DE69734423D1 - Feuerhemmende Labyrinthdichtung für Flugzeuge - Google Patents

Feuerhemmende Labyrinthdichtung für Flugzeuge

Info

Publication number
DE69734423D1
DE69734423D1 DE69734423T DE69734423T DE69734423D1 DE 69734423 D1 DE69734423 D1 DE 69734423D1 DE 69734423 T DE69734423 T DE 69734423T DE 69734423 T DE69734423 T DE 69734423T DE 69734423 D1 DE69734423 D1 DE 69734423D1
Authority
DE
Germany
Prior art keywords
retardant
aircraft
fire
labyrinth seal
labyrinth
Prior art date
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.)
Expired - Lifetime
Application number
DE69734423T
Other languages
English (en)
Other versions
DE69734423T2 (de
DE69734423T3 (de
Inventor
Kurt R Kraft
Gary L Vieth
Peter J Louden
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=24857418&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69734423(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE69734423D1 publication Critical patent/DE69734423D1/de
Publication of DE69734423T2 publication Critical patent/DE69734423T2/de
Publication of DE69734423T3 publication Critical patent/DE69734423T3/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24—Heat or noise insulation
    • F02C7/25—Fire protection or prevention
    • 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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Tires In General (AREA)
  • Gasket Seals (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE69734423T 1996-09-10 1997-08-29 Feuerhemmende Labyrinthdichtung für Flugzeuge Expired - Lifetime DE69734423T3 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US08/711,276 US5910094A (en) 1996-09-10 1996-09-10 Aircraft labyrinth fire seal
US711276 1996-09-10
EP97202643A EP0835805B2 (de) 1996-09-10 1997-08-29 Feuerhemmende Labyrinthdichtung für Flugzeuge

Publications (3)

Publication Number Publication Date
DE69734423D1 true DE69734423D1 (de) 2005-12-01
DE69734423T2 DE69734423T2 (de) 2006-07-06
DE69734423T3 DE69734423T3 (de) 2012-02-09

Family

ID=24857418

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69734423T Expired - Lifetime DE69734423T3 (de) 1996-09-10 1997-08-29 Feuerhemmende Labyrinthdichtung für Flugzeuge

Country Status (4)

