GB1272384A - Jet lift engine assemblies for v/stol aircraft - Google Patents
Jet lift engine assemblies for v/stol aircraftInfo
- Publication number
- GB1272384A GB1272384A GB3214670A GB3214670A GB1272384A GB 1272384 A GB1272384 A GB 1272384A GB 3214670 A GB3214670 A GB 3214670A GB 3214670 A GB3214670 A GB 3214670A GB 1272384 A GB1272384 A GB 1272384A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- aircraft
- duct
- jet
- jet lift
- 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
- B64C29/0008—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)
- Toys (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,272,384. Jet lift engine assemblies. MESSERSCHMITT - BOLKOW - BLOHM G.m.b.H. 2 July, 1970 [7 July, 1969], No. 32146/70. Heading B7G. A jet lift engine assembly is arranged in a V/STOL aircraft to provide two downwardly directed jets one on each side of the aircraft for roll control and comprises: a jet engine 11 pivotally mounted on links 14 so as to discharge an efflux from the discharge end of the engine casing which thereby moves laterally; and a bifurcated duet 20 mounted on the engine and the fuselage of the aircraft, for lateral movement when in use, to receive the efflux from the engine and deliver said two downwardly directed jets. The duct 20 is mounted in the engine casing by a spherical bearing 24 and is provided with a ring 22 mounted to the fuselage of the aircraft by links 23 which constrain the duct to move only laterally when in use. Movement of the duct is caused by pivoting bell cranks 21 mounted on the engine casing. When the engine 11 is in its central vertical position, Fig. 2, the duct may be pivoted about the axis of the engine from an outer operative position (shown in chain lines) to a stowed inoperative position (shown in solid lines in Fig. 2).
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 (1)
| Publication Number | Publication Date |
|---|---|
| GB1272384A true GB1272384A (en) | 1972-04-26 |
Family
ID=5739099
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3214670A Expired GB1272384A (en) | 1969-07-07 | 1970-07-02 | Jet lift engine assemblies for v/stol aircraft |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR2051588B3 (en) |
| GB (1) | GB1272384A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615089A (en) * | 2019-08-22 | 2019-12-27 | 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
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615089A (en) * | 2019-08-22 | 2019-12-27 | 南京航空航天大学 | Roll-over control mechanism suitable for small vertical take-off and landing fixed wing aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1934370B2 (en) | 1976-01-22 |
| DE1934370A1 (en) | 1971-01-28 |
| FR2051588B3 (en) | 1973-04-06 |
| FR2051588A7 (en) | 1971-04-09 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |