GB868419A - Hydraulic system for adjustable pitch aeronautical propeller - Google Patents
Hydraulic system for adjustable pitch aeronautical propellerInfo
- 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
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
- B64C11/42—Blade pitch-changing mechanisms fluid, e.g. hydraulic non-automatic
-
- 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
- B64C11/32—Blade pitch-changing mechanisms mechanical
- B64C11/34—Blade pitch-changing mechanisms mechanical automatic
- B64C11/346—Blade 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.
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)
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 |
-
1957
- 1957-12-16 GB GB39014/57A patent/GB868419A/en not_active Expired
Cited By (4)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2402065A (en) | Propeller control | |
US2781856A (en) | Control system for variable pitch screw propellers | |
US3487820A (en) | Fuel supply systems for internal combustion engines | |
GB868419A (en) | Hydraulic system for adjustable pitch aeronautical propeller | |
GB1078762A (en) | Liquid pumping apparatus | |
US2626669A (en) | Propeller control | |
GB965951A (en) | Improvements in or relating to fluid-pressure servomotor systems | |
GB1315064A (en) | Hydraulic control system for a variable displacement pump supplied by a feed pump | |
US2716459A (en) | Fuel supply for ram jet powered helicopters | |
GB824078A (en) | Aeronautical propeller having safety means for propeller feathering | |
US2935078A (en) | Fuel flow proportioners | |
US2594790A (en) | Fuel system for internal-combustion engines | |
GB996001A (en) | Improvements in or relating to fuel delivery control systems for gas turbine, engines, more particularly for turbojet engines | |
GB1346677A (en) | Hydrodynamic transmission | |
GB763448A (en) | Improvements in or relating to gas turbine engine fuel systems | |
GB684490A (en) | Improvements in or relating to fluid pressure control systems and relief valve for use therein | |
US3199290A (en) | Gas turbine engine afterburner fuel system | |
GB576243A (en) | Improvements in or relating to control devices for hydraulic pressure systems | |
GB568054A (en) | Improvements in or relating to speed governors | |
GB808559A (en) | Improvements in or relating to pitch changing aeronautical propellers | |
US2843140A (en) | Hydraulic supply system for an aeronautical propeller or the like | |
GB983831A (en) | Improved liquid pressure supply system | |
GB1193930A (en) | Combined Hydraulic System for a Vehicle Transmission Mechanism and Power Steering Gear | |
GB586641A (en) | Improvements in or relating to hydraulic control devices | |
GB751361A (en) | Improvements in or relating to liquid fuel control systems particularly for gas turbine apparatus |