BR0210206A - Inversor de empuxo de carenagem pivÈ - Google Patents

Inversor de empuxo de carenagem pivÈ

Info

Publication number
BR0210206A
BR0210206A BR0210206-4A BR0210206A BR0210206A BR 0210206 A BR0210206 A BR 0210206A BR 0210206 A BR0210206 A BR 0210206A BR 0210206 A BR0210206 A BR 0210206A
Authority
BR
Brazil
Prior art keywords
pivè
pivots
inverter
fairing
conduit
Prior art date
Application number
BR0210206-4A
Other languages
English (en)
Other versions
BR0210206B1 (pt
Inventor
Rodger L Modglin
Frederick H Peters
Original Assignee
Nordam Group Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Nordam Group Inc filed Critical Nordam Group Inc
Publication of BR0210206A publication Critical patent/BR0210206A/pt
Publication of BR0210206B1 publication Critical patent/BR0210206B1/pt

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
    • F02K1/54—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
    • F02K1/625—Reversing jet main flow by blocking the rearward discharge by means of flaps the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • 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
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • 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)
  • Power-Operated Mechanisms For Wings (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Seal Device For Vehicle (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Sealing Devices (AREA)

Abstract

"INVERSOR DE EMPUXO DE CARENAGEM PIVÈ". Um inversor de empuxo (18) inclui um par de portas (34) cobrindo portais correspondentes (32) em um conduto (20) de exaustão entre um bico de entrada (26) e um bico de saída (28) em suas extremidades opostas. O conduto inclui também um par de vigas laterais (30) tendo acionadores (38) montados nas mesmas, e unidos operativamente às portas para rotação seletiva das mesmas em torno de pivós correspondentes (36) . Carenagens (42) de bolha são dispostas dentro do conduto e unem, de forma vedada, as portas às vigas em torno de pivós respectivos, dentre os pivós.
BRPI0210206-4A 2001-06-08 2002-06-07 inversor de empuxo de carenagem pivÈ. BR0210206B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/877.826 2001-06-08
US09/877,826 US6487845B1 (en) 2001-06-08 2001-06-08 Pivot fairing thrust reverser
PCT/US2002/017979 WO2002101222A1 (en) 2001-06-08 2002-06-07 Pivot fairing thrust reverser

Publications (2)

Publication Number Publication Date
BR0210206A true BR0210206A (pt) 2004-04-27
BR0210206B1 BR0210206B1 (pt) 2011-09-06

Family

ID=25370802

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0210206-4A BR0210206B1 (pt) 2001-06-08 2002-06-07 inversor de empuxo de carenagem pivÈ.

Country Status (5)

Country Link
US (1) US6487845B1 (pt)
EP (1) EP1399661B1 (pt)
BR (1) BR0210206B1 (pt)
CA (1) CA2448767C (pt)
WO (1) WO2002101222A1 (pt)

