US2509361A - Starter - Google Patents

Starter Download PDF

Info

Publication number
US2509361A
US2509361A US669725A US66972546A US2509361A US 2509361 A US2509361 A US 2509361A US 669725 A US669725 A US 669725A US 66972546 A US66972546 A US 66972546A US 2509361 A US2509361 A US 2509361A
Authority
US
United States
Prior art keywords
housing
casing
starter
engine
rotor
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.)
Expired - Lifetime
Application number
US669725A
Inventor
James R Mccreary
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
WAHLBERG MCCREARY
WAHLBERG-MCCREARY
Original Assignee
WAHLBERG MCCREARY
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by WAHLBERG MCCREARY filed Critical WAHLBERG MCCREARY
Priority to US669725A priority Critical patent/US2509361A/en
Application granted granted Critical
Publication of US2509361A publication Critical patent/US2509361A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02NSTARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N7/00Starting apparatus having fluid-driven auxiliary engines or apparatus
    • F02N7/08Starting apparatus having fluid-driven auxiliary engines or apparatus the engines being of rotary type
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/13Machine starters
    • Y10T74/131Automatic
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/13Machine starters
    • Y10T74/131Automatic
    • Y10T74/137Reduction gearing

Definitions

  • the device has to do with starters for heavy engines such as Diesel engines wherein a gas or airdriven turbine or rotor supplies the driving power for the starter.
  • a gas or airdriven turbine or rotor supplies the driving power for the starter.
  • gas under pressure is at hand, such as in oil field operations, i
  • This gas may be utilized.
  • An object of this invention is to provide a turbine type starter which may be readily installed.
  • Another object is to provide a turbine type starter wherein the rotor casing and drive connection housing may be independently rotated in installation.
  • a further object is to provide a gas turbine starter having a rotatably adjustable connection between the rotor casing and drive connection housing.
  • Still another object is to provide an engine starter in which the drive connection housing may be rotated to any selected position relative to the engine and the rotor casing in installation.
  • Fig. 1 is a sectional side elevation of a starter embodying this invention
  • Fig. 2 is a view taken along the line 2-2 in Fig. 1 in the direction 0! the arrows and rotated degrees in a clockwise direction
  • Fig. 3 is a side elevational view partially in section of a modified starter having a reduction gear assembly between the rotor and engine drive connection with part of the rotor broken away.
  • the numeral l0 designates a cylinder which constitutes a part of the rotor casing. Plates II and i2 bolted to opposite ends of cylinder l0 complete the casing. Cylinder III has two fittings lfla and Illb to receive the connections with the liner or cylinder [3 having ports l3a and l3b through which the power fluid passes.
  • the rotor it is mounted on a shaft l5 extending axially of the casing and journaled in the plates II and I2.
  • Radially extending vanes it are slidably mounted in radial grooves in the rotor. These blades ii are urged against the eccentric liner by centrifugal force. Impingement of the power fluid against the vanes or blades serves to actuate the starter.
  • the drive connection housing H Extending from plate I2 oi the rotor casing is the drive connection housing H.
  • the housing partially encases the drive connection comprising a sleeve l8 mounted for rotation on the extended end of shaft l5, gear l5 threaded to sleeve l8, ring 20 keyed to shaft l5, and a resilient connection between sleeve I8 and ring 20.
  • the resilient connection includes a spring 2
  • a rotatably adjustable joint is provided between the drive connection housing and casing. This joint is accomplished by meansof an element 22 having an internal flange. Element 22 has a central aperture which rotatably receives housing ll. Housing l1 has an outturned flange Ila which is received by an annular groove 23 between end plate l2 and element 22. Bolts 24 secure element 22 to plate 12 and when loosened provide independent rotation of either housing I! or casing III.
  • groove 23 is formed by machined portions in both element 22 and plate I2.
  • the groove could be formed by providing a countersunk portion of suiiicient depth in only one ening of bolts 24 causes the housing flange to be snugly held between the elements anchoring the housing 'against movement relative to the rotor casing.
  • a flange member 25 is provided on the housing.
