GB828858A - Improvements in or relating to control systems for variable pitch propellers - Google Patents

Improvements in or relating to control systems for variable pitch propellers

Info

Publication number
GB828858A
GB828858A GB645857A GB645857A GB828858A GB 828858 A GB828858 A GB 828858A GB 645857 A GB645857 A GB 645857A GB 645857 A GB645857 A GB 645857A GB 828858 A GB828858 A GB 828858A
Authority
GB
United Kingdom
Prior art keywords
pitch
valve
line
propeller
torque
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
GB645857A
Inventor
Robert Kelman Crowe
John Ramsay Cullen
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.)
Bristol Aero Engines Ltd
Original Assignee
Bristol Aero Engines Ltd
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 Bristol Aero Engines Ltd filed Critical Bristol Aero Engines Ltd
Priority to GB645857A priority Critical patent/GB828858A/en
Publication of GB828858A publication Critical patent/GB828858A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/38Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B64C11/385Blade pitch-changing mechanisms fluid, e.g. hydraulic comprising feathering, braking or stopping systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Hydraulic Motors (AREA)

Abstract

828,858. Variable pitch propellers. BRISTOL AERO-ENGINES Ltd. Feb. 17, 1958 [Feb. 26, 1957], No. 6458/57. Class 114 A control system for a variable pitch propeller includes pitch lock means operable by the onset of a predetermined negative-torque in the propeller drive transmission to lock the propeller against pitch fining movement. In the embodiment of Fig. 1, a double acting hydraulic pitch change motor 12 having a fixed brake stop 26 and a fixed feathering stop 27 has a fine pitch line 13 and a coarse pitch line 15. To coarsen the pitch oil is supplied under pressure via line 14, by-pass 16 and non-return valve 29 to the left hand side of the motor piston 10, oil on the other side exhausting through line 13. To reduce pitch oil under pressure is supplied to the line 13 from which it branches to act on the right hand side of the piston 10 and to move the pitch lock valve 17 against the action of its spring 22 so that oil from the left-hand side of the piston can exhaust through said valve into line 14. The port 32 of the reduction gearing driving the propeller shaft 30 is connected to hydraulic piston and cylinder units 33 forming port of a torquemeter so that when negative-torque is experienced, i.e. when the propeller windmills and drives the engine, the port 32 moves clockwise, thus tripping a lever 25 to raise a spring- loaded spill valve 23 which connects the fine pitch line 13 with a low pressure line 24, thereby relieving pressure on the valve 17. The spring 22 then closes said valve, forming a hydraulic lock in the motor cylinder so that fining of the propeller pitch with consequent increase in windmilling drag, is prevented. In another embodiment the spill valve is replaced by a multi-purpose increase pitch valve and the system includes main control, servo, and negative-torque signal valves so arranged that with the onset of negative-torque the lock valve 17 closes as in the first embodiment but the coarse pitch line is placed in direct communication with the delivery side of the governor pump. The propeller moves to a coarser pitch, the windmilling and the negative-torque are reduced, and the propeller is returned to the control of the main control valve. Specification 814,844 is referred to.
GB645857A 1957-02-26 1957-02-26 Improvements in or relating to control systems for variable pitch propellers Expired GB828858A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB645857A GB828858A (en) 1957-02-26 1957-02-26 Improvements in or relating to control systems for variable pitch propellers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB645857A GB828858A (en) 1957-02-26 1957-02-26 Improvements in or relating to control systems for variable pitch propellers

Publications (1)

Publication Number Publication Date
GB828858A true GB828858A (en) 1960-02-24

Family

ID=9814823

Family Applications (1)

Application Number Title Priority Date Filing Date
GB645857A Expired GB828858A (en) 1957-02-26 1957-02-26 Improvements in or relating to control systems for variable pitch propellers

Country Status (1)

Country Link
GB (1) GB828858A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498253A1 (en) * 1981-01-19 1982-07-23 Alexeev Ivan Control for turbine driven constant pitch airscrew - has screw speed controller valves servo-operated for reverse thrust dependent on torque input
US4863347A (en) * 1987-10-03 1989-09-05 Dowty Rotol Limited Bladed rotor assemblies
CN108032993A (en) * 2017-12-15 2018-05-15 惠阳航空螺旋桨有限责任公司 A kind of narrow spacing locks stop device
WO2018234328A1 (en) 2017-06-19 2018-12-27 Rolls-Royce Marine As Rotary actuator, variable pitch hub, propeller mount
EP3640133A1 (en) * 2018-10-15 2020-04-22 Pratt & Whitney Canada Corp. System and method for slowing down aircraft
CN115263871A (en) * 2022-06-23 2022-11-01 河北喆速科技有限公司 Hydraulic self-protection braking system
US11668253B2 (en) 2020-10-16 2023-06-06 Pratt & Whitney Canada Corp. System and method for providing in-flight reverse thrust for an aircraft

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2498253A1 (en) * 1981-01-19 1982-07-23 Alexeev Ivan Control for turbine driven constant pitch airscrew - has screw speed controller valves servo-operated for reverse thrust dependent on torque input
US4863347A (en) * 1987-10-03 1989-09-05 Dowty Rotol Limited Bladed rotor assemblies
WO2018234328A1 (en) 2017-06-19 2018-12-27 Rolls-Royce Marine As Rotary actuator, variable pitch hub, propeller mount
CN108032993A (en) * 2017-12-15 2018-05-15 惠阳航空螺旋桨有限责任公司 A kind of narrow spacing locks stop device
CN108032993B (en) * 2017-12-15 2024-04-09 惠阳航空螺旋桨有限责任公司 Small-distance lock stop device
EP3640133A1 (en) * 2018-10-15 2020-04-22 Pratt & Whitney Canada Corp. System and method for slowing down aircraft
US11427304B2 (en) 2018-10-15 2022-08-30 Pratt & Whitney Canada Corp. System and method for slowing down aircraft
US11668253B2 (en) 2020-10-16 2023-06-06 Pratt & Whitney Canada Corp. System and method for providing in-flight reverse thrust for an aircraft
CN115263871A (en) * 2022-06-23 2022-11-01 河北喆速科技有限公司 Hydraulic self-protection braking system

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