US8145710B2
(en)
|
2003-06-18 |
2012-03-27 |
Symantec Corporation |
System and method for filtering spam messages utilizing URL filtering module
|
FR2866070B1
(fr)
*
|
2004-02-05 |
2008-12-05 |
Snecma Moteurs |
Turboreacteur a fort taux de dilution
|
US7941490B1
(en)
|
2004-05-11 |
2011-05-10 |
Symantec Corporation |
Method and apparatus for detecting spam in email messages and email attachments
|
US7174704B2
(en)
*
|
2004-07-23 |
2007-02-13 |
General Electric Company |
Split shroud exhaust nozzle
|
US7188467B2
(en)
*
|
2004-09-30 |
2007-03-13 |
General Electric Company |
Methods and apparatus for assembling a gas turbine engine
|
US7140174B2
(en)
*
|
2004-09-30 |
2006-11-28 |
General Electric Company |
Methods and apparatus for assembling a gas turbine engine
|
US7475545B2
(en)
*
|
2005-04-29 |
2009-01-13 |
General Electric Company |
Fladed supersonic missile turbojet
|
US7509797B2
(en)
*
|
2005-04-29 |
2009-03-31 |
General Electric Company |
Thrust vectoring missile turbojet
|
US7448199B2
(en)
*
|
2005-04-29 |
2008-11-11 |
General Electric Company |
Self powdered missile turbojet
|
US7424805B2
(en)
*
|
2005-04-29 |
2008-09-16 |
General Electric Company |
Supersonic missile turbojet engine
|
US7739337B1
(en)
|
2005-06-20 |
2010-06-15 |
Symantec Corporation |
Method and apparatus for grouping spam email messages
|
US8010609B2
(en)
*
|
2005-06-20 |
2011-08-30 |
Symantec Corporation |
Method and apparatus for maintaining reputation lists of IP addresses to detect email spam
|
US20070000232A1
(en)
*
|
2005-06-29 |
2007-01-04 |
General Electric Company |
Gas turbine engine and method of operating same
|
US7464536B2
(en)
*
|
2005-07-07 |
2008-12-16 |
General Electric Company |
Methods and apparatus for assembling gas turbine engines
|
US8061145B2
(en)
*
|
2005-09-27 |
2011-11-22 |
Volvo Aero Corporation |
Arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine
|
US7730714B2
(en)
*
|
2005-11-29 |
2010-06-08 |
General Electric Company |
Turbofan gas turbine engine with variable fan outlet guide vanes
|
US7614210B2
(en)
*
|
2006-02-13 |
2009-11-10 |
General Electric Company |
Double bypass turbofan
|
US7631484B2
(en)
*
|
2006-03-13 |
2009-12-15 |
Rollin George Giffin |
High pressure ratio aft fan
|
DE102006013595B4
(de)
*
|
2006-03-22 |
2016-03-31 |
Danger Möricke |
Turbojet-Nachbrenner-und assoziierte Regelungssysteme
|
US7758303B1
(en)
*
|
2006-07-31 |
2010-07-20 |
General Electric Company |
FLADE fan with different inner and outer airfoil stagger angles at a shroud therebetween
|
US7770381B2
(en)
*
|
2006-12-18 |
2010-08-10 |
General Electric Company |
Duct burning mixed flow turbofan and method of operation
|
US7926290B2
(en)
*
|
2006-12-18 |
2011-04-19 |
General Electric Company |
Turbine engine with modulated flow fan and method of operation
|
US7963099B2
(en)
*
|
2007-05-21 |
2011-06-21 |
General Electric Company |
Fluted chevron exhaust nozzle
|
US9359960B2
(en)
|
2007-06-28 |
2016-06-07 |
United Technologies Corporation |
Gas turbines with multiple gas flow paths
|
US7926285B2
(en)
*
|
2007-07-18 |
2011-04-19 |
General Electric Company |
Modular chevron exhaust nozzle
|
US8393158B2
(en)
*
|
2007-10-24 |
2013-03-12 |
Gulfstream Aerospace Corporation |
Low shock strength inlet
|
FR2923270B1
(fr)
*
|
2007-11-06 |
2014-01-31 |
Airbus France |
Turbomoteur a tuyere de flux froid adaptee
|
US8590286B2
(en)
*
|
2007-12-05 |
2013-11-26 |
United Technologies Corp. |
Gas turbine engine systems involving tip fans
|
US8402742B2
(en)
|
2007-12-05 |
2013-03-26 |
United Technologies Corporation |
Gas turbine engine systems involving tip fans
|
US20090165864A1
(en)
*
|
2007-12-26 |
