GB430557A - Improvements in and relating to variable pitch propellers - Google Patents
Improvements in and relating to variable pitch propellersInfo
- Publication number
- GB430557A GB430557A GB26974/34A GB2697434A GB430557A GB 430557 A GB430557 A GB 430557A GB 26974/34 A GB26974/34 A GB 26974/34A GB 2697434 A GB2697434 A GB 2697434A GB 430557 A GB430557 A GB 430557A
- Authority
- GB
- United Kingdom
- Prior art keywords
- racks
- members
- pitch
- move
- rack
- 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
- B64C11/32—Blade pitch-changing mechanisms mechanical
- B64C11/325—Blade pitch-changing mechanisms mechanical comprising feathering, braking or stopping systems
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
430,557. Screw propellers. LAFOND, G., 56, Rue Notre Dame de Lorette, Paris. Sept. 19, 1934, No. 26974. Convention date, Sept. 19, 1933. [Class 114] Variable-pitch screw propellers provided with mechanism for altering the pitch and with an independent locking device have two connecting members between the non-rotating part of the adjustment means and the part rotated with the propeller and these are engaged only when the pitch is being altered, but disengaged during normal operation. The blade roots carry pinions 4, 4<1> engaged by racks 5, 51 which are locked by means of segments 7, 7<1> which co-operate with members 9, 91. Normally, a spring-urged block 10 holds the parts 9, 91 and so locks the racks with the members 7. When it is desired to move the racks to change pitch the block 10 is slidden endwise, the members 9, 9<1> move outwardly under centrifugal force to release the racks. In an alternative form the racks are carried by bars 15 pivoted at 16, these bars being connected by links 17 on a member 19<1> capable of being slidden by a cam arm 20. Normally, the rack member is in engagement with the locking member 7. When it is desired to move the rack by means of the member 13, the handle 21 is turned and the links 17 tilt the rack bar free from the locking member. Instead of the blade roots having interengaging pinions those members may be made segmental so that the part engaging the racks has a different pitch radius from the interengaging parts. Where more than two blades are employed they are intercoupled with each other by gearing and each is provided with an adjustment mechanism.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR430557X | 1933-09-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB430557A true GB430557A (en) | 1935-06-20 |
Family
ID=8899291
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB26974/34A Expired GB430557A (en) | 1933-09-19 | 1934-09-19 | Improvements in and relating to variable pitch propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB430557A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USB353387I5 (en) * | 1972-04-19 | 1975-01-28 | ||
CN112550688A (en) * | 2020-12-16 | 2021-03-26 | 范家铭 | Coaxial helicopter and rotor system thereof |
IT202200022992A1 (en) * | 2022-11-08 | 2024-05-08 | Ge Avio S R L | VARIABLE PITCH PROPELLER OF A GAS TURBINE ENGINE |
-
1934
- 1934-09-19 GB GB26974/34A patent/GB430557A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USB353387I5 (en) * | 1972-04-19 | 1975-01-28 | ||
US3924404A (en) * | 1972-04-19 | 1975-12-09 | Mtu Muenchen Gmbh | Apparatus for adjusting fan blades in a turbojet engine |
CN112550688A (en) * | 2020-12-16 | 2021-03-26 | 范家铭 | Coaxial helicopter and rotor system thereof |
IT202200022992A1 (en) * | 2022-11-08 | 2024-05-08 | Ge Avio S R L | VARIABLE PITCH PROPELLER OF A GAS TURBINE ENGINE |
US12110903B2 (en) | 2022-11-08 | 2024-10-08 | Ge Avio S.R.L. | Variable pitch fan of a gas turbine engine |
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