GB1267571A - Rotor blade and propeller blade mountings - Google Patents
Rotor blade and propeller blade mountingsInfo
- Publication number
- GB1267571A GB1267571A GB1564369A GB1564369A GB1267571A GB 1267571 A GB1267571 A GB 1267571A GB 1564369 A GB1564369 A GB 1564369A GB 1564369 A GB1564369 A GB 1564369A GB 1267571 A GB1267571 A GB 1267571A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- mountings
- fibre
- march
- pins
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C27/48—Root attachment to rotor head
Abstract
1,267,571. Helicopter rotor mountings; propellers. ZAKLAD DOSWIADCZALNY PRZYWYTWORNI SPRZETU KOMUNIKACYJNEGO. 25 March, 1969 [28 March, 1968], No. 15643/69. Headings B7V and B7W. A joint between an aircraft propeller blade or a helicopter main rotor blade and a root end fitting 11 includes a spar core 1 which is reinforced by flanged bushes 5 and 6 embedded in a plastics material filling space 8, and is enfolded by layers of fibre-glass cloth 2 wound so as to form a suitable cavity for bundles of load carrying fibres 7. The load carrying fibres 7 improve the transmission of loads from the blade skin to the bushes 5 and 6 and thence to pins 9 and 10. Several layers of fibre-glass cloth 3 are diagonally laid over bundles 7 and cloth 2 to improve transmission of twisting moments. The root end fitting 11 is held to the blade by the pins 9 and 10 and nuts 15.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL12607168 | 1968-03-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1267571A true GB1267571A (en) | 1972-03-22 |
Family
ID=19949941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1564369A Expired GB1267571A (en) | 1968-03-28 | 1969-03-25 | Rotor blade and propeller blade mountings |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2004934A1 (en) |
GB (1) | GB1267571A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2218473A (en) * | 1988-05-10 | 1989-11-15 | Mtu Muenchen Gmbh | Composite propeller blade |
CN103241367A (en) * | 2012-02-09 | 2013-08-14 | 奥格斯塔韦斯兰股份公司 | Aircraft rotor blade and relative forming method |
CN108069031A (en) * | 2016-11-14 | 2018-05-25 | 昌河飞机工业(集团)有限责任公司 | A kind of structure and assembly technology of blade jointing |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2620178B1 (en) * | 1987-09-09 | 1990-01-19 | Aerospatiale | SOCKET FASTENER, AND ROTOR BLADE PROVIDED WITH SUCH A HUB FASTENER |
-
1969
- 1969-03-25 GB GB1564369A patent/GB1267571A/en not_active Expired
- 1969-03-26 FR FR6908935A patent/FR2004934A1/en not_active Withdrawn
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2218473A (en) * | 1988-05-10 | 1989-11-15 | Mtu Muenchen Gmbh | Composite propeller blade |
US4944655A (en) * | 1988-05-10 | 1990-07-31 | Mtu Motoren- Und Turbinen-Union Munich Gmbh | Propeller blade of a fiber-reinforced plastic material |
GB2218473B (en) * | 1988-05-10 | 1992-07-15 | Mtu Muenchen Gmbh | Propeller blade of fibre-reinforced plastics material |
CN103241367A (en) * | 2012-02-09 | 2013-08-14 | 奥格斯塔韦斯兰股份公司 | Aircraft rotor blade and relative forming method |
EP2626298A1 (en) * | 2012-02-09 | 2013-08-14 | AGUSTAWESTLAND S.p.A. | Aircraft rotor blade and relative forming method |
EP2634089A1 (en) * | 2012-02-09 | 2013-09-04 | Agustawestland S.p.A. | Aircraft rotor blade and relative forming method |
US9441492B2 (en) | 2012-02-09 | 2016-09-13 | Agustawestland S.P.A. | Aircraft rotor blade and relative forming method |
CN108069031A (en) * | 2016-11-14 | 2018-05-25 | 昌河飞机工业(集团)有限责任公司 | A kind of structure and assembly technology of blade jointing |
Also Published As
Publication number | Publication date |
---|---|
DE1916120B2 (en) | 1976-07-29 |
FR2004934A1 (en) | 1969-12-05 |
DE1916120A1 (en) | 1969-10-02 |
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