GB630796A - Improvements to aircrafts of the all-wing type - Google Patents
Improvements to aircrafts of the all-wing typeInfo
- Publication number
- GB630796A GB630796A GB3725/47A GB372547A GB630796A GB 630796 A GB630796 A GB 630796A GB 3725/47 A GB3725/47 A GB 3725/47A GB 372547 A GB372547 A GB 372547A GB 630796 A GB630796 A GB 630796A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- convex
- feb
- plan
- aircrafts
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/10—All-wing aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air-Flow Control Members (AREA)
Abstract
630,796. All-wing aircraft. FAUCHIER, R. L. Feb. 7, 1947, No. 3725. Convention date, Feb. 20, 1946. [Class 4] , An all-wing aircraft has in plan view, Fig. 2, the shape of an isosceles paralellogram which has its shorter base at the front and preferably a height such as to give the wing an aspect ratio of less than 0.5. The side edges of the wing are formed by substantially rectangular section bulges 6, Fig. 3, with their upper edges 7 raised above the surface of the mid-part of the wing 5, thereby providing a central guide passage for the airstream around the root of the fin 8 and rudder 9. The aerofoil section of the wing is part convex and part concave at the upper surface and wholly convex at the lower surface. In the Specification, as open to inspection under Sect. 91 the leading edge of the wing plan as then shown in Fig. 2, was substantially semi-circular, and the underside of the crosssection, Fig. 3, was made slightly convex. This subject-matter does not appear in the Specification as accepted.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR630796X | 1946-02-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB630796A true GB630796A (en) | 1949-10-21 |
Family
ID=8991333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3725/47A Expired GB630796A (en) | 1946-02-20 | 1947-02-07 | Improvements to aircrafts of the all-wing type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB630796A (en) |
-
1947
- 1947-02-07 GB GB3725/47A patent/GB630796A/en not_active Expired
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