FR2051588A7 - - Google Patents
Info
- Publication number
- FR2051588A7 FR2051588A7 FR7025189A FR7025189A FR2051588A7 FR 2051588 A7 FR2051588 A7 FR 2051588A7 FR 7025189 A FR7025189 A FR 7025189A FR 7025189 A FR7025189 A FR 7025189A FR 2051588 A7 FR2051588 A7 FR 2051588A7
- Authority
- FR
- France
- 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
- B64C29/0008—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
- B64C29/0058—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 with vertical jet
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19691934370 DE1934370C3 (en) | 1969-07-07 | Vertical or short take-off aircraft with at least one lift engine installed approximately vertically in the aircraft fuselage |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2051588A7 true FR2051588A7 (en) | 1971-04-09 |
| FR2051588B3 FR2051588B3 (en) | 1973-04-06 |
Family
ID=5739099
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7025189A Expired FR2051588B3 (en) | 1969-07-07 | 1970-07-07 |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR2051588B3 (en) |
| GB (1) | GB1272384A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615089B (en) * | 2019-08-22 | 2022-08-05 | 南京航空航天大学 | Roll-over control mechanism suitable for small vertical take-off and landing fixed wing aircraft |
-
1970
- 1970-07-02 GB GB3214670A patent/GB1272384A/en not_active Expired
- 1970-07-07 FR FR7025189A patent/FR2051588B3/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1272384A (en) | 1972-04-26 |
| DE1934370B2 (en) | 1976-01-22 |
| FR2051588B3 (en) | 1973-04-06 |
| DE1934370A1 (en) | 1971-01-28 |