US1353656A - Fluid-operated motor - Google Patents

Fluid-operated motor Download PDF

Info

Publication number
US1353656A
US1353656A US360939A US36093920A US1353656A US 1353656 A US1353656 A US 1353656A US 360939 A US360939 A US 360939A US 36093920 A US36093920 A US 36093920A US 1353656 A US1353656 A US 1353656A
Authority
US
United States
Prior art keywords
fluid
motor
piston
cylinder
pilot valve
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
US360939A
Inventor
Charles L Heisler
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to US360939A priority Critical patent/US1353656A/en
Application granted granted Critical
Publication of US1353656A publication Critical patent/US1353656A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow

Definitions

  • the present invention relates to fluid operated motors such as used to operate the valve gear of engines, for example, elastic fluid turbines, for regulating the admission operated motor of this character.
  • 5 indicates the cylinder of the fluid operated motor, and 6 the piston to which is connected a stem 7 which operates the valve gear of the turbine or other engine for controlling the admission of elastic fluid thereto.
  • stem 7 is provided at its outer end with a rack 8 which engages a pinion 9 on a shaft 10 from which shaft the admission valve or valves of a turbine or other engine are operated by means of cams or otherwise.
  • Valve gear arrangements of this character are well known and need no detailed deare passages connecting the pilot valve casing to cylinder 5 on opposite sides of pistori 6.
  • the pilot valve stem 17 is connected at its outer end to a floating lever 18 which lever is connected by a rod 19 and bell crank lever 20 to a speed governor 21.
  • Speed gover'nor 21 is the governor of an engine, the valve gear of which is operated by the fluid actuated motor illustrated, and is used to driven from the engine shaft.
  • Floating lever 18 is connected at one end to an arm 22 which projects from stem 7.- f
  • the object of my invention is to overcome the above difliculty and to this end I provide an arrangement of apparatus whereby the fluid-actuated motor which is operated from the forced feed lubricating system may be operated with fluid of a very much lower pressure than heretofore, z'. 6., a pressure no higher than that actually required for the lubricating system, while at the same time, ample motive power is provided for operating the valve gear.
  • a second fluid-actuated motor which term a booster motor and which is operated by high pressure elastic fluid such as is supplied to operate the engine or turbine. 'llhis booster motor is arranged in such manner that it will assist the regular hydraulic motor in operating the valve gear.
  • pilot valve 27A The'admission conduit for pilot valve 2'? is indicated at 28 and the discharge conduit at, 29.
  • the pilot valve casing 27 is connectedto cylinder 24 on the two sides of piston 25 by passages 30 and 31.
  • the stem 32 of pilot valve 27 is connected to a fluid actuated abutment 33 which is shown in the form of a piston which moves in the cylinder 34:.
  • abutment 33 is subjected to the pressure in cylinder 5 on one side of piston 6 through a passage 35, and the other side of the abutment is subjected to the pressure on the other side of the piston 6 through a passage 36'
  • Abutment 33 is normally maintained in an intermediate position in cylinder 34 by means of springs 37 which at opposite ends engage spaced collars 38 loosely mounted on pilot valve stem 32, and normally held against shoulders 39 which are fixed on stem 32.
  • the loose collars 38 are positioned by means of spaced stops 4:0 and 41.
  • pilot valve 12 is moved to connect inlet conduit 13 to passage 15, discharge conduit 14: to passage 16, then the pressure will be increased on the left hand side of piston 6 and decreased on the right hand sidethereof.
  • fluid actuated abutment 33 will be forced toward the left connecting inlet conduit 28 through passage 30 to the left hand side of piston 25 and discharge conduit 29 to the right hand side,
  • actuating fluid as elastic fluid from the engine
  • piston 25 will move toward the right and in a direction to assist the movement of piston 6.
  • abutment 33 will be brought back to its intermediate position by springs 37.
  • left hand collar 38 will be held from movement by the stop 4C0, while the right hand collar 38 will be forced toward the left by shoulder 39 to put spring 37 under compression, the stem 32 at such time sliding through left hand collar 38.
  • I utilize fluid of comparatively lovi pressure, such as would normally be supplied through the force feed lubricating system of an engine, in the main fluid actuated motor, while at the same time i am'enabled to obtain ample power for operating the valve gear by utilizing in series with the fluid-actuated motor, a booster motor which may be operated by high pressure fluid such as the elastic fluid used in the engine, for example, steam.
  • a fluid actuated motor comprising a cylinder, a piston therein, and a pilot valve for controlling the passage of actuating fluid to the cylinder
  • second fluid actuated motor comprising a cylinder, a piston and a pilot valve for controlling the passage of actuating fluid to such cylinder
  • fluid actuated motor comprising a cylinder
  • a piston and a pilot valve for controlling the passage of actuating fluid to such cylinder, means connecting said two pistons together, a movable abutment, a cylinder in 15 which it moves, conduits connecting opposite ends of the last named cylinder to opposite ends of the cylinder of the first-named motor, a stem which connects said abutment to the pilot valve of the second-named 20 motor, and means for normally maintain ing said abutment in a central-position in its cylinder sothe pilot valve of the secondnamed motor is closed

