ATE473365T1 - Verschliessbare strahldüse - Google Patents
Verschliessbare strahldüseInfo
- Publication number
- ATE473365T1 ATE473365T1 AT01308422T AT01308422T ATE473365T1 AT E473365 T1 ATE473365 T1 AT E473365T1 AT 01308422 T AT01308422 T AT 01308422T AT 01308422 T AT01308422 T AT 01308422T AT E473365 T1 ATE473365 T1 AT E473365T1
- Authority
- AT
- Austria
- Prior art keywords
- upstream
- downstream
- flaps
- mount
- flow path
- Prior art date
Links
- 238000011144 upstream manufacturing Methods 0.000 abstract 6
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- 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
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
-
- 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
-
- 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
- F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
-
- 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
- F02K1/78—Other construction of jet pipes
- F02K1/80—Couplings or connections
- F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Exhaust Silencers (AREA)
- Percussion Or Vibration Massage (AREA)
- Testing Of Engines (AREA)
- Treating Waste Gases (AREA)
- Gas Separation By Absorption (AREA)
- Medicines Containing Plant Substances (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/684,095 US6352211B1 (en) | 2000-10-06 | 2000-10-06 | Flow blocking exhaust nozzle |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE473365T1 true ATE473365T1 (de) | 2010-07-15 |
Family
ID=24746650
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT01308422T ATE473365T1 (de) | 2000-10-06 | 2001-10-02 | Verschliessbare strahldüse |
Country Status (8)
Country | Link |
---|---|
US (1) | US6352211B1 (de) |
EP (1) | EP1195512B1 (de) |
JP (1) | JP2002147283A (de) |
AT (1) | ATE473365T1 (de) |
DE (1) | DE60142504D1 (de) |
ES (1) | ES2345871T3 (de) |
IL (1) | IL145573A (de) |
RU (1) | RU2001127069A (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6857600B1 (en) | 2002-04-26 | 2005-02-22 | General Electric Company | Infrared suppressing two dimensional vectorable single expansion ramp nozzle |
US7395657B2 (en) * | 2003-10-20 | 2008-07-08 | General Electric Company | Flade gas turbine engine with fixed geometry inlet |
US7775048B2 (en) * | 2006-06-30 | 2010-08-17 | General Electric Company | Seal assembly |
US20090067993A1 (en) * | 2007-03-22 | 2009-03-12 | Roberge Gary D | Coated variable area fan nozzle |
US8572986B2 (en) * | 2009-07-27 | 2013-11-05 | United Technologies Corporation | Retainer for suspended thermal protection elements in a gas turbine engine |
US8910464B2 (en) * | 2011-04-26 | 2014-12-16 | Lockheed Martin Corporation | Lift fan spherical thrust vectoring nozzle |
US8607574B1 (en) * | 2012-06-11 | 2013-12-17 | United Technologies Corporation | Turbine engine exhaust nozzle flap |
US9476322B2 (en) | 2012-07-05 | 2016-10-25 | Siemens Energy, Inc. | Combustor transition duct assembly with inner liner |
WO2014185272A1 (ja) | 2013-05-15 | 2014-11-20 | 株式会社Ihi | 航空用ガスタービンエンジンのための可変ノズル |
US9915228B2 (en) | 2013-08-16 | 2018-03-13 | United Technologies Corporation | Air with integral spring for a gas turbine engine exhaust drive |
WO2015080779A2 (en) | 2013-09-13 | 2015-06-04 | United Technologies Corporation | Large displacement high temperature seal |
US11661905B1 (en) * | 2022-01-17 | 2023-05-30 | Florida Turbine Technologies, Inc. | 2D variable-area plug nozzle |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4196856A (en) | 1977-11-25 | 1980-04-08 | The Boeing Company | Variable geometry convergent divergent exhaust nozzle |
US4375276A (en) * | 1980-06-02 | 1983-03-01 | General Electric Company | Variable geometry exhaust nozzle |
GB2155552B (en) * | 1981-02-24 | 1986-02-26 | Rolls Royce | Adjustable jet propulsion nozzle |
US4753392A (en) * | 1984-11-02 | 1988-06-28 | United Technologies Corporation | Two dimensional gas turbine engine exhaust nozzle |
US4690329A (en) * | 1984-11-02 | 1987-09-01 | United Technologies Corporation | Exhaust nozzle coupled with reverser exhaust door |
US4819876A (en) * | 1987-06-25 | 1989-04-11 | United Technologies Corporation | Divergent flap actuation system for a two-dimensional exhaust nozzle |
US4884748A (en) * | 1988-09-02 | 1989-12-05 | United Technologies Corporation | Fairing flap arrangement |
US5016818A (en) * | 1989-08-21 | 1991-05-21 | General Electric Company | Integral transition and convergent section exhaust nozzle |
-
2000
- 2000-10-06 US US09/684,095 patent/US6352211B1/en not_active Expired - Lifetime
-
2001
- 2001-09-24 IL IL14557301A patent/IL145573A/en not_active IP Right Cessation
- 2001-10-02 EP EP01308422A patent/EP1195512B1/de not_active Expired - Lifetime
- 2001-10-02 ES ES01308422T patent/ES2345871T3/es not_active Expired - Lifetime
- 2001-10-02 DE DE60142504T patent/DE60142504D1/de not_active Expired - Lifetime
- 2001-10-02 AT AT01308422T patent/ATE473365T1/de not_active IP Right Cessation
- 2001-10-05 RU RU2001127069/06A patent/RU2001127069A/ru not_active Application Discontinuation
- 2001-10-05 JP JP2001309306A patent/JP2002147283A/ja not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
IL145573A0 (en) | 2002-06-30 |
DE60142504D1 (de) | 2010-08-19 |
US6352211B1 (en) | 2002-03-05 |
EP1195512A3 (de) | 2004-01-14 |
IL145573A (en) | 2004-09-27 |
RU2001127069A (ru) | 2003-06-10 |
ES2345871T3 (es) | 2010-10-05 |
JP2002147283A (ja) | 2002-05-22 |
EP1195512B1 (de) | 2010-07-07 |
EP1195512A2 (de) | 2002-04-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |