GB264603A - Improved method for mounting the blades of an aircraft propeller - Google Patents
Improved method for mounting the blades of an aircraft propellerInfo
- Publication number
- GB264603A GB264603A GB2711025A GB2711025A GB264603A GB 264603 A GB264603 A GB 264603A GB 2711025 A GB2711025 A GB 2711025A GB 2711025 A GB2711025 A GB 2711025A GB 264603 A GB264603 A GB 264603A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- sockets
- mounting
- improved method
- screw
- 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
- B64C11/065—Blade mountings for variable-pitch blades variable only when stationary
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
264,603. Morton, F. C. Oct. 29, 1925. Screw propellers.-In an airscrew of the kind wherein the hub consists of two half sockets internally serrated to receive the roots of the blades, the blade roots external to the sockets are screwed to take a locking nut which takes up against the machined ends of the sockets. The hub is formed of two parts 1, 2, each having two half sockets 10, 11, which are held together by bolts 9 and also by a central nut 5 which is secured on to the central sleeve 3 of the main part 1. The blades 14 have a shoulder 16, serrations 19 and an external screw .18.. A lock nut 17 on this screw bears against the end of the socket.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2711025A GB264603A (en) | 1925-10-29 | 1925-10-29 | Improved method for mounting the blades of an aircraft propeller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2711025A GB264603A (en) | 1925-10-29 | 1925-10-29 | Improved method for mounting the blades of an aircraft propeller |
Publications (1)
Publication Number | Publication Date |
---|---|
GB264603A true GB264603A (en) | 1927-01-27 |
Family
ID=10254347
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2711025A Expired GB264603A (en) | 1925-10-29 | 1925-10-29 | Improved method for mounting the blades of an aircraft propeller |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB264603A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2542465A (en) * | 2015-07-13 | 2017-03-22 | Ge Aviation Systems Llc | Hub assembly and propeller assemblies |
-
1925
- 1925-10-29 GB GB2711025A patent/GB264603A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2542465A (en) * | 2015-07-13 | 2017-03-22 | Ge Aviation Systems Llc | Hub assembly and propeller assemblies |
US10137980B2 (en) | 2015-07-13 | 2018-11-27 | Ge Aviation Systems Llc | Hub assembly and propeller assemblies |
GB2542465B (en) * | 2015-07-13 | 2019-06-05 | Ge Aviation Systems Llc | Propeller assemblies with a partial hub |
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