GB580745A - Improvements in or relating to variable pitch propeller systems - Google Patents
Improvements in or relating to variable pitch propeller systemsInfo
- Publication number
- GB580745A GB580745A GB16723/43A GB1672343A GB580745A GB 580745 A GB580745 A GB 580745A GB 16723/43 A GB16723/43 A GB 16723/43A GB 1672343 A GB1672343 A GB 1672343A GB 580745 A GB580745 A GB 580745A
- Authority
- GB
- United Kingdom
- Prior art keywords
- worm
- shaft
- wheel
- drives
- carrying
- 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
- B64C11/44—Blade pitch-changing mechanisms electric
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
580,745. Variable pitch propellers. FAIREY AVIATION CO., Ltd. Oct. 12, 1943, No. 16723. Convention date, Jan. 19. [Class 114] A self-contained unit for mounting on the propeller drive shaft 4 of an aircraft engine 2 comprises a housing 14 carrying a governor 96 driven by the engine for actuating switches or the like controlling a reversible electric or hydraulic motor 72 driving gearing for varying the pitch of the blades 37. Two such units may be applied to contra-rotating propellers mounted on coaxial drive shafts. In the form shown, the housing 14 has a flange 10 secured by nuts 12 and bolts 8 on a front facing 6 of the engine 2. Keyed to the shaft 4 is a ring member 16 to which the hub sleeve 20 is secured by a lock nut 28 and wedge collets 18, 22. The gearing includes a spider 58 continuously rotated in the same. direction by the shaft 4 but at a lower speed. The electric motor 72 is geared to a shaft 70 carrying a worm 68 which rotates a ring gear-wheel 66 which, through pinions 56, drives a large ring gear-wheel 52 geared to annular worm-wheels 38 for rotating the blades 37 about their longitudinal axes. The gear-wheel 66 also drives through a spur gear 108, a worm 110, and a worm-wheel 112, a shaft 114 carrying cams 80, 82, 84 which control switches of the regulating system described in Specification 564,221. The member 16 also carries worm teeth 118 which' engage a worm 120 on a shaft 122, one end of which drives the governor 96 whilst the other end drives a de-icing pump 124. Specification 580,488 also is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US580745XA | 1943-01-19 | 1943-01-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB580745A true GB580745A (en) | 1946-09-18 |
Family
ID=22014507
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16723/43A Expired GB580745A (en) | 1943-01-19 | 1943-10-12 | Improvements in or relating to variable pitch propeller systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB580745A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103661927A (en) * | 2013-12-13 | 2014-03-26 | 左承龙 | Variable pitch propeller of fixed-wing aircraft |
CN112298532A (en) * | 2019-07-26 | 2021-02-02 | 哈米尔顿森德斯特兰德公司 | Pitch variation and control of electric blades of an aircraft propeller |
-
1943
- 1943-10-12 GB GB16723/43A patent/GB580745A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103661927A (en) * | 2013-12-13 | 2014-03-26 | 左承龙 | Variable pitch propeller of fixed-wing aircraft |
CN103661927B (en) * | 2013-12-13 | 2016-03-02 | 左承龙 | A kind of fixed wing aircraft nonuniform pitch propeller |
CN112298532A (en) * | 2019-07-26 | 2021-02-02 | 哈米尔顿森德斯特兰德公司 | Pitch variation and control of electric blades of an aircraft propeller |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3360217A (en) | Duct rotation system for vtol aircraft | |
GB1461069A (en) | Aircraft with variable diameter rotors | |
GB531756A (en) | Device employing epicyclic or bevel gears or a combination of both for controlling the pitch of variable pitch airscrews | |
GB666491A (en) | Improvements in or relating to aircraft | |
GB580745A (en) | Improvements in or relating to variable pitch propeller systems | |
US2403899A (en) | Propeller pitch and diameter control | |
GB587242A (en) | Improvements in or relating to apparatus for operating a ship's variable pitch propeller | |
GB569056A (en) | Improvements in marine screw propellers of the variable pitch and reversing type | |
US2351219A (en) | Gearing | |
US2389161A (en) | Controllable pitch change mechanism for dual rotation propellers | |
GB580923A (en) | Improvements in or relating to variable pitch propellers | |
US2427982A (en) | Helicopter antitorque and steering control | |
GB627847A (en) | Improvements in or relating to apparatus for adjusting the pitch of aircraft propellers | |
GB597931A (en) | Improvements in pitch changing mechanisms for screw propellers | |
GB546995A (en) | Improvements in variable pitch airscrews | |
US2577604A (en) | Propeller pitch changing mechanism | |
US2437189A (en) | Self-contained unit for variable pitch propellers | |
GB554665A (en) | Improvements in or relating to co-axial oppositely rotating airscrews | |
GB559165A (en) | Improvements in and relating to propulsion installations for aircraft | |
GB580488A (en) | Improvements in or relating to variable pitch propeller systems | |
GB544570A (en) | Improvements relating to variable-pitch airscrews | |
US2372667A (en) | Variable speed means for variable pitch propeller systems | |
US2589853A (en) | Aircraft power plant having two or more gas turbine power units to drive one or more airscrews in various combinations | |
US2455000A (en) | Electrically operated pitch changing mechanism | |
GB490747A (en) | Improvements in or relating to oppositely rotating coaxial propellers |