GB537451A - Improvements in or relating to spinners for airscrews - Google Patents
Improvements in or relating to spinners for airscrewsInfo
- Publication number
- GB537451A GB537451A GB613940A GB613940A GB537451A GB 537451 A GB537451 A GB 537451A GB 613940 A GB613940 A GB 613940A GB 613940 A GB613940 A GB 613940A GB 537451 A GB537451 A GB 537451A
- Authority
- GB
- United Kingdom
- Prior art keywords
- key
- airscrews
- spinners
- hub
- pin
- 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
- B64C11/14—Spinners
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Centrifugal Separators (AREA)
- Testing Of Balance (AREA)
Abstract
537,451. Airscrew spinners. CONSTANT SPEED AIRSCREWS, Ltd., and MARSHALL, F. G. April 5, 1940, No. 6139. [Class 114] The spinner shell a is supported at the front and/or rear of the hub by spoked members d, e, radiating from the hub k and terminating in pin and socket connections f between which rubber bushes may be interposed. The spinner shell may be detachably secured by pin and key-hole connections and for this purpose a locking-ring s may be employed which may be moved in and out of its operative position by a key w. A spring u securing the locking ring in operative positions is thrust aside by the insertion of the key. Specifications 451,553 and 485,903 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB613940A GB537451A (en) | 1940-04-05 | 1940-04-05 | Improvements in or relating to spinners for airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB613940A GB537451A (en) | 1940-04-05 | 1940-04-05 | Improvements in or relating to spinners for airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB537451A true GB537451A (en) | 1941-06-23 |
Family
ID=9809133
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB613940A Expired GB537451A (en) | 1940-04-05 | 1940-04-05 | Improvements in or relating to spinners for airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB537451A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8529204B2 (en) | 2008-02-26 | 2013-09-10 | Rolls-Royce Plc | Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction |
-
1940
- 1940-04-05 GB GB613940A patent/GB537451A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8529204B2 (en) | 2008-02-26 | 2013-09-10 | Rolls-Royce Plc | Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction |
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