Description

C. L. HEISLER.
FLUID OPERATED MOTOR.
APPtlCATlON FILED FEB. 24. 1920.
Pawnted Sept. 21,1920.
N. e GP 7 1 g m E Q P .L eL t vs nk l m v 5 m5 F m a Qw .QN
CHARLES L. HEISLEBI, 0F SCHENECTADY, NEW YORK, ASSIGNOR T0 GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
FLUID-OPERATED Moron.
Specification of Letters Patent.
Patented Sept. 21, 1920.
Application filed. February 24, 1920. Serial No 360,939.
To allwhomitmag concern."
Be it known that I, CHARLES L. HEISLER, a citizen of the United States, residing at Schenectady, in the county of Schenectady, State of New York, have invented certain new and useful Improvements in Fluid-Operated Motors, of which-the following is a specification.
The present invention relates to fluid operated motors such as used to operate the valve gear of engines, for example, elastic fluid turbines, for regulating the admission operated motor of this character.
of operating fluid to the engines, and the object of my invention is to provide an improved structure and arrangement in a fluid For a consideration of what I believe to be novel and my invention, attention is directed to the accompanying description and the claims appended thereto. t
In the drawing, the figure is a sectional view of a fluid actuated motor embodying my invention, only as much of the engine parts being indicated as is necessary for an understanding of the invention.
Referring to the drawing, 5 indicates the cylinder of the fluid operated motor, and 6 the piston to which is connected a stem 7 which operates the valve gear of the turbine or other engine for controlling the admission of elastic fluid thereto. In the present instance, stem 7 is provided at its outer end with a rack 8 which engages a pinion 9 on a shaft 10 from which shaft the admission valve or valves of a turbine or other engine are operated by means of cams or otherwise.
Valve gear arrangements of this character are well known and need no detailed deare passages connecting the pilot valve casing to cylinder 5 on opposite sides of pistori 6. The pilot valve stem 17 is connected at its outer end to a floating lever 18 which lever is connected by a rod 19 and bell crank lever 20 to a speed governor 21. Speed gover'nor 21 is the governor of an engine, the valve gear of which is operated by the fluid actuated motor illustrated, and is used to driven from the engine shaft.
control the speed of theengine as is well understood. Floating lever 18 is connected at one end to an arm 22 which projects from stem 7.- f
The arrangement so far described forms an ordinary and well known type of fluid actuated motor arrangement for regulating the valve gear of an engine by means of a speed governor, the connections including a follow-up device to prevent over-travel of the valve gear. The operation of such a fluid actuated motor is well understood and may be briefly described as follows:
In case of increase in speed, the balls of governor 21 will fly out, thereby moving pilot valve 12 toward the right and connecting inlet conduit 13 with passage 15 and exhaust conduit 14 with passage 16. As a result actuating fluid for the motor will be admitted to the left hand side of the iston 6 and exhausted from the right hand side causing it to move in a direction to close the Valve means which is actuated-by rack 8. In case of a decrease in speed of the engine,
the same action takes place, except in the ter, it is customary to utilize as motive fluid 4 for the fluid actuated motor, oil from the forced feed lubricating system for the engine, such oil being supplied by a pump However, the fluid actuated motor requires considerably more pressure for its operation than is required for lubricating purposes. As a result, it has been the custom ,to provide a pump which would maintain a pressure in the lubricating system sufficiently high for use in the fluid-actuated motor for the valve gear although such pressure was much higher than that actually required for lubrieating purposes. This has represented a considerable waste of energy since but comparatively little fluid isused in the fluidactuated motor. I
More particularly, the object of my invention is to overcome the above difliculty and to this end I provide an arrangement of apparatus whereby the fluid-actuated motor which is operated from the forced feed lubricating system may be operated with fluid of a very much lower pressure than heretofore, z'. 6., a pressure no higher than that actually required for the lubricating system, while at the same time, ample motive power is provided for operating the valve gear. Accordingly if provide in connection with the usual fluid-actuated motor which is connected to the lubricating s stem, a second fluid-actuated motor which term a booster motor and which is operated by high pressure elastic fluid such as is supplied to operate the engine or turbine. 'llhis booster motor is arranged in such manner that it will assist the regular hydraulic motor in operating the valve gear.
24 indicates a cylinder in which is a piston 25 provided with a stem 26 which is connected to piston 6, the two cylinders 5 and 2% being arranged in axial alinement. Connected to cylinder 24 is a smallercylinder 27 in which is a pilot valve 27A. The'admission conduit for pilot valve 2'? is indicated at 28 and the discharge conduit at, 29. The pilot valve casing 27 is connectedto cylinder 24 on the two sides of piston 25 by passages 30 and 31. The stem 32 of pilot valve 27 is connected to a fluid actuated abutment 33 which is shown in the form of a piston which moves in the cylinder 34:. One side of abutment 33 is subjected to the pressure in cylinder 5 on one side of piston 6 through a passage 35, and the other side of the abutment is subjected to the pressure on the other side of the piston 6 through a passage 36' Abutment 33 is normally maintained in an intermediate position in cylinder 34 by means of springs 37 which at opposite ends engage spaced collars 38 loosely mounted on pilot valve stem 32, and normally held against shoulders 39 which are fixed on stem 32. The loose collars 38 are positioned by means of spaced stops 4:0 and 41.
Assume that the engine is operating and the various parts are in the positions shown in the drawing. If now speed governor 21 moves pilot valve 12 in one direction or the other, it will result in admitting fluid pressure to one side of piston 6 and permitting it to exhaust from the other side of piston 6 in the usual manner. As aresult the pressures on opposite sides of abutment 33 become unbalanced and consequently abutment 33 will be moved in one direction or the other, thereby moving pilot valve 27 to connect inlet conduit 28 to one side of piston 25 and discharge conduit 29 to the other side, the connections being such that piston 25 will move in a direction to assist the movement of piston 6. For example, assuming that pilot valve 12 is moved to connect inlet conduit 13 to passage 15, discharge conduit 14: to passage 16, then the pressure will be increased on the left hand side of piston 6 and decreased on the right hand sidethereof. As a result fluid actuated abutment 33 will be forced toward the left connecting inlet conduit 28 through passage 30 to the left hand side of piston 25 and discharge conduit 29 to the right hand side,
whereupon actuating fluid, as elastic fluid from the engine, will be admitted to the left hand end of cylinder 24 so that piston 25 will move toward the right and in a direction to assist the movement of piston 6. As soon as the pressures on opposite sides of piston 6 become balanced, then abutment 33 will be brought back to its intermediate position by springs 37. As is clear, when abutment 33 moves to the left, left hand collar 38 will be held from movement by the stop 4C0, while the right hand collar 38 will be forced toward the left by shoulder 39 to put spring 37 under compression, the stem 32 at such time sliding through left hand collar 38.
With the above described arrangement,
therefore, it will be seen that I utilize fluid of comparatively lovi pressure, such as would normally be supplied through the force feed lubricating system of an engine, in the main fluid actuated motor, while at the same time i am'enabled to obtain ample power for operating the valve gear by utilizing in series with the fluid-actuated motor, a booster motor which may be operated by high pressure fluid such as the elastic fluid used in the engine, for example, steam.
In accordance with the provisions of the patent statutes, l have described the principle of operation of my invention, together with the apparatus which ll now consider to represent the best embodiment thereof, but I desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
What ll claim as new and desire to secure by Letters Patent of the United States, is
1. in an apparatus of the character described, the combination of a fluid actuated motor having a pilot valve, a second fluid actuated motor having its moving element connected to the moving element of the first-named motor, and means controlled by the fluid pressure of the first-named motor for admitting fluid pressure to the secondnamed motor.
2. In an apparatus of the character described, the combination of a fluid actuated motor having a pilot valve a second fluid actuated motor having its moving element connected to the moving element of the first-named motor, and valve means controlled by the pressure of the first-named motor for admitting fluid pressure to the second-named motor.
3. In combination, a fluid actuated motor comprising a cylinder, a piston therein, and a pilot valve for controlling the passage of actuating fluid to the cylinder, 2. second fluid actuated motor comprising a cylinder, a piston and a pilot valve for controlling the passage of actuating fluid to such cylinder,
fluid actuated motor comprising a cylinder,
a piston and a pilot valve for controlling the passage of actuating fluid to such cylinder, means connecting said two pistons together, a movable abutment, a cylinder in 15 which it moves, conduits connecting opposite ends of the last named cylinder to opposite ends of the cylinder of the first-named motor, a stem which connects said abutment to the pilot valve of the second-named 20 motor, and means for normally maintain ing said abutment in a central-position in its cylinder sothe pilot valve of the secondnamed motor is closed In Witness whereof, I have hereunto set 25 my hand this 20th day of February, 1920.
CHAR-LES L. HEISLER.
US360939A 1920-02-24 1920-02-24 Fluid-operated motor Expired - Lifetime US1353656A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US360939A US1353656A (en) 1920-02-24 1920-02-24 Fluid-operated motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US360939A US1353656A (en) 1920-02-24 1920-02-24 Fluid-operated motor

