US2366121A - Electrically controlled fluidpressure operated motor - Google Patents

Electrically controlled fluidpressure operated motor Download PDF

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US2366121A
US2366121A US48056443A US2366121A US 2366121 A US2366121 A US 2366121A US 48056443 A US48056443 A US 48056443A US 2366121 A US2366121 A US 2366121A
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housing
pressure
armature
motor
cylinder
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Martin-Hurst William F Forrest
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B17/00Reciprocating-piston machines or engines characterised by use of uniflow principle
    • F01B17/02Engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B17/00Reciprocating-piston machines or engines characterised by use of uniflow principle
    • 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
    • Y10T137/00Fluid handling
    • Y10T137/8593Systems
    • Y10T137/87169Supply and exhaust
    • Y10T137/87193Pilot-actuated
    • Y10T137/87209Electric

Definitions

  • This invention relates to electrically-controlled, fluid-pressure operated motors such as are used for operating control members on aircraft and the like, the invention having particular but not exclusive application to electrically-controlled pneumatic or hydraulic motors used for actuating a two-speed supercharger control gear under control of a manual or a barometric, thermostatic or other automatic switch.
  • the object of the invention is to provide an improved and compact form of motor which will function eiciently under all operating conditions.
  • the improved motor comprises a spring-controlled telescopic housing, a plunger movable within a pressure cylinder and coupled to one of the telescopic housing members, means for supplying pressure fluid to one end of said cylinder to extend or collapse the housing against the action of the spring, and electromagnetically operated valve means for controlling the supply and release of pressure uid to the said pressure cylinder.
  • Fig. 1 is a longitudinal sectional elevation through an electro-pneumatic motor with the housing held in the collapsed position
  • Fig. 2 is a View similar to Fig, V1 but showing the housing held in the extended position
  • Fig. 3 is a view similar to Fig. 1 but showing an electro-hydraulic housing and Fig. 4 is a. fragmentary view showing the valve mechanism of Fig. 3 in the position to set and hold the housing in the extended position.
  • a main body I formed at one side with a tubular, screw-threaded extension 2 upon which is mounted the outer member 3 of a telescopic housing,I the inner member 4 of said housing being mounted to slide in the member'3 and being closed at its end remote from the body I by a cap 5.
  • a pressure cylinder 6 mounted coaxially within the housing member 3 is a pressure cylinder 6, a plunger 1 working in said cylinder being carried by a rod 8 which extends of the cylinder 6 having a vent I3xi communicating with the atmosphere.
  • the cap 5 is formed with a shoulder 5a which bears against the swivel I0 and a compression spring I4 surrounding the casing II normally urges the housing to the extended position, the said spring bearing at one end against a sleeve I5 securing the casing lI to the extension 2 and at the other end 'against a. ring I6 which bears against the cap 5 through the intermediary of a thrust bearing I1.
  • the provision of the bearing I1 enables the inner housing member 4 together with the swivel to be rotated to any desired position for convenient attachment to the member to be controlled.
  • a screw-threaded recess I8 adapted to receive a tubular member I9 which extends within a solenoid 20, the latter being enclosed by a housing 2l bolted to the main body I.
  • armature 22 mounted for axial movement within the tubular member I9 is an armature 22 which is urged to the right by a spiral spring 23 interposed between a shoulder on the member I9 and a iiange on the end of the armature, and is moved to the left against the action of the spring by the action of the solenoid.
  • the end of the casing 2I remote from the body I is closed by a cover plate 24 provided with a hollow extension 25, the said extension being pivotally mounted in a yoke 26 which in turn is carried by a pivot pin 21 mounted in a supporting bracket 28 whereby the motor can be swung to any angular position relative to the bracket;
  • the cover plate 24 also supports a core member 29 arranged coaxial with the armature 22 and threaded to receive a detachable plug 39 having an axial bore 3I, the end of the plug adjacent the armature being formed to provide a valve seating 32.
  • a pressure fluid 34 from which a lateral passage 35 leads to a chamber 36 formed in the end of the tubular member I9.
  • a further passage 31 connects the chamber 36 with an annular chamber 38 in communication with the annular passage I2.
  • the armature is provided at its ends with valve elements 39, 48 respectively, said valve elements consisting each of a disc of rubber or similar resilient material recessed into the respective end walls of the armature, the valve 39 cooperating with the seating 32 whilst the valve 40 cooperates with a seating 4I formed at the outlet of the lateral passage 35.
  • the main body Ia is provided with pressure fluid inlet and outletv connections 44, 45 respectively and has a central bore 46 adapted to receive a ported sleeve 41.
  • a passage 48 leads from the bore 46 to the inlet connection and a I second passage 49 leads from the said bore to the annular chamber 38.
  • a third passage 50 leads from the outlet connection to a chamber 5I into which, the end 0f the sleeve 41 projects.
  • sleeve 41- is provided with three radial ports 52, 53, 54 which communicate with the passages 48, 49 and chamber 5I respectively.
  • a ⁇ valve member 55' mounted to slide within the sleeve 41 and having a close t therein is a ⁇ valve member 55'provided with a peripheral groove 56 whichis adapted to conneet the ports 52 and 53 or 53 and 54 as will be more fully explained hereafter.
  • the valve member is actuated by the armature 22, to which it is attached by a exible blade 51, and is urged to the right byl a spiral spring 58 bearing against a collar 59 fast on said valve member.
  • the armature and valve member are moved to the left, the movement being limited by the engagement of the armature with a core plug 60- In this position, shown in Fig. 3, the groove 56 connects the ports 52,- 53 so that high presure liquid in lpassage 48 can passinto passage 49 and then through anuular chamber 38, annular passage I2 and ports I3 to the interior of pressure cylinder 6. In this manner the housing is moved to and held in the collapsed position.
  • the spiral spring 58 returns the valve member 55 to the position shown in Fig. 4 where the port 52 is covered and ports -53 vand 54 are connected by the groove 56 in the valve member.
  • the spring I4 extends the housing, the liquid in the cylinder being exhausted via ports I3, annular passage I2, annular chamber 38, passage 49, port 53, groove 56 and port 54 to chamberBI from which it flows to the outlet 45 through passage 50.
  • inlet and outlet connections 4 4. 45 have been shown at diametrically opposed points on the main body Ia but it will be understood that they may be arranged at a closer angular disposition, for example at 90, for convenience in attaching pipe lines which are led in the same direction.
  • the motor is employed to actuate a twospeed supercharger control gear for an aircraft engine and is under control of an altitude operated switch
  • the invention provides a simple and compact form of motor capable of application to many forms of control gear and which, having relatively few moving parts, can
  • a fluid pressure operated motor including-a main body, a motor cylinder supported at one end by said body, a plunger mounted to reciprocate in said cylinder, a rod carrying said plunger, a telescopic housing comprising members enclosing said cylinder, onev member of said housing being mounted on one side of said body and another member thereof being movable and carried by the plunger rod,Y a casing enclosing the motor cylinder and providing an annular, axially extending Vpassage through which pressure iluid is ledto the outer end 0f the cylinder to move the plunger towards the inner end of the motor cylinder, spring means mounted externally of the motor cylinder and enclosing casing and urging the plunger towards the outer end of the cylinder, a pressure fluid inlet connection on said main body, an exhaust port, an axially movable valve member, communications controlled by said valve member being provided between said pressure iluid inlet and the exhaust port and said annular passage, and an electromagnetic device for actuating said valve member,
  • said spring means consists of a ⁇ helical compression spring surrounding the motor casing, one end of said spring bearing directly against said main body, and including a member connecting the movable member of the telescopic housing to the plunger rod, and a, thrust vrace through the intermediary of which the other end of said spring bears against said connecting member.
  • a fluid pressure operated motor as claimed in claim l wherein said electromagnetic device comprises a solenoid and an axially movable ar- -mature therefore, and including a chamber coma bore leading to said exhaust port, and a seat ⁇ ⁇ controlling said bore, said armature being movable to one extreme position to engage one end thereof with the seat on the core plug and thereby close the exhaust port and establish communication between said chamber and pressure fluid inlet, and movabletothe other extreme position to engage the other end thereof with the seat on the wall of said chamber to cut oil communication between said chamber and pressure fluid inlet and establish communication between said chamber and exhaust port.
  • a fluid pressure operated motor comprising a main body, a two-part telescopic housing mounted at one end on one side of said body, spring means urging the housing to the extended position, a pressure cylinder mounted coaxially within the housing and having a plunger movable therein and connected to the movable housing member, a casing enclosing the pressure cylinder andl providing an annular passage through which pressure fluid is led to the outer end of the cylinder to collapse the housing, pressure Iiuid inlet and outlet connections on said main body, a ported sleeve mounted in the main body and having ports therein, and passages for connecting said ports to the said pressure fluid inlet and outlet connections and said annular passage respectively, a solenoid mounted on said main body'on the side thereof opposite to that at which said housing is mounted and having an armature movable axially therein, a valve member movable in said ported sleeve and connected to said armature, and a springV urging said valve member to one extreme position in

Description

DeC- 26, 1944. w. F. F. MARTIN-HURST 2,365,121
ELECTRI CALLY- CONTROLLED FLUID- PRES SURE OPERATED MOTOR Filed March 25, 1943 2 Sheets-Sheet l .mw @im l @m4 f Am. www @wmv k,
Dec- 26, 1944- w. F. F. MARTIN-HuRsT 2,366,121
ELECTRICALLY-CONTROLLED FLUID-PRESSURE OPERATED MOTOR Filed March 25, 1945 2 Sheets-Sheet 2 Inventor MTWrPMMJ/M ltorney S Patented Dec. 26, 1944 UNITED ELECTRICALLY CONTROLLED FLUID- PRESSURE OPERATED MOTOR William Frederick Forrest Martin-Hurst, Sunbury-on-Thames, England Application March 25, 1943, Serial No. 480,564 In Great Britain October 16, 1942 7 Claims.
This invention relates to electrically-controlled, fluid-pressure operated motors such as are used for operating control members on aircraft and the like, the invention having particular but not exclusive application to electrically-controlled pneumatic or hydraulic motors used for actuating a two-speed supercharger control gear under control of a manual or a barometric, thermostatic or other automatic switch.
The object of the invention is to provide an improved and compact form of motor which will function eiciently under all operating conditions.
According to the invention the improved motor comprises a spring-controlled telescopic housing, a plunger movable within a pressure cylinder and coupled to one of the telescopic housing members, means for supplying pressure fluid to one end of said cylinder to extend or collapse the housing against the action of the spring, and electromagnetically operated valve means for controlling the supply and release of pressure uid to the said pressure cylinder.
Reference will now be made to the accompanying drawings which illustrate by way of example two embodiments of the invention and wherein Fig. 1 is a longitudinal sectional elevation through an electro-pneumatic motor with the housing held in the collapsed position,
Fig. 2 is a View similar to Fig, V1 but showing the housing held in the extended position,
Fig. 3 is a view similar to Fig. 1 but showing an electro-hydraulic housing and Fig. 4 is a. fragmentary view showing the valve mechanism of Fig. 3 in the position to set and hold the housing in the extended position.
