US2551246A - Fluid motor - Google Patents

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US2551246A
US2551246A US644287A US64428746A US2551246A US 2551246 A US2551246 A US 2551246A US 644287 A US644287 A US 644287A US 64428746 A US64428746 A US 64428746A US 2551246 A US2551246 A US 2551246A
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Prior art keywords
piston
cylinder
rod
pressure
fluid motor
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Expired - Lifetime
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US644287A
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Arcey Alfred C D
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Bendix Aviation Corp
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Bendix Aviation Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/08Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor
    • F15B11/12Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action
    • F15B11/121Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action providing distinct intermediate positions
    • F15B11/123Servomotor systems without provision for follow-up action; Circuits therefor with only one servomotor providing distinct intermediate positions; with step-by-step action providing distinct intermediate positions by means of actuators with fluid-operated stops

Definitions

  • This invention relates to fluid motors, and parfticularly to uid motors of the servo-type, in which each energization of the motor is for the purpose of moving a work performing element from one to another of its several pre-determined settings-as, for example, the forward, reverse, or neutral position of a clutch or reversing gear.
  • An object of the invention is to provide a multiple position motor of novel construction, featuring simplicity of arrangement and a minimum number of parts.
  • Another object is to provide a multiple position motor whose parts are so inter-related as to assure positive action of accurate extent in moving from one position to another, as desired.
  • Another object is to provide a motor in which accurate positioning is accomplished without relsorting to the use of complicated indexing or latching mechanism.
  • Figure 1 is a schematic representation of a hydraulic system embodying the present invention
  • Figure 2 is a sectional view on a larger scale, Showing the moving parts in the positions assumed when the device to be actuated is in one of its three possible settings;
  • Figures 3 and 4 are views similar to Figure 2, but showing two other possible settings.
  • the characters I and II designate a pair of cylinders disposed in tandem relationship, with the smaller cylinder I I integrated with or rigidly secured to the larger cylinder I0, so that the two have a common dividing wall I2 through which there extends a hollow tube or rod I3 carrying at one end a piston I4 and at the other end one or more stop elements I5, I6 threaded to the threaded end portion of the rod I3, for a purpose to be more fully explained.
  • a second piston, i8, is slidable in the larger cylinder E9, and is integrated with a rod I 9 extending through the outer wall 20 of the larger cylinder and having operative connection with the device 2l to be actuated.
  • Such device 2I may be the reversing gear of a marine engine, or any other power or directional control 2 Claims. (Cl. 121-38) 2 that is shiftable to any one of a plurality orsettings.
  • Three-way valves 3l', 32, 33 ( Figure l) control flow of uid to and from ports 34, 35, 36, of the cylinders I0 andi I; the pump for the uid being indicated at 4I in Figure 1, and the reservoir at 42.
  • the piston rod of piston I4 extends through a partition I2. Carried on the end of the piston rod are the adjustable nuts I5, I6, the purpose of which is to adjustably limit the most forward or ahead position of piston I4, thus making adjustable the mid or neutral position of the devlce.
  • , 32, and 33- may be operateddi rectly, or by remote control', as by@ electricl switches in the circuits leading to the solenoid windings of the valves; if theV valves are of a solenoid type.
  • a by-pass valve for pressure relief purposes, may be inserted across lines 62 and G3, as indicated at6
  • a device of'the class described a pair ofl cylinders intandenr relationship having a com-- mon en d wall, Va ⁇ pairof pistons arranged end to-end in-one of; saidl cylinders, ahollow' rodconnectedto one ofthe pistons and extending' through-said common end wall intol the other cylinder so as to communicate the-space-formed in said one cylinder between the adjacent ends ofsaid piston with the othercylinder, an adjustable element'carriedby said rodfor engagement withsaidl common end wall-A tolimit the'- movement-of said oner piston in one direction, saidf other pistonadapted. to be.
  • a pair of cylindersf in tandem relationship having a common end wall, aiv pair of? pistons arranged end to end in one of said cylinders, a hollow rod connetted to one of the pistons and extending through said common end wall into the other cylinder so as to communicate the space formed inl saidon'e cylinder between the adjacent ends of: said?v pistonY with the other cylinder, an adjustablefelein'entv'carried by said rod for engagement with said common end wall to limit the movene'nt of s'aiii' one piston in one direction.
  • said-f other piston adapted to be connected to a member for moving the same to three positions, the effective areasof the adjacent ends of the pistons-.being-.equal and thefeifective areas of the remote end of--said-one piston being greater than the effective area ofthe remote, end. of said other piston,v means for connecting one end of sa-idone cylinder to a fluid rpressure source and the other end A.of saidone cylinder and said other cylinder to exhaust to causesaidother piston to assume onerposition,.means for connecting both ends of saidone cylinder to said source and said other cylinder to exhaust to cause. saidv other pistonto assume a second position, and means for connecting said one end of saidone cylinder tol exhaust and saidother end of said one cylinder and said other cylinder to said source to cause said other pistonh to assumev aV third position.

