ITMI910356A1 - Ugello di scarico comprendente riduzione di spinta al minimo - Google Patents
Ugello di scarico comprendente riduzione di spinta al minimoInfo
- Publication number
- ITMI910356A1 ITMI910356A1 IT000356A ITMI910356A ITMI910356A1 IT MI910356 A1 ITMI910356 A1 IT MI910356A1 IT 000356 A IT000356 A IT 000356A IT MI910356 A ITMI910356 A IT MI910356A IT MI910356 A1 ITMI910356 A1 IT MI910356A1
- Authority
- IT
- Italy
- Prior art keywords
- discharge nozzle
- nozzle including
- including minimum
- thrust reduction
- minimum thrust
- Prior art date
Links
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
- F02K1/04—Mounting of an exhaust cone in the jet pipe
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
- Exhaust Silencers (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/479,503 US5140809A (en) | 1990-02-12 | 1990-02-12 | Exhaust nozzle idle thrust spoiling method |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| ITMI910356A0 ITMI910356A0 (it) | 1991-02-12 |
| ITMI910356A1 true ITMI910356A1 (it) | 1992-08-12 |
| IT1245154B IT1245154B (it) | 1994-09-13 |
Family
ID=23904298
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ITMI910356A IT1245154B (it) | 1990-02-12 | 1991-02-12 | Ugello di scarico comprendente riduzione di spinta al minimo |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5140809A (it) |
| JP (1) | JPH0762465B2 (it) |
| CA (1) | CA2034406A1 (it) |
| DE (1) | DE4103517A1 (it) |
| FR (1) | FR2658247A1 (it) |
| GB (1) | GB2241744A (it) |
| IT (1) | IT1245154B (it) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5328098A (en) * | 1993-07-09 | 1994-07-12 | United Technologies Corporation | Thrust vectoring ejector nozzle |
| US8572986B2 (en) * | 2009-07-27 | 2013-11-05 | United Technologies Corporation | Retainer for suspended thermal protection elements in a gas turbine engine |
| US10378479B2 (en) * | 2015-10-19 | 2019-08-13 | General Electric Company | Variable effective area fan nozzle |
Family Cites Families (24)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2880575A (en) * | 1952-11-28 | 1959-04-07 | Curtiss Wright Corp | Combined variable area nozzle and aerodynamic brake |
| US2846843A (en) * | 1953-01-07 | 1958-08-12 | Curtiss Wright Corp | Variable area convergent-divergent exhaust nozzle and control therefor |
| GB782494A (en) * | 1954-03-26 | 1957-09-11 | Rolls Royce | Improvements in or relating to jet propulsion nozzle arrangements |
| US2711217A (en) * | 1954-04-26 | 1955-06-21 | Lee S Gaty | Automatic feed box |
| US2926491A (en) * | 1958-08-25 | 1960-03-01 | Orenda Engines Ltd | Actuating means for variable nozzles |
| FR1225736A (fr) * | 1959-02-16 | 1960-07-04 | Snecma | Tuyère réglable pour propulseur à réaction |
| US3216691A (en) * | 1963-09-18 | 1965-11-09 | Globe Products Corp | Window shade bracket |
| US3454227A (en) * | 1966-08-19 | 1969-07-08 | United Aircraft Corp | Free floating articulate ejector nozzle |
| FR2180440B1 (it) * | 1972-04-17 | 1976-06-11 | Snecma | |
| FR2277239A2 (fr) * | 1974-07-04 | 1976-01-30 | Snecma | Dispositif de commande de volets de tuyere d'ejection |
| GB1533986A (en) * | 1976-04-12 | 1978-11-29 | Rolls Royce | Nozzles for gas turbine engines |
| US4141501A (en) * | 1975-05-09 | 1979-02-27 | Rolls-Royce (1971) Limited | Nozzles for gas turbine engines |
| US4037405A (en) * | 1975-09-30 | 1977-07-26 | United Technologies Corporation | Two dimensional nozzle with rotating plug |
| US4000854A (en) * | 1975-10-02 | 1977-01-04 | General Electric Company | Thrust vectorable exhaust nozzle |
| DE2711217A1 (de) * | 1976-03-17 | 1977-09-22 | Rolls Royce 1971 Ltd | Verstellduese fuer gasturbinentriebwerke |
| US4091613A (en) * | 1976-07-30 | 1978-05-30 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Independent power generator |
| FR2474592A1 (fr) * | 1980-01-25 | 1981-07-31 | Snecma | Dispositif de tuyere de turboreacteur |
| US4279382A (en) * | 1980-01-28 | 1981-07-21 | The United States Of America As Represented By The Secretary Of The Air Force | Radial and axial flow variable exhaust nozzle for a gas turbine engine |
| US4587806A (en) * | 1981-05-11 | 1986-05-13 | United Technologies Corporation | Area two-dimensional converging/diverging nozzle |
| US4392615A (en) * | 1981-05-11 | 1983-07-12 | United Technologies Corporation | Viol exhaust nozzle with veer flap extension |
| US4463903A (en) * | 1982-05-10 | 1984-08-07 | Nightingale Douglas J | Turbomachine ejector nozzle |
| US4605169A (en) * | 1983-12-27 | 1986-08-12 | United Technologies Corporation | Exhaust nozzle construction |
| FR2608680B1 (fr) * | 1986-12-17 | 1989-03-17 | Snecma | Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion |
| US4994660A (en) * | 1989-04-11 | 1991-02-19 | Hitachi, Ltd. | Axisymmetric vectoring exhaust nozzle |
-
1990
- 1990-02-12 US US07/479,503 patent/US5140809A/en not_active Expired - Fee Related
-
1991
- 1991-01-17 CA CA002034406A patent/CA2034406A1/en not_active Abandoned
- 1991-01-25 JP JP3023684A patent/JPH0762465B2/ja not_active Expired - Lifetime
- 1991-02-01 FR FR9101177A patent/FR2658247A1/fr active Pending
- 1991-02-06 DE DE4103517A patent/DE4103517A1/de not_active Ceased
- 1991-02-11 GB GB9102859A patent/GB2241744A/en not_active Withdrawn
- 1991-02-12 IT ITMI910356A patent/IT1245154B/it active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| JPH04219450A (ja) | 1992-08-10 |
| JPH0762465B2 (ja) | 1995-07-05 |
| ITMI910356A0 (it) | 1991-02-12 |
| GB9102859D0 (en) | 1991-03-27 |
| DE4103517A1 (de) | 1991-08-14 |
| FR2658247A1 (fr) | 1991-08-16 |
| IT1245154B (it) | 1994-09-13 |
| US5140809A (en) | 1992-08-25 |
| GB2241744A (en) | 1991-09-11 |
| CA2034406A1 (en) | 1991-08-13 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 0001 | Granted |