2009-07-02 |
Rolls-Royce North American Technologies, Inc. |
Supersonic inlet
|
US8240126B2
(en)
*
|
2008-03-22 |
2012-08-14 |
Pratt & Whitney Rocketdyne, Inc. |
Valve system for a gas turbine engine
|
US8578716B2
(en)
*
|
2008-03-22 |
2013-11-12 |
United Technologies Corporation |
Valve system for a gas turbine engine
|
US8402744B2
(en)
*
|
2008-03-22 |
2013-03-26 |
Pratt & Whitney Rocketdyne, Inc. |
Valve system for a gas turbine engine
|
US8286416B2
(en)
*
|
2008-04-02 |
2012-10-16 |
Pratt & Whitney Rocketdyne, Inc. |
Valve system for a gas turbine engine
|
US8776527B1
(en)
*
|
2008-06-17 |
2014-07-15 |
Rolls-Royce North American Technologies, Inc. |
Techniques to reduce infrared detection of a gas turbine engine
|
US20100054911A1
(en)
*
|
2008-08-29 |
2010-03-04 |
General Electric Company |
System and method for adjusting clearance in a gas turbine
|
KR20100032054A
(ko)
*
|
2008-09-17 |
2010-03-25 |
인제대학교 산학협력단 |
뇌파 분석을 이용한 치매 진단 장치 및 방법
|
EP2177735A3
(de)
*
|
2008-10-20 |
2012-02-15 |
Rolls-Royce North American Technologies, Inc. |
Turbofan
|
US8713909B2
(en)
|
2009-03-04 |
2014-05-06 |
United Technologies Corporation |
Elimination of unfavorable outflow margin
|
US8572986B2
(en)
|
2009-07-27 |
2013-11-05 |
United Technologies Corporation |
Retainer for suspended thermal protection elements in a gas turbine engine
|
US20110167792A1
(en)
*
|
2009-09-25 |
2011-07-14 |
James Edward Johnson |
Adaptive engine
|
US20110167831A1
(en)
*
|
2009-09-25 |
2011-07-14 |
James Edward Johnson |
Adaptive core engine
|
US20110167784A1
(en)
*
|
2009-09-25 |
2011-07-14 |
James Edward Johnson |
Method of operating a convertible fan engine
|
US8695324B2
(en)
*
|
2009-11-20 |
2014-04-15 |
General Electric Co. |
Multistage tip fan
|
US20110120083A1
(en)
*
|
2009-11-20 |
2011-05-26 |
Rollin George Giffin |
Gas turbine engine with outer fans
|
US9353684B2
(en)
*
|
2009-12-11 |
2016-05-31 |
Northrop Grumman Systems Corporation |
Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching
|
US20110146228A1
(en)
*
|
2009-12-21 |
2011-06-23 |
John Lewis Baughman |
Power extraction system
|
US20110146289A1
(en)
*
|
2009-12-21 |
2011-06-23 |
John Lewis Baughman |
Power extraction method
|
US9109539B2
(en)
*
|
2010-12-27 |
2015-08-18 |
Rolls-Royce North American Technologies, Inc. |
Turbine based combined cycle engine
|
US8783605B2
(en)
*
|
2010-12-28 |
2014-07-22 |
Rolls-Royce North American Technologies, Inc. |
Flight vehicle, propulsion system and thrust vectoring system
|
US8984891B2
(en)
|
2010-12-30 |
2015-03-24 |
General Electric Company |
Flade discharge in 2-D exhaust nozzle
|
FR2975135B1
(fr)
*
|
2011-05-12 |
2016-07-22 |
Snecma |
Cone arriere de turboreacteur tournant a micro-jets
|
US8789376B2
(en)
|
2011-05-27 |
2014-07-29 |
General Electric Company |
Flade duct turbine cooling and power and thermal management
|
US8943796B2
(en)
*
|
2011-06-28 |
2015-02-03 |
United Technologies Corporation |
Variable cycle turbine engine
|
US9777631B2
(en)
|
2011-09-30 |
2017-10-03 |
General Electric Company |
Conformal inlet apparatus for a gas turbine engine
|
US9097133B2
(en)
*
|
2012-06-04 |
2015-08-04 |
United Technologies Corporation |
Compressor tip clearance management for a gas turbine engine
|
US9097199B2
(en)
|
2012-06-21 |
2015-08-04 |
United Technologies Corporation |
Engine signature assessment system
|
US9341075B2
(en)
|
2012-06-25 |
2016-05-17 |
United Technologies Corporation |
Pre-turbine engine case variable area mixing plane
|
US20140096509A1
(en)
*
|
2012-10-05 |
2014-04-10 |
United Technologies Corporation |
Geared Turbofan Engine With Increased Bypass Ratio and Compressor Ratio ...
