GB367880A - Improvements relating to aircraft - Google Patents
Improvements relating to aircraftInfo
- Publication number
- GB367880A GB367880A GB35147/30A GB3514730A GB367880A GB 367880 A GB367880 A GB 367880A GB 35147/30 A GB35147/30 A GB 35147/30A GB 3514730 A GB3514730 A GB 3514730A GB 367880 A GB367880 A GB 367880A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plane
- aircraft
- aeroplane
- replace
- fans
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
367,880. Supporting aircraft. WILLIAMS, G. M., 87, Lambs Conduit Street, London. Nov. 21, 1930, No. 35147. [Class 4.] Aircraft are provided with auxiliary supporting means comprising a plane and fans for forcing air in opposed directions into the space below the plane. As applied to an aeroplane, Fig. 1, the plane a is disposed symmetrically beneath the fuselage b. Oppositely rotating fans d are placed in housings in side walls c and are driven by electromotors d<1>. The plane is provided with end walls such as f pivoted at their upper edges and adjustable rearwardly positively or automatically against the restraint of springs. The front of the plane may be shaped to offer the minimum resistance in flight and may be slightly upwardly inclined. More than one such plane may be provided and may, in an aeroplane, replace the centre section of an upper plane or replace the lower plane of a biplane. According to the Provisional Specification the plane may be closed on the underside, and curved longitudinal surfaces may be fitted downwardly to direct the airflow.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB35147/30A GB367880A (en) | 1930-11-21 | 1930-11-21 | Improvements relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB35147/30A GB367880A (en) | 1930-11-21 | 1930-11-21 | Improvements relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB367880A true GB367880A (en) | 1932-02-22 |
Family
ID=10374373
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB35147/30A Expired GB367880A (en) | 1930-11-21 | 1930-11-21 | Improvements relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB367880A (en) |
-
1930
- 1930-11-21 GB GB35147/30A patent/GB367880A/en not_active Expired
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