GB486614A - Variable pitch airscrews - Google Patents
Variable pitch airscrewsInfo
- Publication number
- GB486614A GB486614A GB3527336A GB3527336A GB486614A GB 486614 A GB486614 A GB 486614A GB 3527336 A GB3527336 A GB 3527336A GB 3527336 A GB3527336 A GB 3527336A GB 486614 A GB486614 A GB 486614A
- Authority
- GB
- United Kingdom
- Prior art keywords
- ring
- cylinder
- hub
- springs
- flange
- 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
- B64C11/02—Hub construction
- B64C11/04—Blade mountings
- B64C11/06—Blade mountings for variable-pitch blades
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
486,614. Screw propellers. FAIRHURST, L. G. Dec. 23, 1936, No. 35273. [Class 114] Variable-pitch air screws in which a load is placed on the air-screw blades, away from the hub, in the direction in which centrifugal force operates, is characterized in that one or more springs are disposed between the blade root and the hub. The root of the blade A carries a flange F<1> and cylinder F in which is disposed a reversed cylinder G having a central spike G<3> and retaining nut G4. Between these two telescopic cylinders are springs G<1>. The base of the cylinder G is formed with a spherical surface engaging a corresponding surface on a flange H secured to shaft H<2>. The studs E<3> for holding the ring F<1> in place are continued, and support a plate E<2> having outer castellations which act as a lock for a final securing ring E<1> on the assembly. The latter ring holds in place a ring E which carries the part D<3> that is coupled to the pitch varying mechanism.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3527336A GB486614A (en) | 1936-12-23 | 1936-12-23 | Variable pitch airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3527336A GB486614A (en) | 1936-12-23 | 1936-12-23 | Variable pitch airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB486614A true GB486614A (en) | 1938-06-08 |
Family
ID=10375851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3527336A Expired GB486614A (en) | 1936-12-23 | 1936-12-23 | Variable pitch airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB486614A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2420424A (en) * | 1942-02-18 | 1947-05-13 | Everel Propeller Corp | Hub construction |
US2425938A (en) * | 1943-09-15 | 1947-08-19 | Walter S Hoover | Circulating ball race propeller blade bearing |
US2514477A (en) * | 1945-06-11 | 1950-07-11 | Curtiss Wright Corp | Variable pitch propeller |
US2515996A (en) * | 1942-04-29 | 1950-07-18 | Everel Propeller Corp | Propeller blade mounting |
US2530520A (en) * | 1946-09-17 | 1950-11-21 | Everel Propeller Corp | Propeller hub |
US2533358A (en) * | 1945-06-11 | 1950-12-12 | Curtiss Wright Corp | Variable pitch propeller |
US2533415A (en) * | 1943-02-04 | 1950-12-12 | United Aircraft Corp | Variable pitch propeller |
US2566696A (en) * | 1947-01-15 | 1951-09-04 | Curtiss Wright Corp | Roller track mounting of a variable pitch propeller |
US2623601A (en) * | 1950-03-14 | 1952-12-30 | United Aircraft Corp | Propeller blade preloading and fluid transfer mechanism |
US2704129A (en) * | 1951-03-23 | 1955-03-15 | Curtiss Wright Corp | Blade retention for aircraft propeller |
GB2518643A (en) * | 2013-09-26 | 2015-04-01 | Ge Aviat Systems Ltd | Propeller assembly and propeller blade retention assembly |
-
1936
- 1936-12-23 GB GB3527336A patent/GB486614A/en not_active Expired
Cited By (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2420424A (en) * | 1942-02-18 | 1947-05-13 | Everel Propeller Corp | Hub construction |
US2515996A (en) * | 1942-04-29 | 1950-07-18 | Everel Propeller Corp | Propeller blade mounting |
US2533415A (en) * | 1943-02-04 | 1950-12-12 | United Aircraft Corp | Variable pitch propeller |
US2425938A (en) * | 1943-09-15 | 1947-08-19 | Walter S Hoover | Circulating ball race propeller blade bearing |
US2514477A (en) * | 1945-06-11 | 1950-07-11 | Curtiss Wright Corp | Variable pitch propeller |
US2533358A (en) * | 1945-06-11 | 1950-12-12 | Curtiss Wright Corp | Variable pitch propeller |
US2530520A (en) * | 1946-09-17 | 1950-11-21 | Everel Propeller Corp | Propeller hub |
US2566696A (en) * | 1947-01-15 | 1951-09-04 | Curtiss Wright Corp | Roller track mounting of a variable pitch propeller |
US2623601A (en) * | 1950-03-14 | 1952-12-30 | United Aircraft Corp | Propeller blade preloading and fluid transfer mechanism |
US2704129A (en) * | 1951-03-23 | 1955-03-15 | Curtiss Wright Corp | Blade retention for aircraft propeller |
GB2518643A (en) * | 2013-09-26 | 2015-04-01 | Ge Aviat Systems Ltd | Propeller assembly and propeller blade retention assembly |
CN104512547A (en) * | 2013-09-26 | 2015-04-15 | 通用电气航空系统有限公司 | Propeller assembly and propeller blade retention assembly for aircrafts |
GB2518643B (en) * | 2013-09-26 | 2016-06-08 | Ge Aviat Systems Ltd | Propeller assembly and propeller blade retention assembly |
CN104512547B (en) * | 2013-09-26 | 2017-04-12 | 通用电气航空系统有限公司 | Propeller assembly for aircrafts |
CN107054642A (en) * | 2013-09-26 | 2017-08-18 | 通用电气航空系统有限公司 | Propeller component and propeller blade for aircraft keep component |
US9764821B2 (en) | 2013-09-26 | 2017-09-19 | Ge Aviation Systems Limited | Propeller assembly and propeller blade retention assembly |
CN107054642B (en) * | 2013-09-26 | 2020-03-20 | 通用电气航空系统有限公司 | Propeller blade retention assembly |
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