DE2360442C3 - Dusenaustrittssystem fur ein Flugzeugstrahltriebwerk - Google Patents
Dusenaustrittssystem fur ein FlugzeugstrahltriebwerkInfo
- Publication number
- DE2360442C3 DE2360442C3 DE2360442A DE2360442A DE2360442C3 DE 2360442 C3 DE2360442 C3 DE 2360442C3 DE 2360442 A DE2360442 A DE 2360442A DE 2360442 A DE2360442 A DE 2360442A DE 2360442 C3 DE2360442 C3 DE 2360442C3
- Authority
- DE
- Germany
- Prior art keywords
- thrust
- flaps
- nozzle outlet
- ramp
- nozzle
- 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
- 230000009194 climbing Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000003351 stiffener Substances 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/56—Reversing jet main flow
- F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Turbines (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US31790872A | 1972-12-26 | 1972-12-26 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| DE2360442A1 DE2360442A1 (de) | 1974-07-11 |
| DE2360442B2 DE2360442B2 (de) | 1978-02-02 |
| DE2360442C3 true DE2360442C3 (de) | 1978-09-28 |
Family
ID=23235777
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE2360442A Expired DE2360442C3 (de) | 1972-12-26 | 1973-11-30 | Dusenaustrittssystem fur ein Flugzeugstrahltriebwerk |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US3791586A (enExample) |
| JP (1) | JPS5419930B2 (enExample) |
| DE (1) | DE2360442C3 (enExample) |
| FR (1) | FR2211595B1 (enExample) |
| GB (1) | GB1448245A (enExample) |
| IT (1) | IT994347B (enExample) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3877663A (en) * | 1973-11-19 | 1975-04-15 | Aeritalia Spa | Translating splitter variable area nozzle and reverser |
| US3893640A (en) * | 1973-11-27 | 1975-07-08 | Gen Electric | Sound suppressing nacelle arrangement |
| US3863867A (en) * | 1973-12-26 | 1975-02-04 | Boeing Co | Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor |
| US3981463A (en) * | 1974-03-21 | 1976-09-21 | Rohr Industries, Inc. | Overwing thrust reverser |
| US3915415A (en) * | 1974-03-21 | 1975-10-28 | Rohr Industries Inc | Overwing thrust reverser |
| USRE31591E (en) * | 1975-03-27 | 1984-05-29 | The Boeing Company | Fuselage tail jet engine thrust reverser and method |
| US3997134A (en) * | 1975-03-27 | 1976-12-14 | The Boeing Company | Fuselage tail jet engine thrust reverser |
| US4183478A (en) * | 1977-11-25 | 1980-01-15 | The Boeing Company | Jet thrust reverser |
| FR2494775B1 (fr) * | 1980-11-27 | 1985-07-05 | Astech | Dispositif pour la commande d'un inverseur de poussee pour moteur a reaction |
| US4579039A (en) * | 1983-12-12 | 1986-04-01 | Sundstrand Corporation | Power drive unit |
| DE102008022289B4 (de) * | 2008-04-25 | 2010-07-29 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugkörper |
| WO2020245513A1 (fr) * | 2019-06-07 | 2020-12-10 | Zipair | Groupe de poussée pour dispositif de propulsion et dispositif de propulsion associe |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB820059A (en) * | 1956-07-30 | 1959-09-16 | Bristol Aero Engines Ltd | Improvements in or relating to jet propulsion nozzles |
| US3080711A (en) * | 1960-01-06 | 1963-03-12 | James F Connors | Penshape exhaust nozzle for supersonic engine |
| US3667680A (en) * | 1970-04-24 | 1972-06-06 | Boeing Co | Jet engine exhaust nozzle system |
-
1972
- 1972-12-26 US US00317908A patent/US3791586A/en not_active Expired - Lifetime
-
1973
- 1973-09-27 IT IT52792/73A patent/IT994347B/it active
- 1973-11-20 GB GB5389573A patent/GB1448245A/en not_active Expired
- 1973-11-29 JP JP13392373A patent/JPS5419930B2/ja not_active Expired
- 1973-11-30 DE DE2360442A patent/DE2360442C3/de not_active Expired
- 1973-11-30 FR FR7342865A patent/FR2211595B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE2360442A1 (de) | 1974-07-11 |
| US3791586A (en) | 1974-02-12 |
| FR2211595A1 (enExample) | 1974-07-19 |
| GB1448245A (en) | 1976-09-02 |
| JPS49100799A (enExample) | 1974-09-24 |
| DE2360442B2 (de) | 1978-02-02 |
| IT994347B (it) | 1975-10-20 |
| FR2211595B1 (enExample) | 1976-06-25 |
| JPS5419930B2 (enExample) | 1979-07-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C3 | Grant after two publication steps (3rd publication) |