Description

May l, 1951 A. c. DARCEY 2,551,246
FLUID MOTOR Filed Jan. 30, 1946 2 Sheets-Sheet l A. C. D'ARCEY May l, 1951 FLUID MOTOR C .ml f.
Filed Jan. 50, 1 946 Patented May 1, 19.51
FLUID MOTOR Alfred C. DArcey, Norwood, Mass., assigner to Bendix Aviation Corporation, Norwood, Mass., a corporation of Delaware Application January 30, 1946, Serial No. 644,287
This invention relates to fluid motors, and parfticularly to uid motors of the servo-type, in which each energization of the motor is for the purpose of moving a work performing element from one to another of its several pre-determined settings-as, for example, the forward, reverse, or neutral position of a clutch or reversing gear.
An object of the invention is to provide a multiple position motor of novel construction, featuring simplicity of arrangement and a minimum number of parts.
Another object is to provide a multiple position motor whose parts are so inter-related as to assure positive action of accurate extent in moving from one position to another, as desired.
Another object is to provide a motor in which accurate positioning is accomplished without relsorting to the use of complicated indexing or latching mechanism.
These and other objects of the invention will become more apparent upon reading the following detailed description of the presently preferred embodiment of the invention, as illustrated in the accompanying drawings. It is to be underf stood, of course, that the drawings are illustrative only, as the invention embraces other embodiments within the scope of the appended claims.
In the drawings, Figure 1 is a schematic representation of a hydraulic system embodying the present invention;
Figure 2 is a sectional view on a larger scale, Showing the moving parts in the positions assumed when the device to be actuated is in one of its three possible settings; and
Figures 3 and 4 are views similar to Figure 2, but showing two other possible settings.
Referring to these drawings, wherein like reference characters designate the same part throughout the several views, the characters I and II designate a pair of cylinders disposed in tandem relationship, with the smaller cylinder I I integrated with or rigidly secured to the larger cylinder I0, so that the two have a common dividing wall I2 through which there extends a hollow tube or rod I3 carrying at one end a piston I4 and at the other end one or more stop elements I5, I6 threaded to the threaded end portion of the rod I3, for a purpose to be more fully explained. A second piston, i8, is slidable in the larger cylinder E9, and is integrated with a rod I 9 extending through the outer wall 20 of the larger cylinder and having operative connection with the device 2l to be actuated. Such device 2I may be the reversing gear of a marine engine, or any other power or directional control 2 Claims. (Cl. 121-38) 2 that is shiftable to any one of a plurality orsettings. Three-way valves 3l', 32, 33 (Figure l) control flow of uid to and from ports 34, 35, 36, of the cylinders I0 andi I; the pump for the uid being indicated at 4I in Figure 1, and the reservoir at 42. Y
For theA ahead, or most extended position of the rod I9 (Figure 4), hydraulic pressure is applied to ports 35 and 36, which pressure acts o n the back or reverse faces of pistons I4 and I8. This pressure drives piston I8 to'its extreme or full ahead position and also drives piston I4 forward until the locknut or adjusting nut hits the partition I2 between the two cavities of the cylinders. function except to put piston I4 in position for the next operation or hold it in place from the preceding operation (Figure 3).
To go into the neutral or mid position (Figure 3) pressure is applied to ports 34 and 35 and re lieved at port 36. The pressure entering port 34 acts on the front or ahead face of piston I8 drivingit in the reverse direction. The uid trapped between pistons I4 and I8 is exhausted through the central bore in the rod I3, then out through port 36, permitting piston I 8 to come up against piston I4; piston I4 then restricts further movement of pistonv I8 by virtue of the fact that 'although the forward face of piston I4 and the rear face of piston I 8 are subject to the-same fluid pressure, the rod of piston I8 is larger in diameter than the rod of piston I 4 and consequently presents less effective area to the pressure exerted, and therefore less force.
The piston rod of piston I4 extends through a partition I2. Carried on the end of the piston rod are the adjustable nuts I5, I6, the purpose of which is to adjustably limit the most forward or ahead position of piston I4, thus making adjustable the mid or neutral position of the devlce.
To go into the reverse, or least extended, position of the cylinder fluid pressure is applied to port 34 and exhausted from ports 35 and 36. This permits the pressure on the front or ahead face of piston IB to drive it and piston I4 into the reverse or astern position (Figure 2).
To go into the mid or neutral position again fluid pressure is applied through ports 34 and 3F. The diiferential area in favor of piston I4 previously mentioned permits it to drive in the forward or ahead direction, forcing piston I8 along with it despite the fact that the same fluid pressure may be exerted on the forward or ahead This latter operation performs no useful- 'cylinder determines-the directionof mot-ion and` ultimate. position cf'theY piston-rod of.' piston*4 I8, from which motion power can be taken for the purpose of operating a marine reverse gear 212 or performing any other function where three positive positions are required.
The valves 3|, 32, and 33-may be operateddi rectly, or by remote control', as by@ electricl switches in the circuits leading to the solenoid windings of the valves; if theV valves are of a solenoid type.
