GB644178A - Improved fluid-pressure control system for variable pitch propellers - Google Patents
Improved fluid-pressure control system for variable pitch propellersInfo
- Publication number
- GB644178A GB644178A GB11201/48A GB1120148A GB644178A GB 644178 A GB644178 A GB 644178A GB 11201/48 A GB11201/48 A GB 11201/48A GB 1120148 A GB1120148 A GB 1120148A GB 644178 A GB644178 A GB 644178A
- Authority
- GB
- United Kingdom
- Prior art keywords
- valve
- pressure
- space
- pitch
- fluid
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Hydraulic Motors (AREA)
Abstract
644,178. Variable-pitch propellers. GENERAL MOTORS CORPORATION. April 23, 1948, No. 11201. Convention date, June 14, 1947. [Class 114] [Also in Group XXIX] A variable-pitch propeller operating motor has pressure fluid supplied to one side of it only, under the control of a speed governor valve, this fluid being also led to a leak orifice controller by a pressure controlled valve. A steady pitch is maintained by the governor valve 22 applying like pressure to the space 46 through the offset Y. This offset also allows fluid to pass to the space 112 below the valve 74, and also to the leak 160. Line pressure from the line 10, together with the spring 96 holds the valve 74 down and vents pressure through ports 152, 154. The reducing valve 161 supplies reduced pressure to the space 48. When increased pitch is required valve 22 moves upward, increasing pressure in space 112 lifting valve 74 and closing ports 152, 154. If pressure demand is great, land 102 also closes the passage 118 to the leak. Fluid from space 48 lifts valve 161 and escapes through slots 195. To decrease pitch, valve 22 descends, venting lead 42 through ports 226. The movement of the piston 50 lowers pressure in space 191, causing valve 161 to descend and supplying fluid from line 70 through ports 187 to line 44 to move piston 50 further.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US644178XA | 1947-06-14 | 1947-06-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB644178A true GB644178A (en) | 1950-10-04 |
Family
ID=22055846
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB11201/48A Expired GB644178A (en) | 1947-06-14 | 1948-04-23 | Improved fluid-pressure control system for variable pitch propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB644178A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3361058A1 (en) * | 2017-02-09 | 2018-08-15 | Safran Aero Boosters SA | Turbomachine compressor and corresponding turbomaschine |
-
1948
- 1948-04-23 GB GB11201/48A patent/GB644178A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3361058A1 (en) * | 2017-02-09 | 2018-08-15 | Safran Aero Boosters SA | Turbomachine compressor and corresponding turbomaschine |
BE1024982B1 (en) * | 2017-02-09 | 2018-09-10 | Safran Aero Boosters Sa | TURBOMACHINE COMPRESSOR WITH AUBES WITH VARIABLE SHIFT |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB644824A (en) | Improvements in or relating to governing devices for the control of hydraulic stabilising apparatus | |
US2667935A (en) | Aircraft propeller and engine control system | |
GB644178A (en) | Improved fluid-pressure control system for variable pitch propellers | |
US2621577A (en) | Cabin pressure change control | |
GB1289883A (en) | ||
GB1396472A (en) | Method of and apparatus for controlling the flow of fluids | |
GB980651A (en) | Automatic hovering gear for submarines | |
GB626549A (en) | Improvements relating to hydraulic governors | |
US2751919A (en) | Servo-motor control valve for an airplane engine | |
GB636150A (en) | Improvements in and relating to supercharger systems for aircraft cabins | |
GB674998A (en) | Aircraft flap control apparatus | |
GB588005A (en) | Improvements relating to hydraulic governors | |
GB959405A (en) | Aircraft for forward and vertical take-off and landing | |
GB672953A (en) | Improvements in or relating to hydraulic, variable-pitch propellers | |
GB672424A (en) | Improved variable pitch propeller control system | |
GB683906A (en) | Improvements in or relating to control units of variable pitch propellers | |
GB538326A (en) | Pressure controlling device for use in raising sunken ships by compressed air | |
GB708635A (en) | Improvements in and relating to adjustable relief valves | |
GB675413A (en) | Improvements in or relating to speed control means | |
GB724654A (en) | Improved propeller pitch control | |
GB710914A (en) | A device for the regulation of the driving engine for variable pitch propellers | |
GB666991A (en) | Improvements relating to hydraulically actuated speed governors | |
GB621671A (en) | Improvements in cabin pressure control systems for aircraft | |
SU400157A1 (en) | Pressure control system | |
GB191116362A (en) | Improvements in Speed Controlling Devices for Engines. |