|
US20140165575A1
(en)
*
|
2012-12-13 |
2014-06-19 |
United Technologies Corporation |
Nozzle section for a gas turbine engine
|
US9863366B2
(en)
*
|
2013-03-13 |
2018-01-09 |
Rolls-Royce North American Technologies Inc. |
Exhaust nozzle apparatus and method for multi stream aircraft engine
|
KR20140125894A
(ko)
*
|
2013-03-26 |
2014-10-30 |
두산중공업 주식회사 |
가스 터빈 장치
|
US9909529B2
(en)
|
2013-09-20 |
2018-03-06 |
United Technologies Corporation |
Flow path routing within a gas turbine engine
|
US10400709B2
(en)
|
2013-09-20 |
2019-09-03 |
United Technologies Corporation |
Auxiliary device for three air flow path gas turbine engine
|
US10371090B2
(en)
|
2014-01-13 |
2019-08-06 |
United Technologies Corporation |
Variable area exhaust mixer for a gas turbine engine
|
US10030606B2
(en)
|
2014-01-27 |
2018-07-24 |
United Technologies Corporation |
Variable exhaust mixer and cooler for a three-stream gas turbine engine
|
US9951721B2
(en)
|
2014-10-21 |
2018-04-24 |
United Technologies Corporation |
Three-stream gas turbine engine architecture
|
US9803557B2
(en)
|
2015-01-20 |
2017-10-31 |
United Technologies Corporation |
Gas turbine engine and blocker door assembly
|
US10119477B2
(en)
|
2015-01-20 |
2018-11-06 |
United Technologies Corporation |
Gas turbine engine with a multi-spool driven fan
|
US11236639B2
(en)
|
2015-02-10 |
2022-02-01 |
Raytheon Technologies Corporation |
Gas turbine engine and an airflow control system
|
US10267160B2
(en)
*
|
2015-08-27 |
2019-04-23 |
Rolls-Royce North American Technologies Inc. |
Methods of creating fluidic barriers in turbine engines
|
PL414889A1
(pl)
*
|
2015-11-23 |
2017-06-05 |
General Electric Company |
Okapotowanie sprężające dla wylotu silnika odrzutowego
|
US10480322B2
(en)
*
|
2018-01-12 |
2019-11-19 |
General Electric Company |
Turbine engine with annular cavity
|
GB201807769D0
(en)
*
|
2018-05-14 |
2018-06-27 |
Rolls Royce Plc |
Electric ducted fan
|
US11060484B2
(en)
|
2018-06-29 |
2021-07-13 |
The Boeing Company |
Nozzle wall for an air-breathing engine of a vehicle and method therefor
|
GB201811852D0
(en)
|
2018-07-20 |
2018-09-05 |
Rolls Royce Plc |
Supersonic aircraft turbofan
|
US11261791B2
(en)
|
2019-02-25 |
2022-03-01 |
Rolls-Royce Corporation |
Hybrid propulsion cooling system
|
CN109854377B
(zh)
*
|
2019-04-08 |
2024-05-03 |
沈阳建筑大学 |
一种新型航空涡轮风扇发动机
|
CN109973244B
(zh)
*
|
2019-05-12 |
2024-07-05 |
西北工业大学 |
自驱动外涵道对转环形扇叶压缩装置
|
CN110552786B
(zh)
*
|
2019-09-18 |
2020-06-19 |
南京航空航天大学 |
具有锯齿状唇口的超声速轴对称进气道及设计方法
|
CA3159326A1
(en)
*
|
2019-10-29 |
2021-05-06 |
Organoworld Inc. |
Segmented augmented turbine assembly
|
US20220213802A1
(en)
|
2021-01-06 |
2022-07-07 |
General Electric Company |
System for controlling blade clearances within a gas turbine engine
|
US11674396B2
(en)
|
2021-07-30 |
2023-06-13 |
General Electric Company |
Cooling air delivery assembly
|
CN113565649A
(zh)
*
|
2021-08-16 |
2021-10-29 |
中国科学院工程热物理研究所 |
一种带Flade风扇和核心机驱动风扇级的三涵道ACE发动机
|
US11920500B2
(en)
|
2021-08-30 |
2024-03-05 |
General Electric Company |
Passive flow modulation device
|
CN113738530B
(zh)
*
|
2021-10-15 |
2022-06-17 |
清华大学 |
带叶尖风扇的多涵道航空发动机机匣结构
|
CN113847163B
(zh)
*
|
2021-10-25 |
2024-02-23 |
中国航发沈阳发动机研究所 |
一种航空发动机风扇外涵道引射系统
|
US11692448B1
(en)
|
2022-03-04 |
2023-07-04 |
General Electric Company |
Passive valve assembly for a nozzle of a gas turbine engine
|
CN114856856B
(zh)
*
|
2022-05-06 |
2024-04-30 |
中国科学院工程热物理研究所 |
一种高升限低油耗中等涵道比变循环发动机
|
CN117738814B
(zh)
*
|
2024-02-21 |
2024-05-17 |
中国航发四川燃气涡轮研究院 |
带叶尖风扇及串联压气机的变流路宽速域发动机
|