GB828858A - Improvements in or relating to control systems for variable pitch propellers - Google Patents
Improvements in or relating to control systems for variable pitch propellersInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
- B64C11/385—Blade 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.
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)
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 |
-
1957
- 1957-02-26 GB GB645857A patent/GB828858A/en not_active Expired
Cited By (9)
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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