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2823259B1 (fr) * 2001-04-05 2003-06-27 Hispano Suiza Sa Systeme de verrouillage synchronise des portes d'un inverseur de poussee
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit
US7278258B2 (en) * 2004-11-12 2007-10-09 Honeywell International, Inc. Floating flexible firewall seal
FR2887854B1 (fr) * 2005-06-30 2008-08-08 Airbus France Sas Nacelle pour aeronef et aeronef muni d'au moins une telle nacelle
US8015797B2 (en) 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine
US20080083210A1 (en) * 2006-10-04 2008-04-10 Spirit Aerosystems, Inc Monolithic thrust reverser components
US8127529B2 (en) * 2007-03-29 2012-03-06 United Technologies Corporation Variable area fan nozzle and thrust reverser
FR2914956A1 (fr) * 2007-04-12 2008-10-17 Aircelle Sa Nacelle pour turboreacteur equipee d'un systeme d'inversion de poussee a porte
US9759087B2 (en) 2007-08-08 2017-09-12 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
CN101939528B (zh) * 2007-08-08 2013-07-24 罗尔股份有限公司 具有旁通流的面积可调风扇喷嘴
FR2920199B1 (fr) * 2007-08-20 2009-10-30 Aircelle Sa Capot mobile d'inverseur de poussee et inverseur de poussee equipe d'un tel capot mobile
US7878451B2 (en) * 2007-11-15 2011-02-01 Spirit Aerosystems, Inc. Low-leakage seal system for pivot door type thrust reverser
US8091827B2 (en) 2007-11-16 2012-01-10 The Nordam Group, Inc. Thrust reverser door
US7735778B2 (en) * 2007-11-16 2010-06-15 Pratt & Whitney Canada Corp. Pivoting fairings for a thrust reverser
US8172175B2 (en) * 2007-11-16 2012-05-08 The Nordam Group, Inc. Pivoting door thrust reverser for a turbofan gas turbine engine
US8051639B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser
US8052085B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
US8052086B2 (en) 2007-11-16 2011-11-08 The Nordam Group, Inc. Thrust reverser door
US8002217B2 (en) * 2007-11-16 2011-08-23 Spirit Aerosystems, Inc. System for adjustment of thrust reverser pivot door
US8127530B2 (en) 2008-06-19 2012-03-06 The Nordam Group, Inc. Thrust reverser for a turbofan gas turbine engine
FR2935444B1 (fr) * 2008-09-02 2010-09-10 Airbus France Inverseur de poussee et nacelle pour aeronef muni d'au moins un tel inverseur
DE102008045851A1 (de) 2008-09-05 2010-03-11 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung zum Öffnen und Schließen einer Schubumkehrertür eines Strahltriebwerks
US9108711B2 (en) * 2009-03-23 2015-08-18 Southern Methodist University Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets
US20140053533A1 (en) * 2012-08-21 2014-02-27 Gabriel L. Suciu Reverse flow gas turbine engine with thrust reverser
WO2014074143A1 (en) * 2012-11-12 2014-05-15 United Technologies Corporation Aircraft with forward sweeping t-tail
US10202941B2 (en) * 2012-11-12 2019-02-12 United Technologies Corporation Reverse core turbine engine mounted above aircraft wing
US9944401B2 (en) * 2012-12-11 2018-04-17 United Technologies Corporation Asymmetric thrust reversers
US9845159B2 (en) * 2013-03-07 2017-12-19 United Technologies Corporation Conjoined reverse core flow engine arrangement
US9394802B2 (en) * 2013-03-10 2016-07-19 United Technologies Corporation Sensor hoop storage and transport apparatus
EP2971728B1 (en) * 2013-03-14 2020-09-02 United Technologies Corporation Twin target thrust reverser module
US10040563B1 (en) * 2013-04-11 2018-08-07 Geoffrey P. Pinto Dual panel actuator system for jet engines
FR3019591B1 (fr) * 2014-04-08 2020-07-17 Safran Nacelles Dispositif d’inversion de poussee a portes pour nacelle de turboreacteur d’aeronef
DE102015206093A1 (de) * 2015-04-02 2016-10-06 Rolls-Royce Deutschland Ltd & Co Kg Triebwerksverkleidung einer Fluggasturbine
FR3063522B1 (fr) * 2017-03-06 2021-05-07 Safran Nacelles Dispositif d'actionnement d'un inverseur de poussee a organe d'antideploiement
US10907577B2 (en) 2017-10-23 2021-02-02 Rohr, Inc. Translating lock for pivot door thrust reverser
US10641208B2 (en) * 2017-11-27 2020-05-05 Rohr, Inc. Translating nozzle for mixed flow turbofan engine
US10704495B2 (en) * 2017-11-27 2020-07-07 Rohr, Inc. Pre-exit pivot door thrust reverser
US10724474B2 (en) * 2018-05-01 2020-07-28 Rohr, Inc. Hybrid articulating/translating trailing edge reverser
US11286879B2 (en) * 2018-07-02 2022-03-29 Rohr, Inc. Target door reverser wit h non-parallel hinge lines
US11346304B2 (en) * 2018-09-06 2022-05-31 Rohr, Inc. Thrust reverser single degree of freedom actuator mechanism systems and methods
US11300077B2 (en) 2018-10-02 2022-04-12 Rohr, Inc. Deployable fairing for door reversers systems and methods
US11333102B2 (en) 2018-09-06 2022-05-17 Rohr, Inc. Thrust reverser actuation arrangement and deployable fairing systems and methods
EP4116524A1 (en) * 2021-07-05 2023-01-11 Rohr, Inc. S-hook latch
FR3130327B1 (fr) * 2021-12-15 2024-07-26 Safran Nacelles Inverseur de poussée à porte d’une nacelle de turboréacteur d’aéronef à organe de déviation des fluides vers l’extérieur
US12025074B1 (en) 2023-08-14 2024-07-02 Rolls-Royce North American Technologies Inc. Plug nozzle for high mach gas turbine engines
US11891964B1 (en) 2023-08-14 2024-02-06 Rolls-Royce North American Technologies Inc. Method of manufacture of plug nozzle with thrust reverser