  • the flange member has a central aperture for rotatably receiving the housing and a concentric series of apertures 25a to facilitate bolting of the flange to the engine.
  • the mounting of the flange on the housing is such that either may be rotated independently of the other to selected positions.
  • Set screw 28 is provided to secure the flange to the housing after proper adjustment has been made.
  • the starter may be assembled with housing l1 rotatably secured to the rotor casing.
  • the nose of housing I1 is inserted within the engine opening, not shown in the drawings, and the flange 25 is secured to the engine.
  • the rotor casing may be rotated independently of housing II or the engine or if preferred, the bolts 24 may be tightened and the rotor casing and drive connection housing may be rotated as a unit within flange 25.
  • the rotor casing is rotated into a selected position in which the power fluid connections, not shown in the drawings, may be most readily secured to fittings Ilia and lilb, respectively.
  • These fittings as shown in Fig. 2, have an opening through protruding ears of cylinder l whereby the connections may be fitted to either end and the unused end plugged.
  • the rotor casing cylinder 30 and engine drive connection housing are similar to those shown in Figs. 1 and 2.
  • the rotor casing and housing H are out of axial alignment to accommodate reduction gears between the end of shaft 3
  • These gears comprise the pinion 33 keyed to shaft 3
  • End plate 35 is adapted to receive the transmission housing 36 which is secured thereto by bolts 31.
  • a plurality of bolts 31 are used and housing 36 may be fastened to plate 35 in a plurality of positions.
  • Plate 35 may have separate bolts securing it to cylinder 30.
  • Housing 36 has a face portion 36a similar to the face of plate l2 and adapted to receive housing II in a similar fashion with the rotatably adjustable joint therebetween.
  • Flange 25 is mounted on housing l'l. This mounting as in Figs. 1. and 2 permits relative rotation therebetween until the set screw 26 is tightened.
  • the operation of this modification is similar to that of the device shown in Figs. 1 and 2.
  • the transmission housing may be adjusted and fastened to the rotor casing in a selected position.
  • the rotatably adjustable joint is provided between the transmission housing and housing I! which permits relative rotation therebetween.
  • Housing I! may be fastened to flange 25 in any selected position.
  • the arrangement is such that the rotor casing in installation may be placed in a selected position to facilitate connection of the device with power fluid fittings.
  • a gas driven starter for an engine having a casing with a rotor iournaled therein and a housing with an engine drive connection mounted casing and housing providing a plurality of in stallation positions therebetween.
  • a, flange member rotatably mounted on the housing and adaptedto be secured to the engine and means for anchoring the flange member to the housing whereby installation of the starter is facilitated.
  • a device as in claim -1 wherein the casing and housing are out of axial alignment.
  • a gas driven starter for an engine having a casing with a rotor journaled therein and a housing with an engine drive connection mounted therein, an element removably mounted on the casing to form an internal annular groove therebetween, an outturned flange on the housing extending into said groove, means to secure the flange in the groove against relative movement in a selected position and a flange member releasably securable to the housing in a selected position relative to the longitudinal axis of the housing and said flange mountable on-the engine. 4.
  • a gas turbine type starter for an engine having a casing with a rotor journaled therein.
  • a motor including a casing, a drive connection for the motor and housed within the casing adapted to operably engage a fly wheel of an internal combustion engine, said casing having a part adapted to extend through an engine housing, said casing part having an opening to provide for engagement of the drive connection with an engine fiy wheel, and a flange member releasably securable to the casi part therein, an adjustable connection between the at a selected rotational and axial position thereon UNITED STATES PATENTS whereby mounting of the starter upon the engine Number Name Date is facilitated- 2,075,119 Lansing- Mar. 30, 1937 McCREARY- 2,099,524 Klein Nov. 16, 1937 5 2,225,790 Nardone Dec. 24, 1940 REFERENCES CITED 2,358,445 Cone Sept. 19, 1944
  • the following references are of record in the 2,368,537 -Gi1bert Jan. 30, 1945 file or this Patent: 2,429,863 Wright Oct. 28, 1947

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydraulic Motors (AREA)

