GB504849A - Improvements in and relating to airscrew blades - Google Patents
Improvements in and relating to airscrew bladesInfo
- Publication number
- GB504849A GB504849A GB3473437A GB3473437A GB504849A GB 504849 A GB504849 A GB 504849A GB 3473437 A GB3473437 A GB 3473437A GB 3473437 A GB3473437 A GB 3473437A GB 504849 A GB504849 A GB 504849A
- Authority
- GB
- United Kingdom
- Prior art keywords
- resin
- parts
- synthetic rubber
- bonding
- edges
- 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
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/24—Hollow blades
Abstract
504,849. Screw propellers. HIGH DUTY ALLOYS, Ltd., and PRYTHERCH, W. E. Dec. 16, 1937, No. 34734. [Class 114] A hollow air-screw is divided longitudinally into two or more parts each of which is a stamping, pressing or forging of light alloy, the parts being united by synthetic rubber or resin. The dish-shaped sections 1 and 2 are secured by a bonding-agent of synthetic rubber or resin. The edges of the parts are morticed or rebated 7 and 8 to form a lateral and longitudinal interlock. The blade may be bound with wire or tape 11, 12 and 13, along whole or part of its length and the edges are grooved 14 to position the wire. The thickness of the walls diminishes from root to tip and the whole assembly is sheathed with synthetic rubber or resin. The bonding-agent and sheathing is conveniently converted isoprene and polymerized butadiene.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3473437A GB504849A (en) | 1937-12-15 | 1937-12-15 | Improvements in and relating to airscrew blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3473437A GB504849A (en) | 1937-12-15 | 1937-12-15 | Improvements in and relating to airscrew blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB504849A true GB504849A (en) | 1939-05-02 |
Family
ID=10369314
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3473437A Expired GB504849A (en) | 1937-12-15 | 1937-12-15 | Improvements in and relating to airscrew blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB504849A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2454200A (en) * | 1944-10-16 | 1948-11-16 | Singer Mfg Co | Molded impeller |
US2596818A (en) * | 1947-05-08 | 1952-05-13 | Piasecki Helicopter Corp | Rotor blade |
-
1937
- 1937-12-15 GB GB3473437A patent/GB504849A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2454200A (en) * | 1944-10-16 | 1948-11-16 | Singer Mfg Co | Molded impeller |
US2596818A (en) * | 1947-05-08 | 1952-05-13 | Piasecki Helicopter Corp | Rotor blade |
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