GB1477490A - Helicopter rotor balde - Google Patents
Helicopter rotor baldeInfo
- Publication number
- GB1477490A GB1477490A GB2479274A GB2479274A GB1477490A GB 1477490 A GB1477490 A GB 1477490A GB 2479274 A GB2479274 A GB 2479274A GB 2479274 A GB2479274 A GB 2479274A GB 1477490 A GB1477490 A GB 1477490A
- Authority
- GB
- United Kingdom
- Prior art keywords
- helicopter rotor
- balde
- june
- comptroller
- heading
- 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
- 238000005516 engineering process Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/467—Aerodynamic features
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Hydraulic Turbines (AREA)
Abstract
1477490 Helicopter rotor blade UNITED TECHNOLOGIES CORP 4 June 1974 [4 June 1973] 24792/74 Heading B7W The subject-matter of this Specification is very similar to that described in Specification 1,391,940 but differs in respect of the negative twist of the blade tip portion, which in the present specification lies within the range of - 1 and - 8 degrees. Reference has been directed by the Comptroller to Specifications 1,391,939 and 1,391,940.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00366825A US3822105A (en) | 1971-09-22 | 1973-06-04 | Helicopter blade |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1477490A true GB1477490A (en) | 1977-06-22 |
Family
ID=23444705
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2479274A Expired GB1477490A (en) | 1973-06-04 | 1974-06-04 | Helicopter rotor balde |
Country Status (8)
Country | Link |
---|---|
JP (1) | JPS51116599A (en) |
BR (1) | BR7404568D0 (en) |
CA (1) | CA988906A (en) |
DE (1) | DE2426689A1 (en) |
FR (1) | FR2231565B1 (en) |
GB (1) | GB1477490A (en) |
IL (1) | IL44661A (en) |
IT (1) | IT1014735B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4331982A1 (en) * | 2022-08-31 | 2024-03-06 | Lockheed Martin Corporation | Method of stabilizing articulated rotor blade |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1538055A (en) * | 1975-05-19 | 1979-01-10 | Westland Aircraft Ltd | Helicopter rotor blades |
US4028003A (en) * | 1976-04-12 | 1977-06-07 | United Technologies Corporation | Torsionally compliant helicopter rotor blade with improved stability and performance characteristics |
FR2479132A1 (en) * | 1980-03-25 | 1981-10-02 | Aerospatiale | HIGH PERFORMANCE BLADE FOR HELICOPTER ROTOR |
DE102015121502A1 (en) | 2015-12-10 | 2017-06-14 | Christoph Fraundorfer | Gyroplane rotor blade for autorotatory lift generation |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3065933A (en) * | 1960-05-20 | 1962-11-27 | Frank Krause Jr A | Helicopter |
-
1974
- 1974-03-18 CA CA195,272A patent/CA988906A/en not_active Expired
- 1974-04-17 IL IL44661A patent/IL44661A/en unknown
- 1974-06-01 DE DE19742426689 patent/DE2426689A1/en not_active Ceased
- 1974-06-03 JP JP49062764A patent/JPS51116599A/en active Pending
- 1974-06-03 BR BR4568/74A patent/BR7404568D0/en unknown
- 1974-06-04 IT IT23551/74A patent/IT1014735B/en active
- 1974-06-04 GB GB2479274A patent/GB1477490A/en not_active Expired
- 1974-06-04 FR FR7419657A patent/FR2231565B1/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP4331982A1 (en) * | 2022-08-31 | 2024-03-06 | Lockheed Martin Corporation | Method of stabilizing articulated rotor blade |
Also Published As
Publication number | Publication date |
---|---|
FR2231565A1 (en) | 1974-12-27 |
JPS51116599A (en) | 1976-10-14 |
IT1014735B (en) | 1977-04-30 |
BR7404568D0 (en) | 1975-01-07 |
FR2231565B1 (en) | 1982-02-05 |
CA988906A (en) | 1976-05-11 |
IL44661A (en) | 1976-12-31 |
DE2426689A1 (en) | 1974-12-12 |
IL44661A0 (en) | 1974-09-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |