restore said contacts to initial condition.
- a pressure switch comprising a pressure re sponsive member,v a contact movable therewith, a stationary contact adapted to be engaged by said flrst contact when a predetermined pressure affects said member, a solenoid energized upon engagement of said contacts, a resilient member associated with said solenoid for applying pressure on said member, said pressure being relieved upon energization of said solenoid permitting the disengagement or said contacts by said member when a second predetermined pressure ailects said member.
- a pressurerswitch comprising a pressure responsive member, a contact movable therewith, a stationary contact adapted to be engaged by said contact when a predetermined pressure aects said member, means for varying the travel of said first contact by adjustment of said second contact, and a resilient member associated with said solenoid for applying pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts by said pressure member when a second predetermined pressure ailects said pressure responsive member.
- a pressure switch comprising a pressure responsive member, a contact movable therewith, a stationary contact adapted to be engaged by said contact when a predetermined pressure affects said member, means for varying the travel of said ilrst contact by adjustment of said second contact, a resilient member associated with said solenoid for applying pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts by said pressure member when a second predetermined pressure affects said pressure responsive member, and means for biasing said resilient member to adjust the pressure applied on said pressure member by said resilient member.
- a pressure switch comprising an aneroid, a contact movable thereby, a second contact adapted to be engaged by said ilrst contact when a predetermined pressure affects said aneroid, a solenoid adapted to be energized upon engagement of said contacts, a movable core for said solenoid, and a spring for returning said core to an initial condition upon de-energization of said solenoid; a second spring of less tensionthan said iirst spring adapted to be biased by said core, said second spring adapted to apply pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts when a second predetermined pressure afl'ects said pressure responsive member.
- a pressure switch comprising an aneroid, a contact movable thereby, a second contact adapted to be engaged by said ilrst contact when a predetermined pressure affects said aneroid, means for vai-ying the travel of said iirst contact by adjustment of said second contact, a solenoid adapted to be energized upon closure of said contacts, a movable core for said solenoid and a spring to return same to an initial position upon de-energization of said solenoid, a second spring oi' less tension than said first spring adapted to be biased by said core, said second spring adapted to apply pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts when a second predetermined pressure affects said pressure member, and means for biasing said second spring to adjust the pressure applied onv said pressure responsive member by said spring.
- means comprising an axially displaceable member adapted for movement in one direction to energize said electrical means and for movement in an opposite direction to de-energise said electrical means, means comprising a yieldable wall adapted for movement in one direction or the other relative to said displaoeable member in response to changes in ambient pressure, means associated with one side of said wall adapted to cause displacement of said member in response to movements of said wall. and resilient means interposed between said member and said wall to restrain movement of said wall.
- means comprising an axially displaceable member adapted for movement in one direction to close said switching means and for movement in an opposite direction to open said switching means, means comprising a yieldable wall adapted for movement toward said displaceable member or away therefrom in response to changes in ambient pressure, means associated with one side member and said wall to restrain movement of said wall in one position o! said member.
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Switches Operated By Changes In Physical Conditions (AREA)
- Measuring Fluid Pressure (AREA)
Description
Sept. 19, 1950 J, E, BEVINS 2,522,596
vALTl'I'UDE SWITCH Filed April 25, 1946 INVE NTOR .JH/7755 EBEV/NS BY f" AT RNEY Patented Sept. 19, 1950 ALTITUDE SWITCH James E. Devin, Ramsey, N. J., assignor to Bendix Aviation Corporation, Teterboro, N. J., a
corporation ot Ilelaware Application April z5, 194e, serai No. 664,118
` 11 claims. (ci. zoo-s1) This invention relates to an altitude switch. and more particularly to an altitude switch which is closed and then opened at diilerent predetermined values of absolute pressure.
An object of my present invention is to provide an altitude switch in which an aneroid will actuate a circuit making device when barometric pressure reaches a predetermined value, and which will restore said device to its initial condition when the absolute pressure returns to a second predetermined value.
Another object of my invention is to provide an altitude switch of the character described in which the absolute pressure values at which the circuit making device will be actuated by the aneroid, and at which said device is restored to its initial condition are readily adjustable.
A further object of my invention is to provide an altitude switch of the character described in which the expansion and contraction of the aneroid is ail'ected by the actuation of the circuit making device to vary the absolute pressure at which said device ls restored to its initial condition by said aneroid.
Still a further object of the present invention is to provide an altitude switch of the character described in which immediate recycling is prevented upon restoration of the circuit making device to initial condition in the event the absolute pressure varies a small amount.
Still another object of the invention is to provide a highly compact and rugged altitude switch of the character described which shall be automatic and positive in its operation, relatively inexpensive to manufacture, which shall4 have a large variety of applications and yet be practical and efllcient to a high degree in use.
Other objects of this invention will in part be obvious and in part hereinafter pointed out.
The invention accordingly consists in the features of construction, combinations of elements, and arrangement of parts which will be exempiiiled in the construction Ihereinafter described, and of which the scope of application will be indi cated in the following claims.
In the accompanying drawings in which one oi the various possible illustrative embodiments of my invention is shown,
Figure l is a side view of an altitude switch, portions of which have been broken away, the working parts of said switch being shown in elevation and cross section, while,
Figure 2 is a wiring diagram showing the electric connections for said altitude switch.
The altitude switch herein provided comprises an aneroid and a solenoid mounted in a, sealed casing, ambient pressures being applied to the interior of said casing through a suitable inlet. The aneroid carries a pilot contact which is adapted upon expansion of the aneroid to engage a stationary contact to complete an energizing circuit for the solenoid. Energization of the sclenoid will cause the core ythereof to be retracted, the movement of the core being used to open and close the controlled circuit.
Two springs are associated with the solenoid of the herein described altitude switch. One of said springs is a return spring normally provided in solenoid construction for the return of the core to its initial condition upon de-energization of the solenoid. The second spring., of less resilience than the first spring, is interposed between the core and the aneroid. When the pressure is higher than the predetermined pressure at which the solenoid is to be energized, the return spring of the solenoid causes pressure to be exerted uponthe aneroid due to the bias of the second spring. ,'Ihus, the normal expansion of the aneroid is retarded by the increased pressure thereon by the aforesaid spring. Upon sumcient expansion of the aneroid against the bias of the spring, the pilot contacts will close to energize the solenoid. 'I'he energization of the solenoid will cause the core to retract, releasing the pressure of the aneroid spring to permit the aneroid to expand normally. The expansion of the aneroid upon release of the spring pressure will cause the pilot contacts to remain closed until the absolute pressure is reduced in value to a lesser value than that at which the pilot contacts were iirst closed. The disengagement of the pilot contacts will open the energizing circuit of the solenoid permitting the solenoid spring to return the core to its initial position causing the aneroid spring to compress the aneroid in the manner previously described. The pilot contacts are thus opened a greater amount which will prevent immediate recycling in the event that the absolute pressure is decreased a small amount.
Referring now in detail to the drawings, I0
designates an altitude switch embodying the in- The shell I4 is formed with a threaded openi A.3.. ing 28 to which a pressure line (not shown) may be connected. Within the opening 28 is a supporting wall 2I provided with a series of ports 22. Fixed to the center of said wall and concentric with opening 28, as by screw 28, is the pressure responsive member I3. The member I 8 is thus ilxed within a sealed casing into which the controlling pressures may be conducted by way of opening 28 and the ports 22.
The shell I4 is further provided with a transverse opening 24, concentric with a threaded opening in a block 28 fixed within the shell. Threaded in the opening 25 is a screw 21, the purpose `oi' which will be hereinafter apparent. The interior end 28 of said screw is beveled, while the cap or slotted end 28 extends exteriorly to said casing. The shank 38 of the screw is sealed against pressure leaks by bushings 3l.
The shell I5 of the casing is provided with an electrical socket connector 85 (broken away) to which the various wires hereinafter described are soldered. Connection of the altitude switch into the controlled circuit or circuits is made bya plug connector (not shown) fitted into the socket connector.
The solenoid I2 is ilxed within the casing II by screws 36 (one shown) passing through a .ange 31 on said solenoid and threaded into a Vby suitable means, and insulated therefrom, a
contact arm 5I adapted to engage the contacts 48 when the solenoid is energized, as indicated in the gures, and to engage the contacts 42 when said solenoid is de-energized.
The solenoid core 41 is formed with a threaded end portion 52. Threaded thereon is a shouldered member 53 and a locknut 54. Abutting the shoulder of member 53 is a coil spring 55, the other end of which abuts a shouldered plate 58 fixed on the aneroid I3. The tension of spring 55 may be adjusted by means of shouldered member and the locknut. The spring is weaker than the solenoid return spring 48 previously described. Thus, when the solenoid is de-energized, the return spring 48 will return the core to its initial condition in which contacts 42 are engaged by contactor 5I, to compress the spring 55.
Compression of spring 55 will exert a pressure on the member I3. Thus, in the case of decreasing ambient pressure, the expansion of the aneroid will be retarded by the pressure vexerted by the spring. Upon actuation of the solenoid, the core will be moved against the bias of spring 48, releasing the compression of spring 55 as shown in Figure 1. The aneroid I3 may thus expand with but a small pressure thereon due to the spring 55.
Means is now provided to energize the solenoid I2 when a predetermined pressure ail'ects the member I3, and to de-energize `the solenoid when a second predetermined pressure affects said member.
To this end, there is ilxed to-the member I3 an electrical contact, grounded as at 8| through a lead 82 (Figure 2). The expansion of the 4 aneroid upon a decrease in ambient pressure within the casing II, will move the contact 58 into engagement with the beveled contact 28 (of screw 21). Engagement oi' contacts 88, 28 will complete an energizing circuit for the solenoid which may be traced in Figure 2 from the ground connection 8|, through the lead 82, contacts 88, 28, through a lead 83, thence through coil 48 of the solenoid, lead 84, to connector 35; continuing through the connector and lead to a high side of a grounded battery 88. Actuation of the solenoid will break the circuit through the contacts 42 to the loadresistor 81, and complete the circuit through contacts 48 to the load resistor 88.
The load resistors 51 and 88 illustrated herein may be any type of electrical equipment, such as electrically driven air pumps for superchargers, control mechanism for pulling a plane out of a dive, retracting mechanism for ilap or landing gears on airplanes when predetermined pressure due to airspeed is reached, etc.
The pressure at which the aneroid will close the contacts 88. 28 is determined by the distance traveled by contact 88 upon the expansion of the aneroid. The distance may be varied by turning the screw 21 to increase or decrease the diameter of contact 28 in the line of travel of the contact 88. Thus the pressure at which the solenoid is energized may be readily changed from the outside of the casing II. This is also true of the pressure at which the solenoid is deenergized, since the pressure on the contacts 88, 28 upon energization of the solenoid will be increased or decreased, as the case may be, by the increase or decrease of the diameter of contact 28.
De-energization of the solenoid will be affected upon the disengagement of the contacts 88, 28. Since the expansion oi the aneroid was retarded by the compression of spring 55 by the solenoid, the pressure value at which the contacts were closed is lower than that at which the contacts would close were there no added spring pressure added thereto. Upon energization of the solenoid the pressure of spring 55 on member` I3 is relieved permitting the member to expand. Thus upon an increase in ambient pressure, the aneroid will contract until a pressure is reached where the aneroid is suillciently contracted to move the contact 88 away from contact 28. The pressure at which the contacts are opened will be higher than that at which the contacts first were closed since the pressure of spring 55 is not aiding in contracting the aneroid.
Upon opening of contacts 88, 28 the solenoid will be de-energized whereupon spring 55 will again compress the aneroid. The contact 88 is thus moved away quickly from contact 28 upon solenoid de-energization to prevent the immediate closure thereof should the ambient pressure affecting the aneroid momentarily decrease at that instant.
From the foregoing it will be obvious that the pressure responsive member I3, instead of being an evacuated capsule as described, actuated by the pressure within the casing II; could be used to operate the herein described switch upon a predetermined pressure diifferential affecting the same. The interior of member I3 would be connected to the exterior of the casing II by a suitable line to which a second pressure line could be fastened in the manner herein described for the threaded opening 28. In the use of the switch for controlling aircraft equipment, the Pitot tube pressures could be used to expand and contract the member I3; the dynamic pressure delivered to the interior of member i3, and the static pressure to the interior of casing il, or vice versa.
Thus in the claims, the expression predetermined pressure will include a predetermined pressure within the casing H, and a predetermined pressure diil'erential of the pressure within member I3 and of the pressure within casing Il.
It will thus be seen that there is provided an altitude switch adapted to be used in an airplane to control many different types of electrical equipment at or between predetermined altitudes (pressure).
As various possible embodiments may be made of the above invention, and as various changes may be made in the embodiment above set forth, it is to be understood that all matter herein set forth, or shown in the accompanying drawings is to be interpreted as illustrative, and not in a limiting sense.
Having th-us described my invention, I claim as new and desire to secure by Letters Patent:
1. A pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said member at a predetermined pressure, and a circuit making device actuated upon actuation of said contacts, said device including resilient means for applying pressure on said member which is relieved upon actuation of said device permitting said contacts to be returned to initial condition by said member when a second predetermined pressure affects said member.
