GB614951A - Improvements in or relating to variable pitch propellers - Google Patents

Improvements in or relating to variable pitch propellers

Info

Publication number
GB614951A
GB614951A GB1902846A GB1902846A GB614951A GB 614951 A GB614951 A GB 614951A GB 1902846 A GB1902846 A GB 1902846A GB 1902846 A GB1902846 A GB 1902846A GB 614951 A GB614951 A GB 614951A
Authority
GB
United Kingdom
Prior art keywords
control
pitch
valve
unit
blades
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
GB1902846A
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 GB1902846A priority Critical patent/GB614951A/en
Publication of GB614951A publication Critical patent/GB614951A/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
    • 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
    • B64C11/305Blade pitch-changing mechanisms characterised by being influenced by other control systems, e.g. fuel supply

Abstract

614,951. Variable-pitch propellers. ROTOL, Ltd., MORRIS, E. H., DANVERS, E., and GODDEN, T. E. June 25, 1946, No. 19028. [Class 114] In a reversible, variablepitch propeller comprising a pitch-change mechanism 6, means 59 for normally limiting the movement of the blades to within the positive pitchrange, and a constant-speed unit 14 for automatically regulating the pitch-change mechanism in the positive and negative pitch ranges, a manual control 17 is connected for over-riding the constantspeed unit so that it operates the pitch-change mechanism to move the blades to within the negative. pitch-range and for simultaneously removing the blade-movement limiting means. The control 17 is connected through a linkage 18 with an axially adjustable sleeve 19 for adjusting the loading on the governor spring 22 of the unit 14. Liquid to operate the mechanism 6 is supplied by a pump 12 fitted with a spring-loaded relief valve 39, and a feathering pump 16 is also provided. The control 17 is shown in the position C corresponding to slow running of the engine, and the ram 7 of the pitch-change mechanism is against stops 59, the blades being at zero pitch. The stops 59 comprise resilient fingers which normally collapse inwardly but are maintained outwardly by a spring-loaded abutment 64. When the control 17 is moved to its full power position A and the speed of the plant exceeds the datum speed for which the unit 14 has been adjusted, liquid is supplied from the pump 12, past the valve 13 of the constant speed unit and a valve 36, through pipe 64 and to the left of the ram 7 so that the latter moves clear of the stops 59 and adjusts the blades to a coarse pitch position, this position being controlled by the unit 14 according to the datum setting corresponding to the position of the control 17 along the slot 23. If, with the parts in the position shown, the control 17 is moved through the gate 25 towards the full power position B, an arm 4 of an electric switch is moved to engage a contact 42, thereby energizing solenoids 35, 37 to raise valves 27 and 28 respectively. Liquid in pipe 31 from the pump 12 flows through valve 27 to actuate a motor 29 which overrides the valve 13 and through valve 28 to motors 32 and 33, the former increasing the load on the relief valve 39 and the latter raising the valve 36 which transposes the connections to the mechanism 6. Liquid at increased pressure then flows from the pump 12, through valves 13 and 36 into pipe 54 to the right-hand side of the ram 7 and to passage 55 to open a normally closed spring-loaded valve 56 and thence into a space 63, thereby moving abutment 64 to allow stops 59 to fall inwardly. The ram is then free to continue its travel to the left and the blades enter the negativepitch range until a pin 53 engages a spring- loaded rod 52 to actuate a slide 48 which moves an electric switch 45 to engage a contact 47, thereby de-energizing the solenoid 35 so that the unit 14 is free to assume control again, the solenoid 37 remaining energized. In a modified embodiment in which the unit 14 is normally adjusted by the control 17 as described above, a manual speed control is added which is capable of over-riding the control 17.
GB1902846A 1946-06-25 1946-06-25 Improvements in or relating to variable pitch propellers Expired GB614951A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1902846A GB614951A (en) 1946-06-25 1946-06-25 Improvements in or relating to variable pitch propellers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1902846A GB614951A (en) 1946-06-25 1946-06-25 Improvements in or relating to variable pitch propellers

Publications (1)

Publication Number Publication Date
GB614951A true GB614951A (en) 1948-12-30

Family

ID=10122547

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1902846A Expired GB614951A (en) 1946-06-25 1946-06-25 Improvements in or relating to variable pitch propellers

Country Status (1)

Country Link
GB (1) GB614951A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4671736A (en) * 1983-01-05 1987-06-09 Short Brothers Limited Apparatus for the control of an aerial propeller
EP3543113A1 (en) * 2018-03-23 2019-09-25 Ge Avio S.r.l. System and method for propeller response enhancement during transition from ground to flight configuration for a turbopropeller engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4671736A (en) * 1983-01-05 1987-06-09 Short Brothers Limited Apparatus for the control of an aerial propeller
EP3543113A1 (en) * 2018-03-23 2019-09-25 Ge Avio S.r.l. System and method for propeller response enhancement during transition from ground to flight configuration for a turbopropeller engine
WO2019180260A1 (en) * 2018-03-23 2019-09-26 Ge Avio S.R.L. System and method for propeller response enhancement during transition from ground to flight configuration for a turbopropeller engine
US11738855B2 (en) 2018-03-23 2023-08-29 Ge Avio S.R.L. System and method for propeller response enhancement during transition from ground to flight configuration for a turbopropeller engine

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