JP2002098002A5 - - Google Patents

Download PDF

Info

Publication number
JP2002098002A5
JP2002098002A5 JP2001156216A JP2001156216A JP2002098002A5 JP 2002098002 A5 JP2002098002 A5 JP 2002098002A5 JP 2001156216 A JP2001156216 A JP 2001156216A JP 2001156216 A JP2001156216 A JP 2001156216A JP 2002098002 A5 JP2002098002 A5 JP 2002098002A5
Authority
JP
Japan
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.)
Pending
Application number
JP2001156216A
Other languages
Japanese (ja)
Other versions
JP2002098002A (ja
Filing date
Publication date
Priority claimed from US09/579,818 external-priority patent/US6336319B1/en
Application filed filed Critical
Publication of JP2002098002A publication Critical patent/JP2002098002A/ja
Publication of JP2002098002A5 publication Critical patent/JP2002098002A5/ja
Pending legal-status Critical Current

Links

JP2001156216A 2000-05-26 2001-05-25 流体式ノズル制御装置 Pending JP2002098002A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/579,818 US6336319B1 (en) 2000-05-26 2000-05-26 Fluidic nozzle control system
US09/579818 2000-05-26

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2011223002A Division JP2012052548A (ja) 2000-05-26 2011-10-07 流体式ノズル制御装置

Publications (2)

Publication Number Publication Date
JP2002098002A JP2002098002A (ja) 2002-04-05
JP2002098002A5 true JP2002098002A5 (enExample) 2008-07-03

Family

ID=24318471

Family Applications (2)

Application Number Title Priority Date Filing Date
JP2001156216A Pending JP2002098002A (ja) 2000-05-26 2001-05-25 流体式ノズル制御装置
JP2011223002A Pending JP2012052548A (ja) 2000-05-26 2011-10-07 流体式ノズル制御装置

Family Applications After (1)

Application Number Title Priority Date Filing Date
JP2011223002A Pending JP2012052548A (ja) 2000-05-26 2011-10-07 流体式ノズル制御装置

Country Status (5)