2. A pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said member at a predetermined pressure, a circuit making device actuated upon actuation of said contacts, said device including resilient l means for applying pressure on said member which is relieved upon actuation of said device permitting said contacts to be returned to initial condition by said member when` a second predetermined pressure affects said member, and means for varying the values of the predetermined pressures at which said contacts are actuated and at which they are restored to initial condition.
3. A pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said member at a predetermined pressure, a solenoid energized upon actuation of said contacts, and a resilient member associated with said solenoid for applying pressure on said member, said pressure being relieved upon energization of said solenoid permitting said contacts to be restored to initial condition by said member when a second predetermined pressure aects said member.
4. 4A pressure switch comprising a pressure responsive member, contacts adapted to be actuated by said .member at a predetermined pressure, a solenoid energized upon actuation of said contacts, a resilient member associated with said solenoid for applying pressure on said member, said pressure being relieved upon energization of said solenoid-'permitting said contacts to be restored to initial condition by said member when a second predetermined pressure ailects said member, and means for varying the bias of said resilient member to adjust the pressures at which said member will actuate said contacts and restore said contacts to initial condition.
5. A pressure switch comprising a pressure re sponsive member,v a contact movable therewith, a stationary contact adapted to be engaged by said flrst contact when a predetermined pressure affects said member, a solenoid energized upon engagement of said contacts, a resilient member associated with said solenoid for applying pressure on said member, said pressure being relieved upon energization of said solenoid permitting the disengagement or said contacts by said member when a second predetermined pressure ailects said member.
6. A pressurerswitch comprising a pressure responsive member, a contact movable therewith, a stationary contact adapted to be engaged by said contact when a predetermined pressure aects said member, means for varying the travel of said first contact by adjustment of said second contact, and a resilient member associated with said solenoid for applying pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts by said pressure member when a second predetermined pressure ailects said pressure responsive member.
1. A pressure switch comprising a pressure responsive member, a contact movable therewith, a stationary contact adapted to be engaged by said contact when a predetermined pressure affects said member, means for varying the travel of said ilrst contact by adjustment of said second contact, a resilient member associated with said solenoid for applying pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts by said pressure member when a second predetermined pressure affects said pressure responsive member, and means for biasing said resilient member to adjust the pressure applied on said pressure member by said resilient member.
8. A pressure switch comprising an aneroid, a contact movable thereby, a second contact adapted to be engaged by said ilrst contact when a predetermined pressure affects said aneroid, a solenoid adapted to be energized upon engagement of said contacts, a movable core for said solenoid, and a spring for returning said core to an initial condition upon de-energization of said solenoid; a second spring of less tensionthan said iirst spring adapted to be biased by said core, said second spring adapted to apply pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts when a second predetermined pressure afl'ects said pressure responsive member.
9. A pressure switch comprising an aneroid, a contact movable thereby, a second contact adapted to be engaged by said ilrst contact when a predetermined pressure affects said aneroid, means for vai-ying the travel of said iirst contact by adjustment of said second contact, a solenoid adapted to be energized upon closure of said contacts, a movable core for said solenoid and a spring to return same to an initial position upon de-energization of said solenoid, a second spring oi' less tension than said first spring adapted to be biased by said core, said second spring adapted to apply pressure on said pressure member, said pressure being relieved upon energization of said solenoid permitting the disengagement of said contacts when a second predetermined pressure affects said pressure member, and means for biasing said second spring to adjust the pressure applied onv said pressure responsive member by said spring.
10. In combination with a controlled electrical means, means comprising an axially displaceable member adapted for movement in one direction to energize said electrical means and for movement in an opposite direction to de-energise said electrical means, means comprising a yieldable wall adapted for movement in one direction or the other relative to said displaoeable member in response to changes in ambient pressure, means associated with one side of said wall adapted to cause displacement of said member in response to movements of said wall. and resilient means interposed between said member and said wall to restrain movement of said wall.
1l. In combination with electrical switching means, means comprising an axially displaceable member adapted for movement in one direction to close said switching means and for movement in an opposite direction to open said switching means, means comprising a yieldable wall adapted for movement toward said displaceable member or away therefrom in response to changes in ambient pressure, means associated with one side member and said wall to restrain movement of said wall in one position o! said member.
' JAMES E. BEVINB.
REFERENCES CITED The following references are of record in the nie of this patent:
UNITED STATES PATENTS Number Name "Date 953,028 Gris'com Mar. 29, 1910 1,830,859 Davis Oct. 4. 1932 1,922,452 Parks Aug. 15, 1933 2,448,167 Baak Aug. 31, 1948 FOREIGN PATENTS Number Country Date 454,931 Great Britain Oct. 6, 1936
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
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US664718A US2522596A (en) | 1946-04-25 | 1946-04-25 | Altitude switch |
GB8255/47A GB633638A (en) | 1946-04-25 | 1947-03-26 | Improvements in or relating to fluid pressure actuated electric switches |
FR945660D FR945660A (en) | 1946-04-25 | 1947-04-25 | Pressure switch |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US664718A US2522596A (en) | 1946-04-25 | 1946-04-25 | Altitude switch |
Publications (1)
Publication Number | Publication Date |
---|---|
US2522596A true US2522596A (en) | 1950-09-19 |
Family
ID=24667178
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US664718A Expired - Lifetime US2522596A (en) | 1946-04-25 | 1946-04-25 | Altitude switch |
Country Status (3)
Country | Link |
---|---|
US (1) | US2522596A (en) |
FR (1) | FR945660A (en) |
GB (1) | GB633638A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2725446A (en) * | 1950-11-18 | 1955-11-29 | Westinghouse Electric Corp | Circuit interrupter |
US2911573A (en) * | 1949-11-16 | 1959-11-03 | Rabinow Jacob | Multiple point altimeter for use with toss bombing integrators |
US2931874A (en) * | 1953-10-08 | 1960-04-05 | Audley B Leaman | Explosive switch |
US2986617A (en) * | 1959-03-16 | 1961-05-30 | Westinghouse Air Brake Co | Fluid compressor motor control apparatus |
US2990780A (en) * | 1959-02-16 | 1961-07-04 | Robertshaw Fulton Controls Co | Control for fluid system |
US3046369A (en) * | 1959-04-27 | 1962-07-24 | Beatrice A Hicks | Device for sensing gas density |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US953028A (en) * | 1907-09-26 | 1910-03-29 | Alfred C Griscom | Automatic switch mechanism. |
US1880859A (en) * | 1932-10-04 | Automatic starting means fob internal combustion engines | ||
US1922452A (en) * | 1932-05-05 | 1933-08-15 | Vapor Car Heating Co Inc | Automatic reclosing circuit breaker and indicator |
GB454931A (en) * | 1935-04-06 | 1936-10-06 | George Maurice Wright | Improvements in altimeters for use in aircraft |
US2448167A (en) * | 1942-12-12 | 1948-08-31 | Honeywell Regulator Co | Flap control device responsive to air speed |
-
1946
- 1946-04-25 US US664718A patent/US2522596A/en not_active Expired - Lifetime
-
1947
- 1947-03-26 GB GB8255/47A patent/GB633638A/en not_active Expired
- 1947-04-25 FR FR945660D patent/FR945660A/en not_active Expired
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1880859A (en) * | 1932-10-04 | Automatic starting means fob internal combustion engines | ||
US953028A (en) * | 1907-09-26 | 1910-03-29 | Alfred C Griscom | Automatic switch mechanism. |
US1922452A (en) * | 1932-05-05 | 1933-08-15 | Vapor Car Heating Co Inc | Automatic reclosing circuit breaker and indicator |
GB454931A (en) * | 1935-04-06 | 1936-10-06 | George Maurice Wright | Improvements in altimeters for use in aircraft |
US2448167A (en) * | 1942-12-12 | 1948-08-31 | Honeywell Regulator Co | Flap control device responsive to air speed |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2911573A (en) * | 1949-11-16 | 1959-11-03 | Rabinow Jacob | Multiple point altimeter for use with toss bombing integrators |
US2725446A (en) * | 1950-11-18 | 1955-11-29 | Westinghouse Electric Corp | Circuit interrupter |
US2931874A (en) * | 1953-10-08 | 1960-04-05 | Audley B Leaman | Explosive switch |
US2990780A (en) * | 1959-02-16 | 1961-07-04 | Robertshaw Fulton Controls Co | Control for fluid system |
US2986617A (en) * | 1959-03-16 | 1961-05-30 | Westinghouse Air Brake Co | Fluid compressor motor control apparatus |
US3046369A (en) * | 1959-04-27 | 1962-07-24 | Beatrice A Hicks | Device for sensing gas density |
Also Published As
Publication number | Publication date |
---|---|
GB633638A (en) | 1949-12-19 |
FR945660A (en) | 1949-05-11 |
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