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2680948A (en) 1948-08-30 1954-06-15 Engineering & Res Corp Variable area tail pipe for jet engines
US2847823A (en) 1955-03-15 1958-08-19 Curtiss Wright Corp Reverse thrust nozzle construction
GB1130268A (en) * 1967-07-01 1968-10-16 Rolls Royce Improvements in or relating to gas turbine by-pass engines
US4182501A (en) 1977-03-04 1980-01-08 Astech Thrust reverser for jet engine forming active extension of jet tube
FR2494775B1 (fr) 1980-11-27 1985-07-05 Astech Dispositif pour la commande d'un inverseur de poussee pour moteur a reaction
FR2601077B1 (fr) 1986-07-07 1988-10-21 Hurel Dubois Avions Structure d'ejection des gaz pour moteur a reaction notamment pour reacteur a double flux.
FR2696212B3 (fr) 1992-09-28 1994-12-02 Avions Hurel Dubois Constructi Ensemble d'inversion de poussée à portes pour moteur d'avion incorporant une barrière thermique.
FR2736390B1 (fr) * 1995-07-05 1997-08-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a une coquille
DE69514224T2 (de) 1995-09-13 2000-08-10 Societe De Construction Des Avions Hurel-Dubois (S.A.), Meudon-La-Foret Elektrohydraulische Schubumkehrvorrichtung mit zwei Klappen
US5794433A (en) * 1996-06-18 1998-08-18 The Nordam Group, Inc. Thrust reverser door side fillers
US6260801B1 (en) * 1999-09-17 2001-07-17 The Nordam Group, Inc. Swing pivot thrust reverser

Also Published As

Publication number Publication date
US20020184874A1 (en) 2002-12-12
EP1399661B1 (en) 2013-11-06
BR0210206B1 (pt) 2011-09-06
US6487845B1 (en) 2002-12-03
CA2448767A1 (en) 2002-12-19
WO2002101222A1 (en) 2002-12-19
EP1399661A1 (en) 2004-03-24
EP1399661A4 (en) 2010-04-28
CA2448767C (en) 2007-10-02

Similar Documents

Publication Publication Date Title
BR0210206A (pt) Inversor de empuxo de carenagem pivÈ
DE69509344D1 (de) Schubumkehrvorrichtung mit schwenkbaren, gebogenen Klappen
NZ502346A (en) Watercraft with transversely oscillating flexible flappers
BRPI0520757B8 (pt) artigo absorvente reconectável tipo calça e método para fazê-lo
FR2719554B1 (fr) Rotor anti-couple caréné à pales flottantes.
NL192827B (nl) Binnenas-achterafdichting voor schepen met twee concentrische, contra-roterende schroefassen.
ATE197687T1 (de) Hexapod-bearbeitungszentrum
SE8406040D0 (sv) Propelleranordning
NO985589L (no) Brostabilisering
FI950321A0 (fi) Ilmentämisjärjestelmä, integraatiovektori ja tällä integraatiovektorilla transformoitu solu
WO1998018371A3 (en) Foldable shirt hanger
IT8423838A0 (it) Sistema compatto di entrata del gas fresco, per motori con sovralimentazione combinata.
NO962799L (no) Sammenrullbart eller sammenleggbart bæreelement
DE60012325D1 (de) Schnittwinkeleinstellvorrichtung
NO20023598L (no) Forbindelsesinnretning
MacMartin et al. Active impedance matching of complex structural systems
Lent et al. Some processes of sound generation in a vortex-airfoil system with parallel axes
ATE400072T1 (de) Entfaltbare tragkonstruktion
ITTO930848A0 (it) Giunto flessibile per tubazioni di scarico, in particolare di motori di veicoli.
Anal Jorgensen, PET (1-IA); Schmitt, LM; Werner, RF (D-OSNB-P) Positive representations of general commutation relations allowing Wick ordering.(English. English summary)
BR0102797A (pt) Processamento contìnuo de lâminas de eva expandida
ES1031702U (es) Perchero mural perfeccionado.
RU92008892A (ru) Лаговый паром
Barche New structuralization and work of current interest in the research area of fluid mechanics
ITPI950020V0 (it) Basamento coperto atto al ricovero di ali di deltaplani u.l.m., provvisti di motore, detti pendolari, e non provvisti come quelli per il volo libero

Legal Events

Date Code Title Description
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 07/06/2002, OBSERVADAS AS CONDICOES LEGAIS.

B24B Patent annual fee: requirement for complementing annual fee

Free format text: REFERENTE A 11A ANUIDADE DE 14 - 06 - 2012 GUIA NO 221203850918.

B24D Patent annual fee: restoration after fee payment
B25G Requested change of headquarter approved

Owner name: THE NORDAM GROUP, INC. (US)

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 19A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2623 DE 13-04-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.