Description

Patented May 30, 1950 UNITED STATES PATENT OFFICE STARTER James B. McGreary, Houston, Tex., assignor to Wahlberg-MeCreary, Houston, Tex, a partnership composed of H. N. Wahlberg and J. B.
McCreary Application May 14, 1946, Serial No. 669,725
Claims. (Cl. 123-479) The device has to do with starters for heavy engines such as Diesel engines wherein a gas or airdriven turbine or rotor supplies the driving power for the starter. To drive the turbine compressed air may be used, or where gas under pressure is at hand, such as in oil field operations, i
this gas may be utilized.
In known starters of this type the casing for the rotor and the housing for the drive connection are either integral or are adapted to be anchored relative to one another in only a single position. Inasmuch as the starters may be used in connection with various styles and makes of engines diillculty is often encountered in installing the starters. Usually an elaborate set of pipe connections must be resorted to in order to connect the power fluid inlet and outlet connections with the corresponding connections of the rotor casing. These pipe connections are expensive, time consuming and cumbersome. 0ften, in certain installations, the engine mounting is such that only a confined space is available for the starter in which case the problem is more serious.
An object of this invention is to provide a turbine type starter which may be readily installed.
Another object is to provide a turbine type starter wherein the rotor casing and drive connection housing may be independently rotated in installation.
A further object is to provide a gas turbine starter having a rotatably adjustable connection between the rotor casing and drive connection housing.
Still another object is to provide an engine starter in which the drive connection housing may be rotated to any selected position relative to the engine and the rotor casing in installation. Other and further objects will be apparent from the following description.
In the accompanying drawings which form a-' part of the instant specification and are to be read in conjunction therewith and in which like reference numerals are used to indicate like parts in the various views,
Fig. 1 is a sectional side elevation of a starter embodying this invention;
Fig. 2 is a view taken along the line 2-2 in Fig. 1 in the direction 0! the arrows and rotated degrees in a clockwise direction and Fig. 3 is a side elevational view partially in section of a modified starter having a reduction gear assembly between the rotor and engine drive connection with part of the rotor broken away.
Referring to the drawings and more particularly to the modification shown in Figs. 1 and 2, the numeral l0 designates a cylinder which constitutes a part of the rotor casing. Plates II and i2 bolted to opposite ends of cylinder l0 complete the casing. Cylinder III has two fittings lfla and Illb to receive the connections with the liner or cylinder [3 having ports l3a and l3b through which the power fluid passes. The rotor it is mounted on a shaft l5 extending axially of the casing and journaled in the plates II and I2. Radially extending vanes it are slidably mounted in radial grooves in the rotor. These blades ii are urged against the eccentric liner by centrifugal force. Impingement of the power fluid against the vanes or blades serves to actuate the starter.
Extending from plate I2 oi the rotor casing is the drive connection housing H. The housing partially encases the drive connection comprising a sleeve l8 mounted for rotation on the extended end of shaft l5, gear l5 threaded to sleeve l8, ring 20 keyed to shaft l5, and a resilient connection between sleeve I8 and ring 20. The resilient connection includes a spring 2| mounted between stops carried by sleeve [8 and ring 20.
A rotatably adjustable joint is provided between the drive connection housing and casing. This joint is accomplished by meansof an element 22 having an internal flange. Element 22 has a central aperture which rotatably receives housing ll. Housing l1 has an outturned flange Ila which is received by an annular groove 23 between end plate l2 and element 22. Bolts 24 secure element 22 to plate 12 and when loosened provide independent rotation of either housing I! or casing III.
In the modification shown, groove 23 is formed by machined portions in both element 22 and plate I2. However, it is to be understood that the groove could be formed by providing a countersunk portion of suiiicient depth in only one ening of bolts 24 causes the housing flange to be snugly held between the elements anchoring the housing 'against movement relative to the rotor casing.
In order to secure the starter to an engine a flange member 25 is provided on the housing. The flange member has a central aperture for rotatably receiving the housing and a concentric series of apertures 25a to facilitate bolting of the flange to the engine. The mounting of the flange on the housing is such that either may be rotated independently of the other to selected positions. Set screw 28 is provided to secure the flange to the housing after proper adjustment has been made.
It is believed that the operation of this invention is obvious from the foregoing description. The starter may be assembled with housing l1 rotatably secured to the rotor casing. The nose of housing I1 is inserted within the engine opening, not shown in the drawings, and the flange 25 is secured to the engine. In this condition the rotor casing may be rotated independently of housing II or the engine or if preferred, the bolts 24 may be tightened and the rotor casing and drive connection housing may be rotated as a unit within flange 25. In any event, the rotor casing is rotated into a selected position in which the power fluid connections, not shown in the drawings, may be most readily secured to fittings Ilia and lilb, respectively. These fittings, as shown in Fig. 2, have an opening through protruding ears of cylinder l whereby the connections may be fitted to either end and the unused end plugged.
When the power fluid connections have been made set screw 26 and bolts 24, or either of them as the case may be, are tightened to complete the installation.
In the modification shown in Fig. 3, the rotor casing cylinder 30 and engine drive connection housing are similar to those shown in Figs. 1 and 2. However, the rotor casing and housing H are out of axial alignment to accommodate reduction gears between the end of shaft 3| extending from the rotor casing and the comple- -mentary end of shaft 32 on which the drive connection sleeve and ring are mounted. These gears comprise the pinion 33 keyed to shaft 3| and gear 34 keyed to shaft 32 and meshing with the pinion.
End plate 35 is adapted to receive the transmission housing 36 which is secured thereto by bolts 31. A plurality of bolts 31 are used and housing 36 may be fastened to plate 35 in a plurality of positions. Plate 35 may have separate bolts securing it to cylinder 30. Housing 36 has a face portion 36a similar to the face of plate l2 and adapted to receive housing II in a similar fashion with the rotatably adjustable joint therebetween. Flange 25 is mounted on housing l'l. This mounting as in Figs. 1. and 2 permits relative rotation therebetween until the set screw 26 is tightened.
The operation of this modification is similar to that of the device shown in Figs. 1 and 2. The transmission housing may be adjusted and fastened to the rotor casing in a selected position. The rotatably adjustable joint is provided between the transmission housing and housing I! which permits relative rotation therebetween. Housing I! may be fastened to flange 25 in any selected position. Thus, in installing the starter 4 inanenginathestarterisplacedinapositionto facilitate connection of its inlet and outlet ports Ilia and lb with the power fluid connections.
It will be seen that the objects of this invention have been accomplished. The arrangement is such that the rotor casing in installation may be placed in a selected position to facilitate connection of the device with power fluid fittings.
There has been provided a turbine type starter which, with the necessary pipe fittings, will occupy a minimum of space when installed. The
construction is such that the rotor casing and drive connection housing may be rotated independently in installation.
It will be understood that certain features and subcombinations are of utility and may be employed without reference to other features and subcombinations. This is contemplated by and is within the scope of the claims.
As many ossible embodiments may be made of the invention without departing from the scope thereof 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 described my invention, I claim: 1. In a gas driven starter for an engine having a casing with a rotor iournaled therein and a housing with an engine drive connection mounted casing and housing providing a plurality of in stallation positions therebetween. a, flange member rotatably mounted on the housing and adaptedto be secured to the engine and means for anchoring the flange member to the housing whereby installation of the starter is facilitated. 2. A device as in claim -1 wherein the casing and housing are out of axial alignment.
3. In a gas driven starter for an engine having a casing with a rotor journaled therein and a housing with an engine drive connection mounted therein, an element removably mounted on the casing to form an internal annular groove therebetween, an outturned flange on the housing extending into said groove, means to secure the flange in the groove against relative movement in a selected position and a flange member releasably securable to the housing in a selected position relative to the longitudinal axis of the housing and said flange mountable on-the engine. 4. In a gas turbine type starter for an engine having a casing with a rotor journaled therein. a housing with an engine drive connection mounted therein, a transmission gear housing between the casing and drive connection housing, meshing gears therein operably connecting the rotor and drive mechanism, the mountings of the casing and drive connection housing on the transmission housing providing for independent rota- .m tion of the casing and transmission housing about the longitudinal axis of the drive connection housing and means for securing the housing in a selected position along its longitudinal axis to the engine whereby installation of the starter is 4;; facilitated.
5. In a starter for an internal combustion engine, a motor including a casing, a drive connection for the motor and housed within the casing adapted to operably engage a fly wheel of an internal combustion engine, said casing having a part adapted to extend through an engine housing, said casing part having an opening to provide for engagement of the drive connection with an engine fiy wheel, and a flange member releasably securable to the casi part therein, an adjustable connection between the at a selected rotational and axial position thereon UNITED STATES PATENTS whereby mounting of the starter upon the engine Number Name Date is facilitated- 2,075,119 Lansing- Mar. 30, 1937 McCREARY- 2,099,524 Klein Nov. 16, 1937 5 2,225,790 Nardone Dec. 24, 1940 REFERENCES CITED 2,358,445 Cone Sept. 19, 1944 The following references are of record in the 2,368,537 -Gi1bert Jan. 30, 1945 file or this Patent: 2,429,863 Wright Oct. 28, 1947
US669725A 1946-05-14 1946-05-14 Starter Expired - Lifetime US2509361A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US669725A US2509361A (en) 1946-05-14 1946-05-14 Starter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US669725A US2509361A (en) 1946-05-14 1946-05-14 Starter

Publications (1)

Publication Number Publication Date
US2509361A true US2509361A (en) 1950-05-30

Family

ID=24687472

Family Applications (1)

Application Number Title Priority Date Filing Date
US669725A Expired - Lifetime US2509361A (en) 1946-05-14 1946-05-14 Starter

Country Status (1)

Country Link
US (1) US2509361A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2998729A (en) * 1960-08-08 1961-09-05 Arthur J Warsaw Engine starting apparatus
US3020771A (en) * 1959-07-30 1962-02-13 Gen Motors Corp Engine starter
US3021715A (en) * 1962-02-20 Motor vehicle engine starting apparatus
US3459165A (en) * 1967-08-22 1969-08-05 Olin Mathieson Diesel engine starter
JPS51129938U (en) * 1975-04-10 1976-10-20
US6026695A (en) * 1998-06-16 2000-02-22 Ingersoll-Rand Company Engine starter housing and an annular housing extension therefor

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2075119A (en) * 1935-08-20 1937-03-30 Eclipse Aviat Corp Engine starting mechanism
US2099524A (en) * 1934-05-07 1937-11-16 Bosch Robert Starter for internal combustion engines
US2225790A (en) * 1939-02-15 1940-12-24 Bendix Aviat Corp Engine starting mechanism
US2358445A (en) * 1943-04-05 1944-09-19 Mid Continent Supply Company Engine starter and actuating mechanism therefor
US2368537A (en) * 1943-02-08 1945-01-30 Bendix Aviat Corp Power plant accessory
US2429863A (en) * 1943-08-11 1947-10-28 Breeze Corp Engine starter

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2099524A (en) * 1934-05-07 1937-11-16 Bosch Robert Starter for internal combustion engines
US2075119A (en) * 1935-08-20 1937-03-30 Eclipse Aviat Corp Engine starting mechanism
US2225790A (en) * 1939-02-15 1940-12-24 Bendix Aviat Corp Engine starting mechanism
US2368537A (en) * 1943-02-08 1945-01-30 Bendix Aviat Corp Power plant accessory
US2358445A (en) * 1943-04-05 1944-09-19 Mid Continent Supply Company Engine starter and actuating mechanism therefor
US2429863A (en) * 1943-08-11 1947-10-28 Breeze Corp Engine starter

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3021715A (en) * 1962-02-20 Motor vehicle engine starting apparatus
US3020771A (en) * 1959-07-30 1962-02-13 Gen Motors Corp Engine starter
US2998729A (en) * 1960-08-08 1961-09-05 Arthur J Warsaw Engine starting apparatus
US3459165A (en) * 1967-08-22 1969-08-05 Olin Mathieson Diesel engine starter
JPS51129938U (en) * 1975-04-10 1976-10-20
JPS5545891Y2 (en) * 1975-04-10 1980-10-28
US6026695A (en) * 1998-06-16 2000-02-22 Ingersoll-Rand Company Engine starter housing and an annular housing extension therefor

Similar Documents

Publication Publication Date Title
US6851255B2 (en) Normally open reverse flow flapper valve
US2309683A (en) Pumping unit
US2250448A (en) Shaft coupling
US2509361A (en) Starter
WO1989011583A1 (en) Turbocharger apparatus
US3130953A (en) carpenter
US4274292A (en) Compact starter assembly
SU670238A3 (en) Internal combustion engine
CZ292057B6 (en) Device for attaching a detail onto a rotary shaft
US2381834A (en) Centrifugal pump for liquid
US2491100A (en) Pump
US4066048A (en) Universal axial spacer for mounting fan on pump shaft and drive pulley
GB2467202A (en) Selective rotation arrangement for a gas turbine shaft
US5220844A (en) Infinite position mounting flange
US4530313A (en) Drive arrangement of an auxiliary device in an internal combustion engine
US2636667A (en) Pump
US2358445A (en) Engine starter and actuating mechanism therefor
US3143078A (en) Well pump
GB2269429A (en) A clutch arrangement
US2666395A (en) Rotary pump adapted to be supported and actuated by a power take-off shaft of a motor
US2103180A (en) Rotary motor
RU196296U1 (en) Borehole Filter with Adjustable Clearance
CN111197549B (en) Water flow power generation device
CN109555602B (en) Oil return system of transmission box
US1730220A (en) Combined engine starter and driving means for mechanisms