Country Link
US (1) US5910094A (de)
EP (1) EP0835805B2 (de)
CA (1) CA2213792C (de)
DE (1) DE69734423T3 (de)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6983912B2 (en) * 2002-04-30 2006-01-10 The Boeing Company Hybrid exhaust heat shield for pylon mounted gas turbine engines
WO2005099999A2 (en) * 2004-04-12 2005-10-27 Xtreme Seal, Llc Compositions and methods for sealing
US20060032974A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Modular installation kit for auxiliary power unit
US7526921B2 (en) * 2005-03-29 2009-05-05 Honeywell International Inc. Auxiliary power unit with integral firebox
US20070056292A1 (en) * 2005-09-14 2007-03-15 Honeywell International, Inc. Auxiliary power unit case flange to cone bolt adapter
US20070200030A1 (en) * 2006-02-24 2007-08-30 Mcfarlane Daniel S Aircraft baffle seal
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2973439B1 (fr) 2011-03-30 2014-08-22 Aircelle Sa Ensemble de joint d'etancheite anti-feu et nacelle comprenant un tel joint
FR2985501B1 (fr) 2012-01-05 2013-12-27 Aircelle Sa Joint d'etancheite pour pylone et nacelle de turboreacteur et ensemble de pylone et nacelle de turboreacteur incorporant un tel joint d'etancheite
US9835090B2 (en) 2012-09-18 2017-12-05 United Technologies Corporation Fire seal for a gas turbine engine
EP2901001B1 (de) 2012-09-28 2019-12-04 United Technologies Corporation Dreieckige blockierelemente für klappen eines schubumkehrsystems
FR2996823B1 (fr) 2012-10-15 2014-11-21 Snecma Protection thermique demontable en ligne pour un palonnier de suspension d'une turbomachine
FR3001197A1 (fr) * 2013-01-22 2014-07-25 Airbus Operations Sas Ensemble propulsif d'un aeronef comprenant au moins un joint a brosse resistant aux hautes temperatures
JP6114042B2 (ja) * 2013-01-25 2017-04-12 三菱航空機株式会社 航空機の防火壁、パイロン、及び、航空機
US9889323B2 (en) * 2013-03-13 2018-02-13 The Boeing Company Fire seal end cap and associated multi-member assembly and method
FR3005696B1 (fr) 2013-05-17 2015-05-01 Aircelle Sa Tuyere d'ejection de gaz chauds pour un turboreacteur, comportant sur l'exterieur un deflecteur de ces gaz
FR3014840B1 (fr) 2013-12-17 2017-10-13 Airbus Operations Sas Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage
FR3015431B1 (fr) * 2013-12-19 2017-12-15 Airbus Operations Sas Structure primaire de mat d'accrochage renforcee.
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
US9643733B2 (en) 2014-06-17 2017-05-09 The Boeing Company Fire seal for an aircraft
US9896970B2 (en) * 2014-11-14 2018-02-20 General Electric Company Method and system for sealing an annulus
US11053614B2 (en) 2015-06-16 2021-07-06 The Boeing Company Single-layer ceramic-based knit fabric for high temperature bulb seals
US10167741B2 (en) 2015-11-03 2019-01-01 Rohr, Inc. Nacelle fluid drain
US9976484B2 (en) * 2015-12-28 2018-05-22 United Technologies Corporation Core compartment ventilation devices for nacelles of gas turbine engines for cooling a core compartment of a gas turbine engine
US10337130B2 (en) 2016-02-01 2019-07-02 The Boeing Company Metal alloy knit fabric for high temperature insulating materials
FR3053957B1 (fr) 2016-07-12 2018-08-31 Safran Nacelles Ensemble arriere de nacelle de turboreacteur comportant un dispositif d'etancheite anti-feu
JP6830804B2 (ja) * 2016-12-05 2021-02-17 三菱航空機株式会社 航空機用のファイアシール構造および航空機
FR3064605A1 (fr) * 2017-03-28 2018-10-05 Airbus Operations Systeme de joints feu metalliques pour une attache moteur d'un aeronef
US10787922B2 (en) 2018-05-02 2020-09-29 Rohr, Inc. Tubular seal with wavy shroud for an aircraft propulsion system
FR3083213B1 (fr) 2018-06-29 2020-10-02 Safran Aircraft Engines Dispositif de resistance au feu ameliore destine a etre interpose entre une extremite de mat d'accrochage de turbomachine d'aeronef, et un capotage de la turbomachine delimitant un compartiment inter-veine
US11118705B2 (en) 2018-08-07 2021-09-14 General Electric Company Quick connect firewall seal for firewall
FR3085183B1 (fr) * 2018-08-22 2020-09-11 Safran Nacelles Dispositif anti-feu de fermeture d’espaces au niveau de jointures d’une nacelle et nacelle comprenant un tel dispositif
US11008089B2 (en) * 2018-10-24 2021-05-18 Gulfstream Aerospace Corporation Fireproof pressure relief assembly
US11156097B2 (en) * 2019-02-20 2021-10-26 General Electric Company Turbomachine having an airflow management assembly
US11156165B2 (en) 2019-06-13 2021-10-26 The Boeing Company Fire seal assemblies for aircraft engines
US11548653B2 (en) * 2019-10-08 2023-01-10 Rohr, Inc. Support structure for inner cowls of an aircraft propulsion system
US11674599B2 (en) 2020-07-15 2023-06-13 The Boeing Company Seal assembly including shape memory stiffening members
US11592112B2 (en) 2020-07-15 2023-02-28 The Boeing Company Labyrinth barrier with members constructed of a shape memory material
US11598419B2 (en) 2020-07-15 2023-03-07 The Boeing Company Seal assembly with actuation members constructed of shape memory material

