GB452053A - Improvements in and relating to aircraft - Google Patents
Improvements in and relating to aircraftInfo
- Publication number
- GB452053A GB452053A GB6103/35A GB610335A GB452053A GB 452053 A GB452053 A GB 452053A GB 6103/35 A GB6103/35 A GB 6103/35A GB 610335 A GB610335 A GB 610335A GB 452053 A GB452053 A GB 452053A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vanes
- plane
- screws
- transverse
- bevel
- 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
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Motorcycle And Bicycle Frame (AREA)
Abstract
452,053. Flying-machines. MALCOLM, A., 66, South Street, Perth. Feb. 26, 1935, No. 6103. [Class 4] A flying-machine comprises a louvred plane of snow-shoe-like outline beneath which is suspended propelling gear comprising air screws adapted to be swivelled about a transverse axis to act either as tractor or as helicopter screws. The plane includes a peripheral frame A, Figs. 1 and 2, and cross members B<1> to B<5>. C<1> and C<2> are front and rear elevators. Longitudinal vanes E are hinged to the cross members and transverse vanes F are hinged to fore-andaft stays. A chassis frame comprises uprights D<1> and bottom rails D<2> ; the latter support propelling mechanism comprising front and rear pairs of air screws G driven by bevel gearing from transverse shafts, Fig. 4. The bevel gear housings may be rotated to alter the line of action of the air screws by lever-androd mechanism actuated by either of two hand levers P<1>, <p2>. Landing legs L are attached to the bevel drive housings. Fluted rudders K<1>, K<2> are provided. Look-out apertures R<1>, R<2> are formed in the plane. The control levers work in gates such that vanes F may be locked in position without preventing control of vanes E.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB6103/35A GB452053A (en) | 1935-02-26 | 1935-02-26 | Improvements in and relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB6103/35A GB452053A (en) | 1935-02-26 | 1935-02-26 | Improvements in and relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB452053A true GB452053A (en) | 1936-08-17 |
Family
ID=9808426
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB6103/35A Expired GB452053A (en) | 1935-02-26 | 1935-02-26 | Improvements in and relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB452053A (en) |
-
1935
- 1935-02-26 GB GB6103/35A patent/GB452053A/en not_active Expired
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