IT1144840B - AIRCRAFT WITH JET PROPULSER USING A SINGLE-SIDED EJECTOR SYSTEM FOR INCREASING THE CARRIER AND THE THRUST - Google Patents
AIRCRAFT WITH JET PROPULSER USING A SINGLE-SIDED EJECTOR SYSTEM FOR INCREASING THE CARRIER AND THE THRUSTInfo
- Publication number
- IT1144840B IT1144840B IT68334/81A IT6833481A IT1144840B IT 1144840 B IT1144840 B IT 1144840B IT 68334/81 A IT68334/81 A IT 68334/81A IT 6833481 A IT6833481 A IT 6833481A IT 1144840 B IT1144840 B IT 1144840B
- Authority
- IT
- Italy
- Prior art keywords
- propulser
- aircraft
- thrust
- jet
- carrier
- Prior art date
Links
Priority Applications (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT68334/81A IT1144840B (en) | 1981-10-15 | 1981-10-15 | AIRCRAFT WITH JET PROPULSER USING A SINGLE-SIDED EJECTOR SYSTEM FOR INCREASING THE CARRIER AND THE THRUST |
| DE198282830254T DE78245T1 (en) | 1981-10-15 | 1982-10-12 | PLANE WITH JET DRIVE. |
| DE8282830254T DE3274535D1 (en) | 1981-10-15 | 1982-10-12 | Aircraft with jet propulsion |
| AT82830254T ATE23971T1 (en) | 1981-10-15 | 1982-10-12 | JET AIRPLANE. |
| US06/434,073 US4478378A (en) | 1981-10-15 | 1982-10-12 | Aircraft with jet propulsion |
| EP82830254A EP0078245B1 (en) | 1981-10-15 | 1982-10-12 | Aircraft with jet propulsion |
| JP18121382A JPS58126291A (en) | 1981-10-15 | 1982-10-15 | Jet propulsion type aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT68334/81A IT1144840B (en) | 1981-10-15 | 1981-10-15 | AIRCRAFT WITH JET PROPULSER USING A SINGLE-SIDED EJECTOR SYSTEM FOR INCREASING THE CARRIER AND THE THRUST |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IT8168334A0 IT8168334A0 (en) | 1981-10-15 |
| IT1144840B true IT1144840B (en) | 1986-10-29 |
Family
ID=11309017
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT68334/81A IT1144840B (en) | 1981-10-15 | 1981-10-15 | AIRCRAFT WITH JET PROPULSER USING A SINGLE-SIDED EJECTOR SYSTEM FOR INCREASING THE CARRIER AND THE THRUST |
Country Status (2)
| Country | Link |
|---|---|
| JP (1) | JPS58126291A (en) |
| IT (1) | IT1144840B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010247627A (en) * | 2009-04-14 | 2010-11-04 | Global Energy Co Ltd | Airplane |
| EP3344535B1 (en) * | 2015-09-02 | 2021-06-09 | Jetoptera, Inc. | Ejector and airfoil configurations |
| KR102416862B1 (en) * | 2016-03-11 | 2022-07-05 | 제톱테라 잉크. | Configuration for vertical take-off and landing system for aerial vehicles |
| CN115520373B (en) * | 2022-08-18 | 2024-07-09 | 北京临近空间飞行器系统工程研究所 | Jet flow control mechanism for controlling airflow direction of trailing edge flow field of aircraft wing |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5340998A (en) * | 1975-10-11 | 1978-04-13 | Yoshio Nozaki | Vertical short range takeoff and landing aircraft |
-
1981
- 1981-10-15 IT IT68334/81A patent/IT1144840B/en active
-
1982
- 1982-10-15 JP JP18121382A patent/JPS58126291A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0254279B2 (en) | 1990-11-21 |
| IT8168334A0 (en) | 1981-10-15 |
| JPS58126291A (en) | 1983-07-27 |
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