GB360275A - Improvements in or relating to heavier than air aircraft - Google Patents
Improvements in or relating to heavier than air aircraftInfo
- Publication number
- GB360275A GB360275A GB154731A GB154731A GB360275A GB 360275 A GB360275 A GB 360275A GB 154731 A GB154731 A GB 154731A GB 154731 A GB154731 A GB 154731A GB 360275 A GB360275 A GB 360275A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- engine
- propeller
- propellers
- screw
- 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
- B64C3/385—Variable incidence wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Abstract
360,275. Aircraft. MUSS, W., 34, Deitersen, Kreis Einbeck, Hanover, Germany. Jan. 16, 1931, No. 1547. [Class 4.] An aircraft having an engine 18, propeller 15 and lifting-screw 17 at its front end has three planes on each side of the body which are transversely arched and tiltable about transverse shafts 2, 3, 4, each successive plane' being of greater chord than the preceding one, while an engine and propeller 11, 13, 12, 14 are provided below or in front of each of the foremost planes. The body is of the section shown in Fig. 1, the inner edges of the planes continuing the lower sides 28. The lifting-screw 17 is inclined as shown and driven from the engine 18. A similar lifting-screw 29 may be mounted at the rear end and driven from an engine which also drives a propeller 32 which is used, when the propeller 15 is stopped, to drive the machine rearwardly. Additional engines and propellers 24, 26 may be mounted beneath or behind the rear planes and transversely arranged propellers 30 also may be provided. The propellers 13, 14, 26 may be arranged obliquely to the direction of flight and driven from a single engine. The shafts 2, 3, 4 are turnable simultaneously by the pilot to tilt the side planes. The side planes may be flat instead of arched.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB154731A GB360275A (en) | 1931-01-16 | 1931-01-16 | Improvements in or relating to heavier than air aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB154731A GB360275A (en) | 1931-01-16 | 1931-01-16 | Improvements in or relating to heavier than air aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB360275A true GB360275A (en) | 1931-11-05 |
Family
ID=9723859
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB154731A Expired GB360275A (en) | 1931-01-16 | 1931-01-16 | Improvements in or relating to heavier than air aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB360275A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2399324A (en) * | 2003-03-14 | 2004-09-15 | John Edward Randell | A propulsion arrangement for vertical takeoff aircraft |
| CN114348254A (en) * | 2021-12-30 | 2022-04-15 | 天津爱思达航天科技有限公司 | Aircraft with double row wheel pair rotation aerodynamic effect |
-
1931
- 1931-01-16 GB GB154731A patent/GB360275A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2399324A (en) * | 2003-03-14 | 2004-09-15 | John Edward Randell | A propulsion arrangement for vertical takeoff aircraft |
| GB2399324B (en) * | 2003-03-14 | 2005-08-03 | John Edward Randell | A propulsion arrangement for a vertical take-off aircraft |
| CN114348254A (en) * | 2021-12-30 | 2022-04-15 | 天津爱思达航天科技有限公司 | Aircraft with double row wheel pair rotation aerodynamic effect |
| WO2023123682A1 (en) * | 2021-12-30 | 2023-07-06 | 天津爱思达航天科技有限公司 | Aircraft having double-row wheel counter-rotating pneumatic effect |
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