GB547433A - Improvements in or relating to spinners for airscrew hubs - Google Patents
Improvements in or relating to spinners for airscrew hubsInfo
- Publication number
- GB547433A GB547433A GB257741A GB257741A GB547433A GB 547433 A GB547433 A GB 547433A GB 257741 A GB257741 A GB 257741A GB 257741 A GB257741 A GB 257741A GB 547433 A GB547433 A GB 547433A
- Authority
- GB
- United Kingdom
- Prior art keywords
- bosses
- shell
- airscrew
- secured
- support plate
- 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)
Abstract
547,433. Air screw spinner, made of synthetic resin. COVERLEY, R. H., and BROWN, D. W. Feb. 25, 1941, No.2577. [Class 2 (iii)] [Also in Group XXXIII] The shell 10 of an airscrew spinner is made of reinforced plastic material and is moulded in one piece with means on its inner surface for securing flanged or like members to it. The material may be synthetic resin rein forced with laminated fabric, felt, paper, or flaked scraps of fabric, and the securing means may comprise spaced bosses 13. A flanged ring 14 secured to the bosses 13 engages the front-support plate 18 of the hub, whilst a second ring 21, secured to the shell by means of similar bosses or by screws passing through the shell, is locked by bosses 20 to the rear support plate 19. The parts 12, 14, 18, 19, 21 also may be made of reinforced plastic material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB257741A GB547433A (en) | 1941-02-25 | 1941-02-25 | Improvements in or relating to spinners for airscrew hubs |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB257741A GB547433A (en) | 1941-02-25 | 1941-02-25 | Improvements in or relating to spinners for airscrew hubs |
Publications (1)
Publication Number | Publication Date |
---|---|
GB547433A true GB547433A (en) | 1942-08-27 |
Family
ID=9742015
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB257741A Expired GB547433A (en) | 1941-02-25 | 1941-02-25 | Improvements in or relating to spinners for airscrew hubs |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB547433A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2765858A (en) * | 1952-11-04 | 1956-10-09 | Leland E Hardy | Model airplane propeller hub and cowl construction |
JP2001349248A (en) * | 2000-03-24 | 2001-12-21 | General Electric Co <Ge> | Composite spinner and its method of manufacture |
US20080022524A1 (en) * | 2006-03-10 | 2008-01-31 | Karl Schreiber | Intake cone in a fiber compound material for a gas turbine engine and method for its manufacture |
-
1941
- 1941-02-25 GB GB257741A patent/GB547433A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2765858A (en) * | 1952-11-04 | 1956-10-09 | Leland E Hardy | Model airplane propeller hub and cowl construction |
JP2001349248A (en) * | 2000-03-24 | 2001-12-21 | General Electric Co <Ge> | Composite spinner and its method of manufacture |
EP1136353A3 (en) * | 2000-03-24 | 2003-01-15 | General Electric Company | Composite spinner and method of making the same |
US20080022524A1 (en) * | 2006-03-10 | 2008-01-31 | Karl Schreiber | Intake cone in a fiber compound material for a gas turbine engine and method for its manufacture |
US8677622B2 (en) * | 2006-03-10 | 2014-03-25 | Rolls-Royce Deutschland Ltd & Co Kg | Intake cone in a fiber compound material for a gas turbine engine and method for its manufacture |
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