GB832542A - Improvements in vertical take-off aircraft - Google Patents
Improvements in vertical take-off aircraftInfo
- Publication number
- GB832542A GB832542A GB8555/57A GB855557A GB832542A GB 832542 A GB832542 A GB 832542A GB 8555/57 A GB8555/57 A GB 8555/57A GB 855557 A GB855557 A GB 855557A GB 832542 A GB832542 A GB 832542A
- Authority
- GB
- United Kingdom
- Prior art keywords
- container
- aircraft
- vertical take
- thrust
- wing
- 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
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
- B64C39/062—Aircraft not otherwise provided for having disc- or ring-shaped wings having annular wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Tires In General (AREA)
Abstract
832,542. Vertical take-off aircraft. ZBOROWSKI, H. P. G. A. R. VON March 15, 1957 [March 17, 1956], No. 8555/57. Class 4. An aircraft intended for vertical take-off and comprising an annular wing 1 surrounding and attached to a central fuselage 3, is provided with a supplementary load-carrying container 6 secured at 8 to the wing 1. The attachments 8 may be releasable in order that the container may be jettisoned to descend by a parachute stored in a compartment 6b. The supplementary load is housed in a compartment 6a and the container is provided with an auxiliary rocket propulsion unit 7 having a thrust so related to the weight of container 6 and the thrust of the main turbo-jet engine 2 that the resultant thrust P passes through the centre of gravity G. Jetdeflecting flaps 2a, control surfaces 4 and landing legs 5 are provided. Container 6 may be mounted on the inner wall of wing 1. Specification 730,069 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR832542X | 1956-03-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB832542A true GB832542A (en) | 1960-04-13 |
Family
ID=9296083
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8555/57A Expired GB832542A (en) | 1956-03-17 | 1957-03-15 | Improvements in vertical take-off aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB832542A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001096179A1 (en) * | 2000-06-10 | 2001-12-20 | Bae Systems Plc | Ring-wing aircraft |
CN102756806A (en) * | 2012-07-26 | 2012-10-31 | 沈阳申蓝航空科技有限公司 | Upright-standing vertical take-off and landing airplane |
-
1957
- 1957-03-15 GB GB8555/57A patent/GB832542A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001096179A1 (en) * | 2000-06-10 | 2001-12-20 | Bae Systems Plc | Ring-wing aircraft |
US6607162B2 (en) | 2000-06-10 | 2003-08-19 | Bae Systems Plc | Ring-wing aircraft |
CN102756806A (en) * | 2012-07-26 | 2012-10-31 | 沈阳申蓝航空科技有限公司 | Upright-standing vertical take-off and landing airplane |
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