Referring rlrst to the construction shown in Figs. 1 and 2, there is provided a main body I formed at one side with a tubular, screw-threaded extension 2 upon which is mounted the outer member 3 of a telescopic housing,I the inner member 4 of said housing being mounted to slide in the member'3 and being closed at its end remote from the body I by a cap 5. Mounted coaxially within the housing member 3 is a pressure cylinder 6, a plunger 1 working in said cylinder being carried by a rod 8 which extends of the cylinder 6 having a vent I3xi communicating with the atmosphere. The cap 5 is formed with a shoulder 5a which bears against the swivel I0 and a compression spring I4 surrounding the casing II normally urges the housing to the extended position, the said spring bearing at one end against a sleeve I5 securing the casing lI to the extension 2 and at the other end 'against a. ring I6 which bears against the cap 5 through the intermediary of a thrust bearing I1. The provision of the bearing I1 enables the inner housing member 4 together with the swivel to be rotated to any desired position for convenient attachment to the member to be controlled.
On the side of the body I opposite to that at which the motor is mounted there is provided a screw-threaded recess I8 adapted to receive a tubular member I9 which extends within a solenoid 20, the latter being enclosed by a housing 2l bolted to the main body I. Mounted for axial movement within the tubular member I9 is an armature 22 which is urged to the right by a spiral spring 23 interposed between a shoulder on the member I9 and a iiange on the end of the armature, and is moved to the left against the action of the spring by the action of the solenoid. The end of the casing 2I remote from the body I is closed by a cover plate 24 provided with a hollow extension 25, the said extension being pivotally mounted in a yoke 26 which in turn is carried by a pivot pin 21 mounted in a supporting bracket 28 whereby the motor can be swung to any angular position relative to the bracket; The cover plate 24 also supports a core member 29 arranged coaxial with the armature 22 and threaded to receive a detachable plug 39 having an axial bore 3I, the end of the plug adjacent the armature being formed to provide a valve seating 32.
Mounted in the main body I is a pressure fluid 34 from which a lateral passage 35 leads to a chamber 36 formed in the end of the tubular member I9. A further passage 31 connects the chamber 36 with an annular chamber 38 in communication with the annular passage I2. The armature is provided at its ends with valve elements 39, 48 respectively, said valve elements consisting each of a disc of rubber or similar resilient material recessed into the respective end walls of the armature, the valve 39 cooperating with the seating 32 whilst the valve 40 cooperates with a seating 4I formed at the outlet of the lateral passage 35.`
nular passage I2- and ports I3 to-the-interior' of cylinder 6 where, acting upon the rear side vof and holds it in thev retracted position. vWhen the solenoid is de-energised, the spring 23 moves the armature t the right hand position (see Fig. 2), opening valve 39, 32 and closing valve 48, 4I. Supply of compressed air is thus out off and the housing is moved to the fully extended position by the spring I4. During this outward movement;` of the plunger assembly, the air in the cylinder is exhausted through ports I3, an-
, nular passage I2, annular chamber 38, passage the plunger, it moves the plunger assembly to 31, chamber 36, the spaces between the armature and the tubular body I9, and passage 3l, the air finally escaping to atmosphere through Van aperture 42 formed in a cover 43 closing the end of the tubular extension 25.
Referring now to the embodiment; illustrated in Figs. 3 and 4 in which the motor is hydraulically operated, the telescopic housing, the solenoid and its housing and the motor supporting means are all constructed as in the form previously described and the component parts there'- of are indicated by like reference numerals. In this form, the main body Ia is provided with pressure fluid inlet and outletv connections 44, 45 respectively and has a central bore 46 adapted to receive a ported sleeve 41. A passage 48 leads from the bore 46 to the inlet connection and a I second passage 49 leads from the said bore to the annular chamber 38. A third passage 50 leads from the outlet connection to a chamber 5I into which, the end 0f the sleeve 41 projects. 'I'he sleeve 41-is provided with three radial ports 52, 53, 54 which communicate with the passages 48, 49 and chamber 5I respectively. Mounted to slide within the sleeve 41 and having a close t therein is a `valve member 55'provided with a peripheral groove 56 whichis adapted to conneet the ports 52 and 53 or 53 and 54 as will be more fully explained hereafter. The valve member is actuated by the armature 22, to which it is attached by a exible blade 51, and is urged to the right byl a spiral spring 58 bearing against a collar 59 fast on said valve member.
