US4203286A
(en)
*
|
1976-08-27 |
1980-05-20 |
The United States Of America As Represented By The Secretary Of The Air Force |
Cooling apparatus for an exhaust nozzle of a gas turbine engine
|
US4074523A
(en)
*
|
1976-12-08 |
1978-02-21 |
The United States Of America As Represented By The Secretary Of The Air Force |
Pressure actuated collapsible curtain liners for a gas turbine engine nozzle
|
US4081137A
(en)
*
|
1977-01-05 |
1978-03-28 |
The United States Of America As Represented By The Secretary Of The Air Force |
Finned surface cooled nozzle
|
US4128208A
(en)
*
|
1977-07-11 |
1978-12-05 |
General Electric Company |
Exhaust nozzle flap seal arrangement
|
US4176792A
(en)
*
|
1977-07-11 |
1979-12-04 |
General Electric Company |
Variable area exhaust nozzle
|
US4171093A
(en)
*
|
1977-08-19 |
1979-10-16 |
The United States Of America As Represented By The Secretary Of The Air Force |
Durability flap and seal liner assembly for exhaust nozzles
|
US4643356A
(en)
*
|
1977-08-31 |
1987-02-17 |
United Technologies Corporation |
Cooling liner for convergent-divergent exhaust nozzle
|
US4544098A
(en)
*
|
1982-12-27 |
1985-10-01 |
United Technologies Corporation |
Cooled exhaust nozzle flaps
|
FR2557211A1
(fr)
*
|
1983-12-21 |
1985-06-28 |
Camboulives Andre |
Ensemble d'ejection, en particulier pour turboreacteur
|
FR2565293B1
(fr)
*
|
1984-06-04 |
1986-10-17 |
Aerospatiale |
Ensemble dilueur-deviateur de jet pour turbomoteur d'aerodyne
|
US4747543A
(en)
*
|
1987-04-14 |
1988-05-31 |
United Technologies Corporation |
Nozzle flap cooling liner
|
US4742961A
(en)
*
|
1987-05-04 |
1988-05-10 |
United Technologies Corporation |
Exhaust gas nozzle including a cooling air diverter
|
US5039014A
(en)
*
|
1989-04-11 |
1991-08-13 |
General Electric Company |
Axisymmetric vectoring exhaust nozzle seal
|
JPH0711259B2
(ja)
*
|
1989-09-07 |
1995-02-08 |
ゼネラル・エレクトリック・カンパニイ |
排気ノズルヒンジ
|
US5101624A
(en)
*
|
1989-09-07 |
1992-04-07 |
General Electric Company |
Exhaust nozzle hinge
|
US5080284A
(en)
*
|
1990-06-25 |
1992-01-14 |
United Technologies Corporation |
Cooling system for the trailing edge of a liner
|
US5141154A
(en)
*
|
1991-04-22 |
1992-08-25 |
United Technologies Corporation |
Variable throat convergent/divergent nozzle
|
US5143292A
(en)
*
|
1991-05-09 |
1992-09-01 |
General Electric Company |
Cooled leaf seal
|
US5255849A
(en)
*
|
1991-11-05 |
1993-10-26 |
General Electric Company |
Cooling air transfer apparatus for aircraft gas turbine engine exhaust nozzles
|
US5720434A
(en)
*
|
1991-11-05 |
1998-02-24 |
General Electric Company |
Cooling apparatus for aircraft gas turbine engine exhaust nozzles
|
US5511376A
(en)
*
|
1993-08-31 |
1996-04-30 |
United Technologies Corporation |
Axisymmetric vectoring nozzle
|
US5435127A
(en)
*
|
1993-11-15 |
1995-07-25 |
General Electric Company |
Method and apparatus for boosting ram airflow to an ejection nozzle
|
US6021637A
(en)
*
|
1997-09-29 |
2000-02-08 |
General Electric Company |
Integrated fluidic CD nozzle for gas turbine engine
|
US7225622B2
(en)
*
|
2003-07-21 |
2007-06-05 |
United Technologies Corporation |
Turbine engine nozzle
|
FR2858833B1
(fr)
*
|
2003-08-12 |
2006-01-06 |
Snecma Moteurs |
Tuyere convergente divergente du turboreacteur
|
EP1735531A4
(en)
*
|
2003-12-01 |
2015-01-21 |
Univ Mississippi |
METHOD AND DEVICE FOR REDUCING MOTOR NOISE
|
US7739872B2
(en)
*
|
2005-02-14 |
2010-06-22 |
United Technologies Corporation |
Cooled dual wall liner closeout
|
US20070062199A1
(en)
*
|
2005-09-22 |
2007-03-22 |
United Technologies Corporation |
Turbine engine nozzle
|
US8015819B2
(en)
*
|
2006-09-29 |
2011-09-13 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Wet active chevron nozzle for controllable jet noise reduction
|
US8029234B2
(en)
*
|
2007-07-24 |
2011-10-04 |
United Technologies Corp. |
Systems and methods involving aerodynamic struts
|
US8739548B2
(en)
*
|
2007-12-20 |
2014-06-03 |
United Technologies Corporation |
Sliding ramp nozzle system for a gas turbine engine
|
US8127526B2
(en)
*
|
2008-01-16 |
2012-03-06 |
United Technologies Corporation |
Recoatable exhaust liner cooling arrangement
|
US8156745B2
(en)
*
|
2008-02-29 |
2012-04-17 |
General Electric Company |
Exhaust nozzle seal with segmented basesheet
|
FR2933128B1
(fr)
*
|
2008-06-25 |
2010-09-17 |
Snecma |
Dispositif de prelevement d'air de refroidissement dans une turbomachine
|
FR2933127B1
(fr)
*
|
2008-06-25 |
2015-04-24 |
Snecma |
Dispositif de prelevement d'air de refroidissement dans une turbomachine
|
FR2937679B1
(fr)
*
|
2008-10-24 |
2010-12-03 |
Snecma |
Dispositif de prelevement d'air de refroidissement dans une turbomachine
|
US8595930B2
(en)
|
2010-03-24 |
2013-12-03 |
Dresser-Rand Company |
Press-fitting corrosion resistant liners in nozzles and casings
|
US10400710B2
(en)
*
|
2013-05-07 |
2019-09-03 |
General Electric Company |
Secondary nozzle for jet engine
|
FR3100284B1
(fr)
*
|
2019-08-30 |
2021-12-03 |
Safran Aircraft Engines |
Couple volet convergent-volet divergent pour tuyère de turboréacteur à géométrie variable dont les volets comprennent chacun un conduit de circulation d’air de refroidissement
|
CN113530706B
(zh)
*
|
2021-08-18 |
2022-08-05 |
中国航发贵阳发动机设计研究所 |
一种发动机尾喷管的外调节片与主动调节片的连接结构
|
CN114151228B
(zh)
*
|
2022-02-09 |
2022-04-22 |
中国航发四川燃气涡轮研究院 |
二元矢量喷管调节片离散式冷气分区的方法
|
CN115680781B
(zh)
*
|
2022-08-30 |
2024-05-03 |
中国航发四川燃气涡轮研究院 |
一种带冷却功能的叶轮排气装置
|