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GB818611A - Improvements in or relating to hydraulic variable pitch propellers - Google Patents

Improvements in or relating to hydraulic variable pitch propellers

Info

Publication number
GB818611A
GB818611A GB3860656A GB3860656A GB818611A GB 818611 A GB818611 A GB 818611A GB 3860656 A GB3860656 A GB 3860656A GB 3860656 A GB3860656 A GB 3860656A GB 818611 A GB818611 A GB 818611A
Authority
GB
United Kingdom
Prior art keywords
stop
switch
pitch
propeller
retaining means
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
GB3860656A
Inventor
John Alfred Chilman
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.)
Rotol Ltd
Original Assignee
Rotol 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 Rotol Ltd filed Critical Rotol Ltd
Priority to GB3860656A priority Critical patent/GB818611A/en
Publication of GB818611A publication Critical patent/GB818611A/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)
  • Control Of Fluid Gearings (AREA)

Abstract

818,611. Variable pitch propellers. ROTOL Ltd. Aug. 14, 1957 [Dec. 18, 1956], No. 38606/56. Class 114. A propeller comprising, in the hub 12, a hydraulic pitch change motor 22, pitch stop means 25 operative to prevent the propeller fining off below a predetermined pitch and stop retaining means 28 displaceable between a first position (shown in Fig. 1) in which said retaining means maintains the stop 25 operative and a second position in which the stop is rendered inoperative, has a fluid pressure operated switch 51 outside the hub, conduit means 46 for communicating the switch with a source of hydraulic fluid under pressure to operate the switch, and hydraulic valve means 34 in the propeller hub, said valve means communicating said switch with a bleed 35 to relieve the pressure of fluid in said switch only when the stop retaining means 28 is in its operative position, the switch being operable only when the pressure of fluid in the switch is unrelieved through the bleed 35. A pump 17 supplies pressure fluid via a constant speed unit 14 and conduits 18, 19 to the pitch change motor 22, and also to a solenoid-operated valve 37 which is energized when it is required to render the stop 25 inoperative to permit fining off the propeller pitch, and to a control valve 39 from which a conduit 44, separate from the motor conduits 18, 19, is taken to a piston 31 for moving the stop retaining means 28 against the action of a spring 29 and to an annulus 33 communicating with said hydraulic means 34, formed by an annular recess in the stop retaining means 28 which recess is normally in communication with the bleed 35. Whenever, intentionally or unintentionally, the retaining means 28 is in the position allowing the stop 25 to be inoperative, the recess 34 is out of register with the bleed 35 so that pressure builds up on the spring- loaded piston 50 of the switch 51 to close the switch so that an indicator light (not shown) comes on. The invention is shown applied to a propeller in which the stop means has two stop positions, i.e. a first predetermined fine pitch position and then a second and finer pitch position. Specifications 742,148 and 818,612 are referred to.
GB3860656A 1956-12-18 1956-12-18 Improvements in or relating to hydraulic variable pitch propellers Expired GB818611A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3860656A GB818611A (en) 1956-12-18 1956-12-18 Improvements in or relating to hydraulic variable pitch propellers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3860656A GB818611A (en) 1956-12-18 1956-12-18 Improvements in or relating to hydraulic variable pitch propellers

Publications (1)

Publication Number Publication Date
GB818611A true GB818611A (en) 1959-08-19

Family

ID=10404537

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3860656A Expired GB818611A (en) 1956-12-18 1956-12-18 Improvements in or relating to hydraulic variable pitch propellers

Country Status (1)

Country Link
GB (1) GB818611A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2981684A1 (en) * 2011-10-21 2013-04-26 Snecma TURBOMACHINE BLADE AND TURBOMACHINE BLADE IMPLANT CONTROL SYSTEM
US8672632B2 (en) 2010-01-06 2014-03-18 Rolls-Royce Plc Back-up featherer
IT202300008460A1 (en) * 2023-04-28 2024-10-28 Ge Avio Srl METHODS AND EQUIPMENT TO PREVENT DANGEROUS FAILURES IN DOUBLE ACTION PROPELLERS

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8672632B2 (en) 2010-01-06 2014-03-18 Rolls-Royce Plc Back-up featherer
FR2981684A1 (en) * 2011-10-21 2013-04-26 Snecma TURBOMACHINE BLADE AND TURBOMACHINE BLADE IMPLANT CONTROL SYSTEM
US9200525B2 (en) 2011-10-21 2015-12-01 Snecma Turbomachine blade incidence control system and turbomachine
IT202300008460A1 (en) * 2023-04-28 2024-10-28 Ge Avio Srl METHODS AND EQUIPMENT TO PREVENT DANGEROUS FAILURES IN DOUBLE ACTION PROPELLERS

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