When the solenoid is energised, the armature and valve member are moved to the left, the movement being limited by the engagement of the armature with a core plug 60- In this position, shown in Fig. 3, the groove 56 connects the ports 52,- 53 so that high presure liquid in lpassage 48 can passinto passage 49 and then through anuular chamber 38, annular passage I2 and ports I3 to the interior of pressure cylinder 6. In this manner the housing is moved to and held in the collapsed position. When the solenoid is de-energised, the spiral spring 58 returns the valve member 55 to the position shown in Fig. 4 where the port 52 is covered and ports -53 vand 54 are connected by the groove 56 in the valve member. 'I'he pressure being thus cut oiI, the spring I4 extends the housing, the liquid in the cylinder being exhausted via ports I3, annular passage I2, annular chamber 38, passage 49, port 53, groove 56 and port 54 to chamberBI from which it flows to the outlet 45 through passage 50.
For illustrative purposes, the inlet and outlet connections 4 4. 45 have been shown at diametrically opposed points on the main body Ia but it will be understood that they may be arranged at a closer angular disposition, for example at 90, for convenience in attaching pipe lines which are led in the same direction.
Where the motor is employed to actuate a twospeed supercharger control gear for an aircraft engine and is under control of an altitude operated switch, it is preferred to so mount the motor that the housing is extended when holding the control gear in the position corresponding to the lower speed. In this manner, failure of the electric or fluid pressure supply leaves the supercharger operating at the lower speed and thus avoids the possibility of causing damage to the engine by excessive supercharging at low altitudes.
It will be seen that the invention provides a simple and compact form of motor capable of application to many forms of control gear and which, having relatively few moving parts, can
' be installed and maintained with the minimum of skilled attention.
I claim:
1. A fluid pressure operated motor including-a main body, a motor cylinder supported at one end by said body, a plunger mounted to reciprocate in said cylinder, a rod carrying said plunger, a telescopic housing comprising members enclosing said cylinder, onev member of said housing being mounted on one side of said body and another member thereof being movable and carried by the plunger rod,Y a casing enclosing the motor cylinder and providing an annular, axially extending Vpassage through which pressure iluid is ledto the outer end 0f the cylinder to move the plunger towards the inner end of the motor cylinder, spring means mounted externally of the motor cylinder and enclosing casing and urging the plunger towards the outer end of the cylinder, a pressure fluid inlet connection on said main body, an exhaust port, an axially movable valve member, communications controlled by said valve member being provided between said pressure iluid inlet and the exhaust port and said annular passage, and an electromagnetic device for actuating said valve member, said electromagnetic device being also carried by the main body and being mounted on the side thereof opposite to that at which the motor cylinder is supported.
2. A fluid pressure operated motor as claimed in claim 1, wherein said spring means consists of a `helical compression spring surrounding the motor casing, one end of said spring bearing directly against said main body, and including a member connecting the movable member of the telescopic housing to the plunger rod, and a, thrust vrace through the intermediary of which the other end of said spring bears against said connecting member.
3. A fluid pressure operated motor as claimed in claim l, wherein said electromagnetic device comprises a solenoid and an axially movable ar- -mature therefore, and including a chamber coma bore leading to said exhaust port, and a seat` `controlling said bore, said armature being movable to one extreme position to engage one end thereof with the seat on the core plug and thereby close the exhaust port and establish communication between said chamber and pressure fluid inlet, and movabletothe other extreme position to engage the other end thereof with the seat on the wall of said chamber to cut oil communication between said chamber and pressure fluid inlet and establish communication between said chamber and exhaust port.
4. A fluid pressure operated motor as claimed in claim 1, wherein said electromagnetic device comprises a solenoid and an axially movable armature, and said valve memberis connected to said armature for movement therewith, and including aported sleeve mounted in said main body and having pOrtscommunicating with said pressure uid inlet, annular passage and exhaust port respectively, said valve member being mounted to slide in said sleeve and formed with a peripheral groove which cooperates with the DOrts in said sleeve to establish communication between the pressure fluid inlet and annular passage and close the exhaust port while the valve member is in one extreme position, and to close the pressure fluid inlet and establish communication between said annular passage and the exhaust port while the valve member is in the other extreme position.`
5. A fluid pressure operated motor as claimed in claim 1, wherein said electromagnetic device comprises a solenoid and an axially movable armature, and including a spring urging the armature to a position to close the pressure uuid inlet and establish communication between said annular passage and exhaust port, and wherein said armature is moved by the solenoid to a position to close the exhaust port and establish pressure fluid is led to the outer end of the cylinder to collapse the housing, a pressure uid inlet on said mainbody, an exhaust port, a solenoid mounted on the main body on the side thereof opposite ,to that on which the housing is mounted and having an armature movable axially therein, and two valve elements carried by the armature and cooperating with xed valve seats communicating respectively with the pressure fiuid inlet and exhaust port, and a spring urging said armature to one extreme position in which one of said valve elements engages the respective valve seat to close the pressureV fluid inlet connection with said annular passage and to connect said passage to atmosphere through the exhaust port, said armature being moved by the4 solenoid to the other extreme position in which the other valve element engages the other seat to close the exhaust port connection with said annular passage and to establish communication between said annular passage and the pressure fluid inlet.
7. A fluid pressure operated motor comprising a main body, a two-part telescopic housing mounted at one end on one side of said body, spring means urging the housing to the extended position, a pressure cylinder mounted coaxially within the housing and having a plunger movable therein and connected to the movable housing member, a casing enclosing the pressure cylinder andl providing an annular passage through which pressure fluid is led to the outer end of the cylinder to collapse the housing, pressure Iiuid inlet and outlet connections on said main body, a ported sleeve mounted in the main body and having ports therein, and passages for connecting said ports to the said pressure fluid inlet and outlet connections and said annular passage respectively, a solenoid mounted on said main body'on the side thereof opposite to that at which said housing is mounted and having an armature movable axially therein, a valve member movable in said ported sleeve and connected to said armature, and a springV urging said valve member to one extreme position in which it shuts oil communication between said fluid inlet and annular passage and establishes communication between said annular passage and the fluid outlet connection, and said valve member being moved by the solenoid to the other extreme position in which it closes communication between said annular passage and the fluid outlet connection and establishes communication between said annular passage and the pressure fluid inlet connection.`
WILLIAM FREDERICK FORREST MARTIN-HURST.
US48056443 1942-10-16 1943-03-25 Electrically controlled fluidpressure operated motor Expired - Lifetime US2366121A (en)

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Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447355A (en) * 1945-01-26 1948-08-17 Louis H Morin Die-casting machine