A by-pass valve, for pressure relief purposes, may be inserted across lines 62 and G3, as indicated at6|-.V Also-,- af lter 64- may be inserted in return line 63'for uid cleaning purposes.
VWhere specific-speed or power differentialsfare desired, in moving from one predetermined posi-` tionI to` another, thesecan` bey obtained by use of4 the concept disclosed therein of providing dif#- ferential effective areas on opposite sides of the pistonA I8. Byvarying-z` the degreeof` difference inthescfhrespectiv-eA areas; any;r desired' ratio of power ditferential .maybe' effected',-
What-is claimed-is: Y
1-.I n a device of'the class described, a pair ofl cylinders intandenr relationship having a com-- mon en d wall, Va` pairof pistons arranged end to-end in-one of; saidl cylinders, ahollow' rodconnectedto one ofthe pistons and extending' through-said common end wall intol the other cylinder so as to communicate the-space-formed in said one cylinder between the adjacent ends ofsaid piston with the othercylinder, an adjustable element'carriedby said rodfor engagement withsaidl common end wall-A tolimit the'- movement-of said oner piston in one direction, saidf other pistonadapted. to be. connected tofal memberfor moving the same-to three-positions,- means-forconnecting one endv ofL said one cylin der toafluid pressure source and the other end of saidf one cylinder andsaid other cylinder toexhaust to. cause said other pistonto assume one? position; means. for connecting both endsofi said one cylinder to said source and said other cylinder to exhaust to cause said other piston to assume a second position, and means for connecting said one end of said one cylinder to exhaust and said other end of said one cylinder and said other cylinder to said source to cause said other piston to assume a third position.
2. In a device of the class described, a pair of cylindersf in tandem relationship having a common end wall, aiv pair of? pistons arranged end to end in one of said cylinders, a hollow rod connetted to one of the pistons and extending through said common end wall into the other cylinder so as to communicate the space formed inl saidon'e cylinder between the adjacent ends of: said?v pistonY with the other cylinder, an adjustablefelein'entv'carried by said rod for engagement with said common end wall to limit the movene'nt of s'aiii' one piston in one direction. said-f other" piston adapted to be connected to a member for moving the same to three positions, the effective areasof the adjacent ends of the pistons-.being-.equal and thefeifective areas of the remote end of--said-one piston being greater than the effective area ofthe remote, end. of said other piston,v means for connecting one end of sa-idone cylinder to a fluid rpressure source and the other end A.of saidone cylinder and said other cylinder to exhaust to causesaidother piston to assume onerposition,.means for connecting both ends of saidone cylinder to said source and said other cylinder to exhaust to cause. saidv other pistonto assume a second position, and means for connecting said one end of saidone cylinder tol exhaust and saidother end of said one cylinder and said other cylinder to said source to cause said other pistonh to assumev aV third position.
ALFRED C. DARCEY.
REFERENCES CITED The following references are of record in the flle of' this. patent:
UNITED STATES- PATENTS Number y Name Date 833,631 Rhodes Oct. 1'6, 1906 2,005,387 Pelton --.June 18, '1935 2`,095,820 Lenz Oct. 12, 1937 2,244,770 Englesson June A10,1941 2,401,197 Simpson May 281946
US644287A 1946-01-30 1946-01-30 Fluid motor Expired - Lifetime US2551246A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2738663A (en) * 1951-02-21 1956-03-20 Robert Gair Co Inc Pressure loading control
US3164956A (en) * 1963-03-14 1965-01-12 Boeing Co Two part thrust reverser
US3259251A (en) * 1963-12-26 1966-07-05 Galion Jeffrey Mfg Co Extensible boom with tandem operating cylinders
US3793925A (en) * 1971-06-15 1974-02-26 Livingston Doughty Ltd Fluid pressure-operated piston/cylinder units
US3877349A (en) * 1974-05-15 1975-04-15 Singer Co Dual opposite motion extending and retracting ram fluid cylinders
FR2305621A1 (en) * 1975-03-24 1976-10-22 Westin & Backlund Ab Position regulator with pressure transmission elements - features individually adjustable stops for pressure transmission elements
US4061080A (en) * 1975-08-18 1977-12-06 Ab Westin & Backlund Position regulator
DE3109684A1 (en) * 1981-03-13 1982-09-23 Zahnräderfabrik Renk AG, 8900 Augsburg Regulating device for producing linear movements of varying magnitude
US20140033652A1 (en) * 2012-08-03 2014-02-06 Poly-Clip System Gmbh & Co. Kg Clipping module drive device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US833631A (en) * 1905-04-15 1906-10-16 Charles Edgar Rhodes Steam-engine.
US2005387A (en) * 1930-08-11 1935-06-18 Filer & Stowell Company Tapering mechanism
US2095820A (en) * 1934-08-23 1937-10-12 Gen Electric Control mechanism for multiple hydraulic gears
US2244770A (en) * 1937-01-15 1941-06-10 Englesson John Elov Operating device for propellers, turbine wheels, and pump wheels having rotatable blades
US2401197A (en) * 1944-03-02 1946-05-28 H M Hobson Aircraft & Motor Co Servomotor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US833631A (en) * 1905-04-15 1906-10-16 Charles Edgar Rhodes Steam-engine.
US2005387A (en) * 1930-08-11 1935-06-18 Filer & Stowell Company Tapering mechanism
US2095820A (en) * 1934-08-23 1937-10-12 Gen Electric Control mechanism for multiple hydraulic gears
US2244770A (en) * 1937-01-15 1941-06-10 Englesson John Elov Operating device for propellers, turbine wheels, and pump wheels having rotatable blades
US2401197A (en) * 1944-03-02 1946-05-28 H M Hobson Aircraft & Motor Co Servomotor

