GB756469A - Improvements in power plants for aircraft - Google Patents

Improvements in power plants for aircraft

Info

Publication number
GB756469A
GB756469A GB447/54A GB44754A GB756469A GB 756469 A GB756469 A GB 756469A GB 447/54 A GB447/54 A GB 447/54A GB 44754 A GB44754 A GB 44754A GB 756469 A GB756469 A GB 756469A
Authority
GB
United Kingdom
Prior art keywords
clutch
gears
shaft
gear
propeller
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
Application number
GB447/54A
Inventor
Charles J Mcdowall
Victor W Paterson
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation 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 Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to GB447/54A priority Critical patent/GB756469A/en
Publication of GB756469A publication Critical patent/GB756469A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D48/00External control of clutches
    • F16D48/02Control by fluid pressure
    • F16D48/0206Control by fluid pressure in a system with a plurality of fluid-actuated clutches
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D35/00Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • B64D35/08Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D41/00Freewheels or freewheel clutches
    • F16D41/22Freewheels or freewheel clutches with clutching ring or disc axially shifted as a result of lost motion between actuating members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16DCOUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D2500/00External control of clutches by electric or electronic means
    • F16D2500/50Problem to be solved by the control system
    • F16D2500/51Relating safety

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)

Abstract

756.469. Gas turbine plant. GENERAL MOTORS CORPORATION. Jan. 7. 1954, No. 447/54. Class 110(3) [Also in Groups XXIV, XXXIII and XXXIV] . Two gas tubine engines A and B each have an output shaft 10 which connects to a common propeller gear 12 through an overrunning clutch 14, an intermediate shaft 16, a friction clutch 18, a pinion shaft 19 and a pinion 20. A starter motor 22 drives a shaft 24 on which is splined a. sliding toothed clutch element 26 which may be engaged with mating clutch elements of either of two gears 28 and 30 rotatable with respect to the shaft 24. The gears 28 and 30 couple to gears 32 on the intermediate shafts 16 through gears 33, 34 and 35. The clutch element 26 can be shifted to couple the starter with either gear 28 or gear 30, by a 'sliding fork 36 actuated into either extreme position by solenoids (not shown). The friction: clutches 18 are of the type described in Specification 690,592 (see Group XXIV), and they are engaged and disengaged by a hydraulic system supplied from a pump 46 which also supplies oil to the reduction gear and to the clutches 14 (see Group XXIV) and is driven through gears 64, 54 and an overrunning clutch 60 from the starter 22 or through gears 56, 70 and overrunning clutch 62 from the propeller shaft 62. The clutch 14 is a spring loaded ratcheting type and axial movement of one element thereof against spring action as the result of reverse torque from the propeller D resulting from an engine failure operates a micro-switch 240 which effects disengagement of the failed engine's clutch 18 and shuts off the failed engine's fuel supply. Reference has been directed by the Comptroller to Specification 690,592.
GB447/54A 1954-01-07 1954-01-07 Improvements in power plants for aircraft Expired GB756469A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB447/54A GB756469A (en) 1954-01-07 1954-01-07 Improvements in power plants for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB447/54A GB756469A (en) 1954-01-07 1954-01-07 Improvements in power plants for aircraft

Publications (1)

Publication Number Publication Date
GB756469A true GB756469A (en) 1956-09-05

Family

ID=9704502

Family Applications (1)

Application Number Title Priority Date Filing Date
GB447/54A Expired GB756469A (en) 1954-01-07 1954-01-07 Improvements in power plants for aircraft

Country Status (1)

Country Link
GB (1) GB756469A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9611786B2 (en) 2012-01-09 2017-04-04 Honeywell International Inc. Engine systems with enhanced start control schedules

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9611786B2 (en) 2012-01-09 2017-04-04 Honeywell International Inc. Engine systems with enhanced start control schedules

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