US2497489A (en) * 1946-01-03 1950-02-14 United Aircraft Corp Hydraulic strut
US2533953A (en) * 1947-09-08 1950-12-12 Vilbiss Co Spray gun
US2556531A (en) * 1949-08-20 1951-06-12 Globe Oil Tools Co Mechanism for the control and operation of a gate
US2586683A (en) * 1947-09-08 1952-02-19 Detroit Harvester Co Solenoid valve assembly
US2604639A (en) * 1950-01-18 1952-07-29 Jack L Killifer Hydraulic hospital bed lift
US2612140A (en) * 1946-05-04 1952-09-30 Leonidas C Miller Fluid driven actuator for tools
US2635583A (en) * 1949-10-21 1953-04-21 Robert O Bill Pressure fluid motor and combined telescopic guide and housing therefor
US2662635A (en) * 1949-05-24 1953-12-15 Joy Mfg Co Materials handling apparatus
US2663285A (en) * 1949-04-23 1953-12-22 Mason Lifting apparatus
US2667173A (en) * 1946-11-26 1954-01-26 Int Cigar Mach Co Cigar machine
US2714505A (en) * 1948-05-01 1955-08-02 Joy Mfg Co Apparatus for mine roof control
US2761425A (en) * 1952-06-17 1956-09-04 Gen Motors Corp Reciprocatory fluid actuated device
US2766673A (en) * 1951-09-29 1956-10-16 Ferguson Harry Inc Adjusting mechanism for agricultural implement parts
US2814872A (en) * 1955-07-05 1957-12-03 William A Gerrans Fluid actuated tool
US2896583A (en) * 1956-12-28 1959-07-28 Jarvis A Stixrood Counterbalancing hydraulic cylinder
US2914034A (en) * 1956-07-06 1959-11-24 Logansport Machine Co Inc Vacuum control valve
US2982256A (en) * 1954-04-13 1961-05-02 Littlefield Eflie Dora Jones Electrical apparatus and methods
US2987049A (en) * 1957-03-29 1961-06-06 Dura Corp Cylinder and valve assembly
US3375760A (en) * 1966-07-26 1968-04-02 John F. Taplin Rolling diaphragm device having springbiased piston and means for precluding transmission of spring-windup to piston
US3415487A (en) * 1966-05-16 1968-12-10 North American Plastics Magnetic control valve with concentric coils
WO1987002642A1 (en) * 1985-10-31 1987-05-07 Sundstrand Corporation Deployment-retraction apparatus for aircraft turbines

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447355A (en) * 1945-01-26 1948-08-17 Louis H Morin Die-casting machine
US2497489A (en) * 1946-01-03 1950-02-14 United Aircraft Corp Hydraulic strut
US2612140A (en) * 1946-05-04 1952-09-30 Leonidas C Miller Fluid driven actuator for tools
US2667173A (en) * 1946-11-26 1954-01-26 Int Cigar Mach Co Cigar machine
US2533953A (en) * 1947-09-08 1950-12-12 Vilbiss Co Spray gun
US2586683A (en) * 1947-09-08 1952-02-19 Detroit Harvester Co Solenoid valve assembly
US2714505A (en) * 1948-05-01 1955-08-02 Joy Mfg Co Apparatus for mine roof control
US2663285A (en) * 1949-04-23 1953-12-22 Mason Lifting apparatus
US2662635A (en) * 1949-05-24 1953-12-15 Joy Mfg Co Materials handling apparatus
US2556531A (en) * 1949-08-20 1951-06-12 Globe Oil Tools Co Mechanism for the control and operation of a gate
US2635583A (en) * 1949-10-21 1953-04-21 Robert O Bill Pressure fluid motor and combined telescopic guide and housing therefor
US2604639A (en) * 1950-01-18 1952-07-29 Jack L Killifer Hydraulic hospital bed lift
US2766673A (en) * 1951-09-29 1956-10-16 Ferguson Harry Inc Adjusting mechanism for agricultural implement parts
US2761425A (en) * 1952-06-17 1956-09-04 Gen Motors Corp Reciprocatory fluid actuated device
US2982256A (en) * 1954-04-13 1961-05-02 Littlefield Eflie Dora Jones Electrical apparatus and methods
US2814872A (en) * 1955-07-05 1957-12-03 William A Gerrans Fluid actuated tool
US2914034A (en) * 1956-07-06 1959-11-24 Logansport Machine Co Inc Vacuum control valve
US2896583A (en) * 1956-12-28 1959-07-28 Jarvis A Stixrood Counterbalancing hydraulic cylinder
US2987049A (en) * 1957-03-29 1961-06-06 Dura Corp Cylinder and valve assembly
US3415487A (en) * 1966-05-16 1968-12-10 North American Plastics Magnetic control valve with concentric coils
US3375760A (en) * 1966-07-26 1968-04-02 John F. Taplin Rolling diaphragm device having springbiased piston and means for precluding transmission of spring-windup to piston
WO1987002642A1 (en) * 1985-10-31 1987-05-07 Sundstrand Corporation Deployment-retraction apparatus for aircraft turbines

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