GB9307662D0 - Construction of airfoils - Google Patents
Construction of airfoilsInfo
- Publication number
- GB9307662D0 GB9307662D0 GB939307662A GB9307662A GB9307662D0 GB 9307662 D0 GB9307662 D0 GB 9307662D0 GB 939307662 A GB939307662 A GB 939307662A GB 9307662 A GB9307662 A GB 9307662A GB 9307662 D0 GB9307662 D0 GB 9307662D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- airfoils
- construction
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/20—Integral or sandwich constructions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AUPL189692 | 1992-04-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9307662D0 true GB9307662D0 (en) | 1993-06-02 |
GB2266085A GB2266085A (en) | 1993-10-20 |
Family
ID=3776094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9307662A Withdrawn GB2266085A (en) | 1992-04-14 | 1993-04-14 | Aerofoil construction. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2266085A (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3823895A1 (en) * | 2018-07-16 | 2021-05-26 | BAE SYSTEMS plc | Wing structure |
EP3597529A1 (en) * | 2018-07-16 | 2020-01-22 | BAE SYSTEMS plc | Wing structure |
US20210362830A1 (en) * | 2020-05-21 | 2021-11-25 | The Boeing Company | Structural composite airfoils with an improved leading edge, and related methods |
US11554848B2 (en) | 2020-05-21 | 2023-01-17 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
US11572152B2 (en) * | 2020-05-21 | 2023-02-07 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
US11453476B2 (en) | 2020-05-21 | 2022-09-27 | The Boeing Company | Structural composite airfoils with an improved leading edge, and related methods |
US11401026B2 (en) | 2020-05-21 | 2022-08-02 | The Boeing Company | Structural composite airfoils with a single spar, and related methods |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2327393A1 (en) * | 1972-05-31 | 1973-12-13 | United Aircraft Corp | COMPOSITE HELICOPTER ROTOR BLADE |
WO1987001354A1 (en) * | 1985-09-04 | 1987-03-12 | Offshore Marine Pty. Ltd. | Airfoil construction |
-
1993
- 1993-04-14 GB GB9307662A patent/GB2266085A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2266085A (en) | 1993-10-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |