JPS5048700A - - Google Patents
Info
- Publication number
- JPS5048700A JPS5048700A JP7289474A JP7289474A JPS5048700A JP S5048700 A JPS5048700 A JP S5048700A JP 7289474 A JP7289474 A JP 7289474A JP 7289474 A JP7289474 A JP 7289474A JP S5048700 A JPS5048700 A JP S5048700A
- Authority
- JP
- Japan
- 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.)
- Pending
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
- B64C29/0066—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 horizontal jet and jet deflector
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/587,219 US3988827A (en) | 1974-06-21 | 1975-06-16 | Small-size cutter |
| DE2527634A DE2527634C3 (de) | 1974-06-27 | 1975-06-20 | Tragbare Schneidvorrichtung |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3084773A GB1473088A (ko) | 1973-06-28 | 1973-06-28 | |
| GB433474 | 1974-01-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS5048700A true JPS5048700A (ko) | 1975-04-30 |
Family
ID=26239049
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7289474A Pending JPS5048700A (ko) | 1973-06-28 | 1974-06-27 |
Country Status (4)
| Country | Link |
|---|---|
| JP (1) | JPS5048700A (ko) |
| DE (1) | DE2430406A1 (ko) |
| FR (1) | FR2235047A1 (ko) |
| IT (1) | IT1026017B (ko) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3013759A1 (de) * | 1980-04-10 | 1981-12-03 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Verfahren zur verbesserung der steuerbarkeit von strahlgetriebenen flugzeugen |
| GB2188887B (en) * | 1986-04-08 | 1989-11-29 | Rolls Royce Plc | Aircraft with stowable vectorable nozzle and ejector thrust augmentation |
-
1974
- 1974-06-25 DE DE19742430406 patent/DE2430406A1/de active Pending
- 1974-06-27 JP JP7289474A patent/JPS5048700A/ja active Pending
- 1974-06-27 FR FR7422374A patent/FR2235047A1/fr not_active Withdrawn
- 1974-06-27 IT IT5178374A patent/IT1026017B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| FR2235047A1 (en) | 1975-01-24 |
| DE2430406A1 (de) | 1975-01-16 |
| IT1026017B (it) | 1978-09-20 |