DE1431148A1 - Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln - Google Patents
Vorrichtung zum Beiklappen von HubschrauberdrehfluegelnInfo
- Publication number
- DE1431148A1 DE1431148A1 DE19641431148 DE1431148A DE1431148A1 DE 1431148 A1 DE1431148 A1 DE 1431148A1 DE 19641431148 DE19641431148 DE 19641431148 DE 1431148 A DE1431148 A DE 1431148A DE 1431148 A1 DE1431148 A1 DE 1431148A1
- Authority
- DE
- Germany
- Prior art keywords
- folding
- rotating wings
- helicopter rotating
- helicopter
- wings
- 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.)
- Pending
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
- B64C27/50—Blades foldable to facilitate stowage of aircraft
Description
Claims (1)
- Patentansprüche
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US309809A US3247907A (en) | 1963-09-18 | 1963-09-18 | Blade folding mechanism for rotary wing aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1431148A1 true DE1431148A1 (de) | 1969-07-31 |
Family
ID=23199745
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19641431148 Pending DE1431148A1 (de) | 1963-09-18 | 1964-09-03 | Vorrichtung zum Beiklappen von Hubschrauberdrehfluegeln |
Country Status (3)
Country | Link |
---|---|
US (1) | US3247907A (de) |
DE (1) | DE1431148A1 (de) |
GB (1) | GB1036028A (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3484175A (en) * | 1967-10-12 | 1969-12-16 | United Aircraft Corp | Means and method of synchronously folding helicopter blades |
US3438447A (en) * | 1967-10-12 | 1969-04-15 | United Aircraft Corp | Dual linear output and dual rotary output actuator with redundant drive |
US3749515A (en) * | 1971-06-01 | 1973-07-31 | Textron Inc | Powered folding mechanism |
US4284387A (en) * | 1979-05-02 | 1981-08-18 | United Technologies Corp. | Blade fold restraint system |
DE3272187D1 (en) * | 1981-11-19 | 1986-08-28 | Westland Plc | Helicopter rotors |
US5031858A (en) * | 1989-11-20 | 1991-07-16 | Bell Helicopter Textron, Inc. | Apparatus and method for folding and locking rotor blades |
US5322415A (en) * | 1992-11-18 | 1994-06-21 | United Technologies Corporation | Pitch actuation system restraint device for a helicopter blade folding system |
US5868351A (en) * | 1996-05-23 | 1999-02-09 | Bell Helicopter Textron Inc. | Rotor blade stowing system |
US20120134821A1 (en) * | 2010-11-28 | 2012-05-31 | Bruce Eugene Swanson | Fluid Turbine Having Improved Cam and Follower Mechanism |
US10301015B2 (en) * | 2014-08-21 | 2019-05-28 | Sikorsky Aircraft Corporation | System for shimming blade fold angle about an axis of rotation |
US11511848B2 (en) * | 2020-05-20 | 2022-11-29 | Textron Innovations Inc. | Pitch-fold lock |
CN114193989B (zh) * | 2021-12-29 | 2024-02-20 | 广东汇天航空航天科技有限公司 | 折叠机构、折叠机翼以及飞行器 |
CN115056964B (zh) * | 2022-03-16 | 2024-04-12 | 南京理工大学 | 一种用于空天飞行器内置式电液伺服驱动折翼机构 |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB852841A (en) * | 1957-12-10 | 1960-11-02 | Westland Aircraft Ltd | Improvements in or relating to rotary wing aircraft |
US3153455A (en) * | 1962-10-15 | 1964-10-20 | Boeing Co | Folding mechanism |
-
1963
- 1963-09-18 US US309809A patent/US3247907A/en not_active Expired - Lifetime
-
1964
- 1964-09-02 GB GB36029/64A patent/GB1036028A/en not_active Expired
- 1964-09-03 DE DE19641431148 patent/DE1431148A1/de active Pending
Also Published As
Publication number | Publication date |
---|---|
GB1036028A (en) | 1966-07-13 |
US3247907A (en) | 1966-04-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
SH | Request for examination between 03.10.1968 and 22.04.1971 |