Country Link
US (1) US6336319B1 (enExample)
EP (1) EP1158156B1 (enExample)
JP (2) JP2002098002A (enExample)
DE (1) DE60127756T2 (enExample)
ES (1) ES2284593T3 (enExample)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7159383B2 (en) * 2000-10-02 2007-01-09 Rohr, Inc. Apparatus, method and system for gas turbine engine noise reduction
US6758032B2 (en) 2002-02-07 2004-07-06 Lockheed Martin Corporation System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
US7296411B2 (en) * 2002-06-21 2007-11-20 Darko Segota Method and system for regulating internal fluid flow within an enclosed or semi-enclosed environment
US6655632B1 (en) 2002-08-27 2003-12-02 General Electric Company System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine
EP1585896B1 (en) * 2002-12-18 2012-07-25 Lockheed Martin Corporation Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
RU2241135C1 (ru) * 2003-03-19 2004-11-27 Государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" Способ возбуждения колебаний газа в выходном устройстве газотурбинного двигателя
US7308966B2 (en) * 2003-12-30 2007-12-18 General Electric Company Device for reducing jet engine exhaust noise using oscillating jets
US7412832B2 (en) * 2004-03-26 2008-08-19 General Electric Company Method and apparatus for operating gas turbine engines
US7481038B2 (en) * 2004-10-28 2009-01-27 United Technologies Corporation Yaw vectoring for exhaust nozzle
SE527829C2 (sv) * 2004-11-05 2006-06-13 Volvo Aero Corp Utloppsmunstycke till en jetmotor och förfarande för styrning av ett gasflöde från jetmotorn
EP1696116B1 (en) 2005-02-24 2018-04-11 Rolls-Royce plc Thrust vectoring using fluid jets
RU2296875C2 (ru) * 2005-03-05 2007-04-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Способ отклонения вектора тяги воздушно-реактивного двигателя
US7509797B2 (en) * 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
US7424805B2 (en) * 2005-04-29 2008-09-16 General Electric Company Supersonic missile turbojet engine
US7448199B2 (en) * 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
US7475545B2 (en) * 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
FR2887929B1 (fr) 2005-06-30 2010-12-03 Soc Nat Detude Et De Construction De Moteurs Daviation Snecma Tuyere a orientation de poussee
DE102006013595B4 (de) * 2006-03-22 2016-03-31 Danger Möricke Turbojet-Nachbrenner-und assoziierte Regelungssysteme
US7793504B2 (en) * 2006-05-04 2010-09-14 Rolls-Royce Corporation Nozzle with an adjustable throat
FR2904663B1 (fr) * 2006-08-01 2012-02-03 Snecma Turbomachine a double flux a variation artificielle de sa section de col
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
US7775460B2 (en) * 2006-10-24 2010-08-17 United Technologies Corporation Combustion nozzle fluidic injection assembly
US8096104B2 (en) * 2007-05-31 2012-01-17 United Technologies Corporation Fluidic vectoring for exhaust nozzle
EP2163754A1 (en) * 2008-09-16 2010-03-17 BAE Systems PLC Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine
PL2315928T3 (pl) 2008-07-04 2012-04-30 Bae Systems Plc Urządzenie do wektorowania ciągu w silniku odrzutowym, odpowiedni silnik odrzutowy, metoda wektorowania ciągu i metoda ulepszenia silnika odrzutowego
US8800259B2 (en) 2008-09-22 2014-08-12 Rolls-Royce North American Technologies, Inc. Thrust vector system
US8371104B2 (en) * 2008-10-10 2013-02-12 Lockheed Martin Corporation System and apparatus for vectoring nozzle exhaust plume from a nozzle
US9551296B2 (en) 2010-03-18 2017-01-24 The Boeing Company Method and apparatus for nozzle thrust vectoring
US8316631B2 (en) * 2010-09-30 2012-11-27 Lockheed Martin Corporation Exhaust plume heat effect reducing method and apparatus
US10060389B2 (en) 2010-12-14 2018-08-28 The Boeing Company Method and apparatus for variable exhaust nozzle exit area
US20120145808A1 (en) * 2010-12-14 2012-06-14 The Boeing Company Method and apparatus for variable exhaust nozzle exit area
US20130305731A1 (en) * 2012-05-17 2013-11-21 Philip John MORRIS Methods and apparatus for providing fluidic inserts into an exhaust stream to reduce jet noise from a nozzle
CN103644043A (zh) * 2012-12-22 2014-03-19 摩尔动力(北京)技术股份有限公司 质量增益喷管
CN203441604U (zh) * 2013-02-15 2014-02-19 通用电气公司 用于降低燃气涡轮系统中的背压的系统
CN103899433A (zh) * 2014-03-31 2014-07-02 西北工业大学 一种新型激波控制推力矢量喷管结构
US10563613B2 (en) 2015-08-31 2020-02-18 Rolls-Royce North American Technologies Inc. Coanda device for a round exhaust nozzle
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
US11001378B2 (en) 2016-08-08 2021-05-11 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
IL257811B (en) 2015-09-02 2022-08-01 Jetoptera Inc Pleoidal propulsion system
WO2017218841A1 (en) 2016-06-15 2017-12-21 The Regents Of The University Of California Two-dimensional supersonic nozzle thrust vectoring using staggered ramps
US10739002B2 (en) 2016-12-19 2020-08-11 General Electric Company Fluidic nozzle assembly for a turbine engine
CA3068569A1 (en) 2017-06-27 2019-01-03 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
US10807703B2 (en) * 2018-07-19 2020-10-20 General Electric Company Control system for an aircraft
CN117227987B (zh) * 2023-11-14 2024-03-12 中国空气动力研究与发展中心计算空气动力研究所 一种与操纵面一体化设计的单边膨胀尾喷槽

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA618830A (en) 1961-04-25 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Device for varying the effective area of a jet propulsion nozzle
US2699906A (en) 1949-10-25 1955-01-18 Northrop Aircraft Inc Air inlet for airplane gaseous combustion turbine engines
DE1043723B (de) * 1952-05-21 1958-11-13 Snecma Verfahren und Vorrichtung zum Beeinflussen des Querschnittes und/oder der Richtung des durch das Strahlrohr eines Rueckstossantriebes hindurchgehenden Gasstromkernes
FR1117244A (fr) 1954-12-20 1956-05-18 Snecma Soufflerie supersonique à nombre de mach variable
FR1182810A (fr) 1957-09-16 1959-06-30 Snecma Perfectionnements aux tuyères d'éjection à section réglable
DE1240747C2 (de) * 1962-02-08 1975-07-10 Societe Bertin & Cie., Paris Strahlschubduese fuer heisse gase mit strahlablenkung durch einfuehren eines hilfsstroemungsmittels
FR1332003A (enExample) * 1962-02-12 1963-12-16
FR1351404A (fr) * 1962-08-07 1964-02-07 Snecma Servo-valve aérodynamique ou hydrodynamique utilisable notamment pour la gouverne et la stabilisation des fusées
US3204405A (en) * 1964-02-20 1965-09-07 Raymond W Warren Three dimensional jet vectoring system
US3289410A (en) 1964-06-17 1966-12-06 William W Balwanz Method and apparatus for weeding the flame plasma of a rocket exhaust
GB1019203A (en) 1964-06-18 1966-02-02 Rolls Royce Jet nozzle
US3325103A (en) 1964-08-05 1967-06-13 Aerospace Corp Thrust vector control for reaction engines
US3425431A (en) * 1965-03-29 1969-02-04 American Standard Inc Control apparatus and methods
FR1456926A (fr) * 1965-09-17 1966-07-08 Bertin & Cie Perfectionnements apportés aux dispositifs de déviation de fluides et à leur application à la dilution
US3370794A (en) 1965-11-08 1968-02-27 Navy Usa Annular plenum nozzle for controlling trajectory of rockets
US3374954A (en) * 1966-03-03 1968-03-26 Thiokol Chemical Corp Nozzle cooling and thrust vector control apparatus
US3420060A (en) * 1966-04-22 1969-01-07 Mc Donnell Douglas Corp Pressure induced jet vectoring augmentation apparatus
US3421324A (en) * 1966-05-03 1969-01-14 Philco Ford Corp Fluid flow control apparatus
US3698642A (en) * 1966-11-04 1972-10-17 Thiokol Chemical Corp Thrust vector control system
US3740003A (en) * 1972-03-13 1973-06-19 Us Army Secondary injection/jet reaction control
US4077572A (en) * 1976-03-25 1978-03-07 Chandler Evans Inc. Reduced size altitude insensitive thrust vector control nozzle
JPS59728B2 (ja) * 1976-08-10 1984-01-09 晴海 浅尾 副噴流による流体の流動方向制御装置
US5664415A (en) 1994-06-01 1997-09-09 Lockheed Fort Worth Company After-burning turbo-fan engine with a fixed geometry exhaust nozzle having a variable flow coefficient
US6112513A (en) * 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow
US5996936A (en) * 1997-09-29 1999-12-07 General Electric Company Fluidic throat exhaust nozzle

Similar Documents

Publication Publication Date Title
BE2022C531I2 (enExample)
BE2022C547I2 (enExample)
BE2017C059I2 (enExample)
BE2017C057I2 (enExample)
BE2017C051I2 (enExample)
BE2017C032I2 (enExample)
BE2012C050I2 (enExample)
BE2007C047I2 (enExample)
AU2002307149A8 (enExample)
BE2011C034I2 (enExample)
JP2001271792A5 (enExample)
JP2002174474A5 (enExample)
JP2002098002A5 (enExample)
BRPI0209186B1 (enExample)
JP2002011871A5 (enExample)
BRPI0204884A2 (enExample)
JP2002149673A5 (enExample)
CH1379220H1 (enExample)
JP2002223412A5 (enExample)
BRPI0101486B8 (enExample)
BE2012C051I2 (enExample)
BRPI0210463A2 (enExample)
AU2000280389A8 (enExample)
JP2002240059A5 (enExample)
JP2002135617A5 (enExample)