FR2283053A1 - VSTOL able to land on water - has flying wing configuration, and jet deflectors - Google Patents
VSTOL able to land on water - has flying wing configuration, and jet deflectorsInfo
- Publication number
- FR2283053A1 FR2283053A1 FR7429603A FR7429603A FR2283053A1 FR 2283053 A1 FR2283053 A1 FR 2283053A1 FR 7429603 A FR7429603 A FR 7429603A FR 7429603 A FR7429603 A FR 7429603A FR 2283053 A1 FR2283053 A1 FR 2283053A1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- vstol
- land
- water
- flying 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.)
- Withdrawn
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
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
-
- 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)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
The cabin is part of the wing surface and the longitudinal and transverse sections are bi-convex and symmetrical to their respective chords. The curve of the lateral parts is equal to the curve of the max. longitudinal section, the ends of these lateral curves being tangents to a parallel to the central longitudinal axis. The arc of the circle which forms the rear end has the nose as its centre. The aircraft has two rudders and elevators. Engines embedded within the structure on either side of the centre line provide thrust for forward flight but by means of deflectors they can provide vertical thrust. A lift engine at the forward end of the aircraft gives the aircraft a slight positive angle of incidence.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7429603A FR2283053A1 (en) | 1974-08-30 | 1974-08-30 | VSTOL able to land on water - has flying wing configuration, and jet deflectors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7429603A FR2283053A1 (en) | 1974-08-30 | 1974-08-30 | VSTOL able to land on water - has flying wing configuration, and jet deflectors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2283053A1 true FR2283053A1 (en) | 1976-03-26 |
Family
ID=9142679
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7429603A Withdrawn FR2283053A1 (en) | 1974-08-30 | 1974-08-30 | VSTOL able to land on water - has flying wing configuration, and jet deflectors |
Country Status (1)
| Country | Link |
|---|---|
| FR (1) | FR2283053A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2575723A1 (en) * | 1985-01-04 | 1986-07-11 | Chaneac Henri | Flying wing |
| CN112327922A (en) * | 2020-11-18 | 2021-02-05 | 南京航空航天大学 | Autonomous take-off and landing integrated control method for flying wing unmanned aerial vehicle |
-
1974
- 1974-08-30 FR FR7429603A patent/FR2283053A1/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2575723A1 (en) * | 1985-01-04 | 1986-07-11 | Chaneac Henri | Flying wing |
| CN112327922A (en) * | 2020-11-18 | 2021-02-05 | 南京航空航天大学 | Autonomous take-off and landing integrated control method for flying wing unmanned aerial vehicle |
| CN112327922B (en) * | 2020-11-18 | 2022-04-22 | 南京航空航天大学 | Autonomous take-off and landing integrated control method for flying wing unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |