US3218797A - Starting system - Google Patents

Starting system Download PDF

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Publication number
US3218797A
US3218797A US384646A US38464664A US3218797A US 3218797 A US3218797 A US 3218797A US 384646 A US384646 A US 384646A US 38464664 A US38464664 A US 38464664A US 3218797 A US3218797 A US 3218797A
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US
United States
Prior art keywords
motor
flow
supply conduit
hydraulic
fluid
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
US384646A
Inventor
Lyston C Jennings
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.)
New York Air Brake LLC
Original Assignee
New York Air Brake LLC
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 New York Air Brake LLC filed Critical New York Air Brake LLC
Priority to US384646A priority Critical patent/US3218797A/en
Priority to GB8624/65A priority patent/GB1045224A/en
Priority to DE19651476462 priority patent/DE1476462B1/en
Priority to FR11319A priority patent/FR1427547A/en
Application granted granted Critical
Publication of US3218797A publication Critical patent/US3218797A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started

Definitions

  • This invention relates to hydraulic starting systems for engines, and particularly for engines of the turbine type.
  • the object of the invention is to provide a lightweight, simple, relatively inexpensive and automatic hydraulic starting system.
  • the starting system includes a fixed displacement starter motor 1, a supply pump 2, and a supply conduit 3 which connects the discharge port 2:: of the pump with the inlet port 1a of the motor.
  • Motor 1 discharges to a hydraulic reservoir 4 which serves as a source of fluid for pump 2.
  • Pump 2 is driven by a prime mover (not shown) and motor 1 is connected with the engine 5 through a one-way, overrunning clutch 6.
  • the supply pump 2 may be either a variable delivery, discharge pressure compensated pump or a fixed delivery pump provided with a relief valve.
  • a start valve 7 Interposed in supply conduit 3 is a start valve 7 which is biased closed and which has an actuating solenoid 7a that is connected in an electrical circuit including battery 8 and switches 9 and 11.
  • Switch 9 is provided with a holding coil 9a so that once it is closed by the operator it remains closed until switch 11 opens.
  • Switch 11 is biased closed by a spring 12 and is opened by a diaphragm actuating motor 13.
  • the opposed working spaces 13a and 13b of motor 13 are connected with the entrance and throat, respectively, of a venturi 14 located in conduit 3.
  • the parts 11, 12, 13 and 14 constitute a flow sensitive switch that opens whenever the rate of flow through supply conduit 3 exceeds a predetermined value.
  • this value is the flow demand of motor 1 at starter cut-out speed, i.e., a speed higher than ignition speed at which the engine is capable of independent operation.
  • a hydraulic starting system comprising (a) a source of hydraulic fluid under pressure; (b) a fixed displacement hydraulic motor; (0) a supply conduit for leading fluid from the source to the motor; and (d) means responsive to the rate of flow through the supply conduit for terminating the supply of fluid to the motor when the rate of flow exceeds a predetermined value.
  • a hydraulic starting system for accelerating an engine to starter cut-out speed comprising a pp y p p; (b) a fixed displacement starter motor; (0) a supply conduit for leading fluid from the source to the motor; (d) a start valve controlling flow through the supply conduit; (e) means for opening the start valve; and (f) means responsive to the rate of flow through the supply conduit for closing the start valve when the rate of flow exceeds a predetermined value indicative of starter cut-out speed.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Pumps (AREA)
  • Fluid-Pressure Circuits (AREA)

Description

Nov. 23, 1965 L. c. JENNINGS STARTING SYSTEM Filed July 23, 1964 EOkOE ATTORNEYS United States Patent 3,218,797 STARTING SYSTEM Lyston C. Jennings, Watertown, N.Y., assignor to The New York Air Brake Company, a corporation of New Jerse y Filed July 23, 1964, Ser. No. 384,646
2 Claims. (Cl. 60-19) This invention relates to hydraulic starting systems for engines, and particularly for engines of the turbine type.
The object of the invention is to provide a lightweight, simple, relatively inexpensive and automatic hydraulic starting system.
The preferred embodiment of the invention is described herein with reference to the accompanying drawing whose single figure is a schematic diagram of the system.
As shown in the drawing, the starting system includes a fixed displacement starter motor 1, a supply pump 2, and a supply conduit 3 which connects the discharge port 2:: of the pump with the inlet port 1a of the motor. Motor 1 discharges to a hydraulic reservoir 4 which serves as a source of fluid for pump 2. Pump 2 is driven by a prime mover (not shown) and motor 1 is connected with the engine 5 through a one-way, overrunning clutch 6. The supply pump 2 may be either a variable delivery, discharge pressure compensated pump or a fixed delivery pump provided with a relief valve.
Interposed in supply conduit 3 is a start valve 7 which is biased closed and which has an actuating solenoid 7a that is connected in an electrical circuit including battery 8 and switches 9 and 11. Switch 9 is provided with a holding coil 9a so that once it is closed by the operator it remains closed until switch 11 opens. Switch 11 is biased closed by a spring 12 and is opened by a diaphragm actuating motor 13. The opposed working spaces 13a and 13b of motor 13 are connected with the entrance and throat, respectively, of a venturi 14 located in conduit 3. It will be understood that the parts 11, 12, 13 and 14 constitute a flow sensitive switch that opens whenever the rate of flow through supply conduit 3 exceeds a predetermined value. In accordance with the invention, this value is the flow demand of motor 1 at starter cut-out speed, i.e., a speed higher than ignition speed at which the engine is capable of independent operation.
Assuming that pump 2 is running, the starting cycle is initiated by depressing switch 9 to thereby complete the electrical circuit and cause solenoid 7a to open start valve 7. Fluid discharged by pump 2 may now flow to 3,218,797 Patented Nov. 23, 1965 and through motor 1 causing it to develop torque and accelerate engine 5. As the speed of the engine increases, so too does the flow demand of motor 1, and consequently the rate of flow through supply conduit 3. Thus, the switch-opening force developed by the pressure differential between spaces 13a and 13b of actuating motor 13 commences to increase. However, until the engine reaches cut-out speed, this force is not large enough to overcome the opposing bias or spring 12 and switch 11 remains closed. When the engine 5 is accelerated to this speed, motor 13 overpowers spring 12 and opens switch 11. As a result, starting valve 7 closes and interrupts the flow of fluid to motor 1. Therefore, the starter motor comes to rest. Since opening of switch 11 de-energizes holding coil 9a, and thus allows switch 9 to open, the system is automatically reset for the next starting cycle. As stated previously, the drawing and description relate only to the preferred embodiment of the invention. Since changes can be made in the structure of this embodiment without departing from the inventive concept, the following claims should provide the sole measure of the scope of the invention.
What I claim is: 1. A hydraulic starting system comprising (a) a source of hydraulic fluid under pressure; (b) a fixed displacement hydraulic motor; (0) a supply conduit for leading fluid from the source to the motor; and (d) means responsive to the rate of flow through the supply conduit for terminating the supply of fluid to the motor when the rate of flow exceeds a predetermined value. 2. A hydraulic starting system for accelerating an engine to starter cut-out speed comprising a pp y p p; (b) a fixed displacement starter motor; (0) a supply conduit for leading fluid from the source to the motor; (d) a start valve controlling flow through the supply conduit; (e) means for opening the start valve; and (f) means responsive to the rate of flow through the supply conduit for closing the start valve when the rate of flow exceeds a predetermined value indicative of starter cut-out speed.
No references cited.
JULIUS E. WEST, Primary Examiner.

Claims (1)

1. A HYDRAULIC STARTING SYSTEM COMPRISING (A) A SOURCE OF HYDRAULIC FLUID UNDER PRESSURE; (B) A FIXED DISPLACMENT HYDRAULIC MOTOR; (C) A SUPPLY CONDUIT FOR LEADING FLUID FROM THE SOURCE TO THE MOTOR; AND (D) MEANS RESPONSIVE TO THE RATE OF FLOW THROUGH THE SUPPLY CONDUIT FOR TERMINATING THE SUPPLY OF FLUID TO THE MOTOR WHEN THE RATE OF FLOW EXCEDS A PREDETERMINED VALUE.
US384646A 1964-07-23 1964-07-23 Starting system Expired - Lifetime US3218797A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US384646A US3218797A (en) 1964-07-23 1964-07-23 Starting system
GB8624/65A GB1045224A (en) 1964-07-23 1965-03-01 Improvements in hydraulic starting systems for engines
DE19651476462 DE1476462B1 (en) 1964-07-23 1965-03-12 Hydraulic turning system for internal combustion engines
FR11319A FR1427547A (en) 1964-07-23 1965-03-31 Starting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US384646A US3218797A (en) 1964-07-23 1964-07-23 Starting system

Publications (1)

Publication Number Publication Date
US3218797A true US3218797A (en) 1965-11-23

Family

ID=23518154

Family Applications (1)

Application Number Title Priority Date Filing Date
US384646A Expired - Lifetime US3218797A (en) 1964-07-23 1964-07-23 Starting system

Country Status (3)

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US (1) US3218797A (en)
DE (1) DE1476462B1 (en)
GB (1) GB1045224A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5048295A (en) * 1988-04-13 1991-09-17 Hydromatik Gmbh Hydrostatic transmission

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1358863A (en) * 1963-06-07 1964-04-17 New York Air Brake Co Hydraulic starting system for heat engine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5048295A (en) * 1988-04-13 1991-09-17 Hydromatik Gmbh Hydrostatic transmission

Also Published As

Publication number Publication date
GB1045224A (en) 1966-10-12
DE1476462B1 (en) 1970-02-26

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