Family Cites Families (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1419927A (en) * 1918-05-24 1922-06-20 Westinghouse Electric & Mfg Co Packing
US1626237A (en) * 1921-07-02 1927-04-26 Westinghouse Electric & Mfg Co Turbine gland
US2544538A (en) * 1948-12-01 1951-03-06 Wright Aeronautical Corp Liner for hot gas chambers
GB723936A (en) * 1952-07-01 1955-02-16 West Midlands Gas Board Improved flame and explosion traps
US2997845A (en) * 1957-03-22 1961-08-29 Rolls Royce Jet propulsion nozzle adjustable to give forward and reverse thrusts
US2986878A (en) * 1957-08-08 1961-06-06 Chance Vought Corp Firewall
US3020185A (en) † 1958-07-28 1962-02-06 Connecticut Hard Rubber Co Wire reinforced polytetrafluoroethylene seal
FR1376576A (fr) * 1963-08-02 1964-10-31 Snecma Silencieux pour réacteurs
US3409228A (en) * 1966-02-10 1968-11-05 Gen Electric Ejector nozzle
FR1525355A (fr) * 1967-04-07 1968-05-17 Breguet Aviat Silencieux débrayable pour avion à réaction
FR1547756A (fr) * 1967-10-19 1968-11-29 Snecma Silencieux pour réacteurs aéronautiques
US3583730A (en) * 1968-08-09 1971-06-08 Gen Connector Corp Dual fire resistant seal
FR2061849A5 (de) * 1969-06-30 1971-06-25 Bertin & Cie
US3647020A (en) * 1970-02-02 1972-03-07 Rohr Corp Jet propulsion apparatus and operating method
US3637041A (en) * 1970-09-02 1972-01-25 Rohr Corp Sound suppression system for fan jet engines
US3695387A (en) * 1970-09-08 1972-10-03 Rohr Corp Sound suppression system for fan jet engines
GB1291939A (en) * 1970-11-30 1972-10-04 Rolls Royce Flame shield for a gas turbine engine
US3664455A (en) * 1971-03-15 1972-05-23 Rohr Corp Twisted vane sound suppressor for aircraft jet engine
US3774868A (en) * 1972-12-11 1973-11-27 G Goetz Integrated nozzle
US3897169A (en) * 1973-04-19 1975-07-29 Gen Electric Leakage control structure
GB1474030A (en) * 1973-09-22 1977-05-18 Rolls Royce Fire seal
US4175640A (en) * 1975-03-31 1979-11-27 Boeing Commercial Airplane Company Vortex generators for internal mixing in a turbofan engine
DE7523365U (de) * 1975-07-23 1975-11-13 Deutsche Metalltueren Werke Schwarze A Ag Zweiflügeliges feuerschutztor mit in einem flügel angeordneter schlupftür
US4095417A (en) * 1976-08-23 1978-06-20 Avco Corporation Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine
US4165609A (en) * 1977-03-02 1979-08-28 The Boeing Company Gas turbine mixer apparatus
US4215536A (en) * 1978-12-26 1980-08-05 The Boeing Company Gas turbine mixer apparatus
US4361296A (en) * 1980-03-10 1982-11-30 The Boeing Company Uniflange coupling assembly
US4422524A (en) * 1982-03-22 1983-12-27 Lockheed Corporation Variable shape, fluid flow nozzle for sound suppression
US4537026A (en) * 1982-04-07 1985-08-27 Rolls-Royce Inc. Variable area nozzles for turbomachines
US4477088A (en) * 1982-12-20 1984-10-16 United Technologies Corporation Face seal means with back-up seal
US4690329A (en) * 1984-11-02 1987-09-01 United Technologies Corporation Exhaust nozzle coupled with reverser exhaust door
US5251917A (en) * 1987-06-22 1993-10-12 The Boeing Company Fire-resistant seal
US4819876A (en) * 1987-06-25 1989-04-11 United Technologies Corporation Divergent flap actuation system for a two-dimensional exhaust nozzle
US5044559A (en) * 1988-11-02 1991-09-03 United Technologies Corporation Gas assisted liquid atomizer
US5154052A (en) * 1990-05-07 1992-10-13 General Electric Company Exhaust assembly for a high speed civil transport aircraft engine
US5156360A (en) * 1991-04-08 1992-10-20 The Boeing Company Flexible fire seal for overlapping cowl side edges
US5291672A (en) * 1992-12-09 1994-03-08 General Electric Company Sound suppression mixer
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
US5524846A (en) * 1993-12-21 1996-06-11 The Boeing Company Fire protection system for airplanes
US5690279A (en) * 1995-11-30 1997-11-25 United Technologies Corporation Thermal relief slot in sheet metal

Also Published As

Publication number Publication date
DE69734423T2 (de) 2006-07-06
EP0835805A3 (de) 2001-05-09
EP0835805B1 (de) 2005-10-26
DE69734423T3 (de) 2012-02-09
EP0835805A2 (de) 1998-04-15
CA2213792A1 (en) 1998-03-10
CA2213792C (en) 2005-04-12
EP0835805B2 (de) 2011-09-07
US5910094A (en) 1999-06-08

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