GB868419A - Hydraulic system for adjustable pitch aeronautical propeller - Google Patents

Hydraulic system for adjustable pitch aeronautical propeller

Info

Publication number
GB868419A
GB868419A GB39014/57A GB3901457A GB868419A GB 868419 A GB868419 A GB 868419A GB 39014/57 A GB39014/57 A GB 39014/57A GB 3901457 A GB3901457 A GB 3901457A GB 868419 A GB868419 A GB 868419A
Authority
GB
United Kingdom
Prior art keywords
conduit
valve
pitch
fluid
control 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
Application number
GB39014/57A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB868419A publication Critical patent/GB868419A/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
    • B64C11/42Blade pitch-changing mechanisms fluid, e.g. hydraulic non-automatic
    • 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
    • B64C11/32Blade pitch-changing mechanisms mechanical
    • B64C11/34Blade pitch-changing mechanisms mechanical automatic
    • B64C11/346Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Operation Control Of Excavators (AREA)

Abstract

868,419. Variable pitch propellers. UNITED AIRCRAFT CORPORATION. Dec. 16, 1957 [Dec. 18,1956], No. 39014/57. Class 114. Variable-pitch propellers are adjusted by an hydraulic motor fed with fluid under the action of a control valve, normally adjusted by a speed governor driven from the engine, and a feathering valve. The housing 14 contains the hydraulic motor which varies the pitch of the blades 12 through suitable cam and gear mechanism. The feathering valve 32 when in its " closed position (as shown) allows communication between the fluid supply source fed to conduit 28 and conduit 28a, which leads to control valve 34, and also connects conduits 26a, 26 and 30a, 30, conduit 26 feeding fluid to the hydraulic motor to decrease the pitch and conduit 30 supplying fluid to increase the pitch. The control valve 34 when in its " central " position (as shown) terminates the flow through conduit 28a from the supply source and this valve is moved by a governor 48, driven from gearing 42, against the action of spring 52 to connect conduits 28a, 30a to provide fluid to the hydraulic motor to increase the pitch, and when the spring loading is sufficient to overcome the governor action conduit 28a communicates with conduit 26a to decrease the pitch. The supply of hydraulic fluid is provided by a main pump 62 and a standby pump 64 which deliver fluid from a tank 56 supplied by pumps 58 from a tank 54. The main pump 62 delivers fluid past filter 66 and conduit 22 to the conduit 28 which is provided with a branch conduit 94 leading to a normally closed valve 92. The standby pump 64 delivers past filter 68 to a conduit 70 which communicates when valve 32 is " closed " with a conduit 70a leading to a spring loaded valve 72 having a small orifice 88, the main delivery flows through conduit 78 to a drain conduit 80 communicating with the tank 56 while part of the flow passes through the orifice 88 to conduit 82 which communicates through passage 84 of control valve 34, when in its " central " position, with conduit 86 which leads to the drain conduit 80. When control valve 34 is moved to vary the pitch it closes conduit 82 and the pressure in this conduit increases to the value existing in conduit 70a thus allowing valve 72 to close under the influence of its spring, thus the pressure in conduit 70 increases and opens a non-return valve 74 thus permitting the delivery from standby pump 64 to join the delivery from the main pump 62 whenever the pitch is changed. Similarly, when the feathering valve 32 is " opened " conduit 70 is closed and the two deliveries combine as above. Specifications 683,906, 724,284 and 824,078 are referred to.
GB39014/57A 1956-12-18 1957-12-16 Hydraulic system for adjustable pitch aeronautical propeller Expired GB868419A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US868419XA 1956-12-18 1956-12-18

Publications (1)

Publication Number Publication Date
GB868419A true GB868419A (en) 1961-05-17

Family

ID=22201259

Family Applications (1)

Application Number Title Priority Date Filing Date
GB39014/57A Expired GB868419A (en) 1956-12-18 1957-12-16 Hydraulic system for adjustable pitch aeronautical propeller

Country Status (1)

Country Link
GB (1) GB868419A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0054310A2 (en) * 1980-12-17 1982-06-23 Herbert Karnikowski Transfer foil for the transfer of figures onto surfaces; transfer process and apparatus therefor
US7997074B2 (en) 2009-07-10 2011-08-16 Vestas Wind Systems A/S Hydraulic station and method for controlling pressure in a hydraulic system of a wind turbine
US8123304B2 (en) 2009-06-16 2012-02-28 Vestas Wind Systems A/S Hydraulic system and method for operating a brake of a wind turbine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0054310A2 (en) * 1980-12-17 1982-06-23 Herbert Karnikowski Transfer foil for the transfer of figures onto surfaces; transfer process and apparatus therefor
EP0054310A3 (en) * 1980-12-17 1985-06-12 Herbert Karnikowski Transfer foil for the transfer of figures onto surfaces; transfer process and apparatus therefor
US8123304B2 (en) 2009-06-16 2012-02-28 Vestas Wind Systems A/S Hydraulic system and method for operating a brake of a wind turbine
US7997074B2 (en) 2009-07-10 2011-08-16 Vestas Wind Systems A/S Hydraulic station and method for controlling pressure in a hydraulic system of a wind turbine

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