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2738663A (en) * 1951-02-21 1956-03-20 Robert Gair Co Inc Pressure loading control
US3164956A (en) * 1963-03-14 1965-01-12 Boeing Co Two part thrust reverser
US3259251A (en) * 1963-12-26 1966-07-05 Galion Jeffrey Mfg Co Extensible boom with tandem operating cylinders
US3793925A (en) * 1971-06-15 1974-02-26 Livingston Doughty Ltd Fluid pressure-operated piston/cylinder units
US3877349A (en) * 1974-05-15 1975-04-15 Singer Co Dual opposite motion extending and retracting ram fluid cylinders
FR2305621A1 (en) * 1975-03-24 1976-10-22 Westin & Backlund Ab Position regulator with pressure transmission elements - features individually adjustable stops for pressure transmission elements
US4061080A (en) * 1975-08-18 1977-12-06 Ab Westin & Backlund Position regulator
DE3109684A1 (en) * 1981-03-13 1982-09-23 Zahnräderfabrik Renk AG, 8900 Augsburg Regulating device for producing linear movements of varying magnitude
US20140033652A1 (en) * 2012-08-03 2014-02-06 Poly-Clip System Gmbh & Co. Kg Clipping module drive device
US9803659B2 (en) * 2012-08-03 2017-10-31 Poly-Clip System Gmbh & Co. Kg Clipping module drive device

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