Publications (1)

Publication Number Publication Date
US1353656A true US1353656A (en) 1920-09-21

Family

ID=23420006

Family Applications (1)

Application Number Title Priority Date Filing Date
US360939A Expired - Lifetime US1353656A (en) 1920-02-24 1920-02-24 Fluid-operated motor

Country Status (1)

Country Link
US (1) US1353656A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2466391A (en) * 1943-10-30 1949-04-05 Franklin Railway Supply Co Steam locomotive power adjusting mechanism for cam actuated valve
US2791092A (en) * 1952-07-07 1957-05-07 Mercier Jean Hydraulic follow-up systems
US2824426A (en) * 1955-03-29 1958-02-25 Gen Motors Corp Temperature modified speed switch mechanism
US2892310A (en) * 1954-02-17 1959-06-30 Mercier Jean Automatic follow-up system for successive application of power sources
US2980069A (en) * 1958-11-24 1961-04-18 Holley Carburetor Co Mechanical computing device
US3045714A (en) * 1959-07-13 1962-07-24 John R Greeno Automatic spring assembly machine
US3070071A (en) * 1960-03-11 1962-12-25 North American Aviation Inc Failure protected signal translating system
US4222309A (en) * 1976-09-07 1980-09-16 Theodore Ongaro Hydraulic power system

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2466391A (en) * 1943-10-30 1949-04-05 Franklin Railway Supply Co Steam locomotive power adjusting mechanism for cam actuated valve
US2791092A (en) * 1952-07-07 1957-05-07 Mercier Jean Hydraulic follow-up systems
US2892310A (en) * 1954-02-17 1959-06-30 Mercier Jean Automatic follow-up system for successive application of power sources
US2824426A (en) * 1955-03-29 1958-02-25 Gen Motors Corp Temperature modified speed switch mechanism
US2980069A (en) * 1958-11-24 1961-04-18 Holley Carburetor Co Mechanical computing device
US3045714A (en) * 1959-07-13 1962-07-24 John R Greeno Automatic spring assembly machine
US3070071A (en) * 1960-03-11 1962-12-25 North American Aviation Inc Failure protected signal translating system
US4222309A (en) * 1976-09-07 1980-09-16 Theodore Ongaro Hydraulic power system

Similar Documents

Publication Publication Date Title
US1353656A (en) Fluid-operated motor
US2393313A (en) Steam power plant
US1411991A (en) Governor
US740203A (en) Fluid-pressure engine.
US1973443A (en) Apparatus for governing steam turbines
US991950A (en) Valve-control system.
US801399A (en) Governing mechanism for turbines.
US796518A (en) Governing mechanism for turbines.
US769300A (en) Turbine of the multiple-expansion type.
US908033A (en) Reversing mechanism for engines.
US1573781A (en) Governing mechanism for turbines
US803041A (en) Turbine valve mechanism.
US1116346A (en) Fluid-pressure engine.
US1141146A (en) Automatic control of cut-off valves.
US861085A (en) Governing mechanism for turbines.
US592248A (en) Engine
US1198635A (en) Heat-balancing valve.
US1476100A (en) Safety device for prime movers, especially for steam turbines
US787134A (en) Steam-engine.
US690620A (en) Telescopic compound engine.
US1553119A (en) Power installation
US295179A (en) Chaeles ii
US1656573A (en) Engine-valve gear
US743326A (en) Pneumatic engine.
US715924A (en) Apparatus for controlling pumping-engines.