GB785633A - Improvements in aircraft having a variable wing area - Google Patents
Improvements in aircraft having a variable wing areaInfo
- Publication number
- GB785633A GB785633A GB32264/55A GB3226455A GB785633A GB 785633 A GB785633 A GB 785633A GB 32264/55 A GB32264/55 A GB 32264/55A GB 3226455 A GB3226455 A GB 3226455A GB 785633 A GB785633 A GB 785633A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- fuselage
- aircraft
- nov
- carries
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
Abstract
785,633. Aircraft wings. HUREL, M. L. Nov. 11, 1955 [Nov. 13, 1954], No. 32264/55. Class 4. A jet propelled aircraft provided with a thin fixed wing for high speed flight has an auxiliary high lift wing 6 for use during low speed flight which is normally housed within the fuselage 1 in the position shown by chain dotted lines and for use, is rotated about a ball-and-socket pivot 13, 15 to the position shown by full lines. The opening 7 in the fuselage to accommodate the wing is closed by flaps (not shown) and the wing carries a circular structure 14 which is slotted at 18 to receive supporting lugs 17 mounted on a framework 14, 19 within the fuselage. The structure 16 carries a toothed ring 22 engaged by the pinion 21 of an electric motor 20 for retraction of the wing 6.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR785633X | 1954-11-13 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB785633A true GB785633A (en) | 1957-10-30 |
Family
ID=9217948
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32264/55A Expired GB785633A (en) | 1954-11-13 | 1955-11-11 | Improvements in aircraft having a variable wing area |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB785633A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2434783A (en) * | 2006-02-01 | 2007-08-08 | Sam Proctor | Aircraft with folded wings |
-
1955
- 1955-11-11 GB GB32264/55A patent/GB785633A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2434783A (en) * | 2006-02-01 | 2007-08-08 | Sam Proctor | Aircraft with folded wings |
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