BR9205410A - Componente estrutural de avião, capota dianteira de nacela de um motor de avião e capota dianteira de motor de avião - Google Patents

Componente estrutural de avião, capota dianteira de nacela de um motor de avião e capota dianteira de motor de avião

Info

Publication number
BR9205410A
BR9205410A BR9205410A BR9205410A BR9205410A BR 9205410 A BR9205410 A BR 9205410A BR 9205410 A BR9205410 A BR 9205410A BR 9205410 A BR9205410 A BR 9205410A BR 9205410 A BR9205410 A BR 9205410A
Authority
BR
Brazil
Prior art keywords
airplane
front hood
engine
structural component
airplane engine
Prior art date
Application number
BR9205410A
Other languages
English (en)
Inventor
Michael John Arnold
Derek Cole
Original Assignee
Short Brothers Plc
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 Short Brothers Plc filed Critical Short Brothers Plc
Publication of BR9205410A publication Critical patent/BR9205410A/pt

Links

Classifications

    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
    • B64D15/04—Hot gas application
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Paints Or Removers (AREA)
  • Bridges Or Land Bridges (AREA)
  • Laminated Bodies (AREA)
BR9205410A 1991-09-20 1992-09-17 Componente estrutural de avião, capota dianteira de nacela de um motor de avião e capota dianteira de motor de avião BR9205410A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB919120113A GB9120113D0 (en) 1991-09-20 1991-09-20 Thermal antiicing of aircraft structures
PCT/GB1992/001710 WO1993006005A1 (en) 1991-09-20 1992-09-17 Thermal anti-icing of aircraft structures

Publications (1)

Publication Number Publication Date
BR9205410A true BR9205410A (pt) 1994-06-07

Family

ID=10701737

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9205410A BR9205410A (pt) 1991-09-20 1992-09-17 Componente estrutural de avião, capota dianteira de nacela de um motor de avião e capota dianteira de motor de avião

Country Status (10)

Country Link
US (1) US5400984A (pt)
EP (1) EP0558726B1 (pt)
JP (1) JPH06502825A (pt)
AU (1) AU655077B2 (pt)
BR (1) BR9205410A (pt)
CA (1) CA2095530A1 (pt)
DE (1) DE69207889D1 (pt)
GB (2) GB9120113D0 (pt)
IL (1) IL103208A (pt)
WO (1) WO1993006005A1 (pt)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6003814A (en) * 1996-06-17 1999-12-21 Seniors Flexonics Inc. Stainless Steel Products Division Double-walled duct assembly for aircraft anti-icing conduit systems
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2771451B1 (fr) * 1997-11-21 2000-04-14 Aerospatiale Dispositif de protection pour capot d'entree d'air de moteur a reaction, pourvu d'un systeme de degivrage
FR2771452B1 (fr) * 1997-11-21 2000-04-14 Aerospatiale Dispositif de degivrage pour capot d'entree d'air de moteur a reaction
FR2771776B1 (fr) * 1997-12-02 2000-01-28 Aerospatiale Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage
US6688558B2 (en) 1999-11-23 2004-02-10 The Boeing Company Method and apparatus for aircraft inlet ice protection
US6371411B1 (en) 1999-11-23 2002-04-16 The Boeing Company Method and apparatus for aircraft inlet ice protection
FR2802573B1 (fr) 1999-12-21 2002-02-15 Aerospatiale Matra Airbus Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage
FR2823533B1 (fr) * 2001-04-17 2003-08-08 Eads Airbus Sa Capot d'entree d'air pour moteur a reaction, pourvu de moyens de degivrage
GB0211800D0 (en) 2002-05-22 2002-07-03 Short Brothers Plc An ice protection system for aircraft structures
US6910659B2 (en) * 2002-10-22 2005-06-28 The Boeing Company Method and apparatus for liquid containment, such as for aircraft fuel vessels
US7175136B2 (en) * 2003-04-16 2007-02-13 The Boeing Company Method and apparatus for detecting conditions conducive to ice formation
CA2535885C (en) * 2003-08-20 2014-04-15 The Boeing Company Methods and systems for detecting icing conditions
US7137240B2 (en) * 2004-08-18 2006-11-21 Hamilton Sundstrand Corporation Inlet muff anti-icing system for an auxiliary power unit
EP1657156A1 (en) * 2004-11-16 2006-05-17 Saab Ab An air intake appliance for an aircraft engine
US7331421B2 (en) * 2005-03-30 2008-02-19 The Boeing Company Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods
FR2886674B1 (fr) * 2005-06-07 2007-08-03 Airbus France Sas Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
FR2887294B1 (fr) * 2005-06-21 2007-08-10 Airbus France Sas Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
US7900872B2 (en) * 2007-12-12 2011-03-08 Spirit Aerosystems, Inc. Nacelle inlet thermal anti-icing spray duct support system
FR2928695B1 (fr) * 2008-03-13 2012-06-29 Aircelle Sa Dispositif d'acheminement d'air sous pression entre un moteur d'aeronef et un compartiment de degivrage d'une structure d'entree d'air de nacelle
US8769924B2 (en) 2008-05-30 2014-07-08 United Technologies Corporation Gas turbine engine assembly including accessory components within the nacelle
GB0812562D0 (en) * 2008-07-10 2008-08-13 Airbus Uk Ltd A Connector for an aircraft fuel pipe
GB2462826B (en) * 2008-08-20 2014-03-12 Rolls Royce Plc A method for detecting overpressure inside a compartment associated with a gas turbine nacelle
US8061657B2 (en) * 2008-12-31 2011-11-22 General Electric Company Method and apparatus for aircraft anti-icing
FR2954279B1 (fr) * 2009-12-18 2014-08-22 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises
FR2961483B1 (fr) * 2010-06-18 2013-01-18 Aircelle Sa Carter de soufflante de turboreacteur d'aeronef
JP5582927B2 (ja) * 2010-08-30 2014-09-03 三菱重工業株式会社 航空機の防除氷システム及びこれを備える航空機
DE102011102458A1 (de) * 2011-05-24 2012-11-29 Rolls-Royce Deutschland Ltd & Co Kg Enteisungsvorrichtung eines Fluggasturbinentriebwerks
US20140263837A1 (en) * 2013-03-12 2014-09-18 Spirit Aerosystems, Inc. Nacelle inlet thermal anti-ice spray duct
FR3004485B1 (fr) 2013-04-11 2015-05-08 Snecma Dispositif de degivrage d'un bec de separation de turbomachine aeronautique
US9528442B2 (en) * 2013-08-21 2016-12-27 The Boeing Company Aircraft engine anti-icing (EAI) barrier assembly, system and method
FR3021350B1 (fr) * 2014-05-20 2016-07-01 Snecma Procede de detection de fuite de fluide dans une turbomachine et systeme de distribution de fluide
US10399684B2 (en) * 2014-10-29 2019-09-03 The Boeing Company Induction heating coils with uniform heating
FR3031141B1 (fr) * 2014-12-24 2017-02-10 Snecma Procede de detection de fuite de fluide dans une turbomachine et systeme de distribution de fluide
ITUB20151085A1 (it) * 2015-05-28 2016-11-28 Alenia Aermacchi Spa Gondola per motore aeronautico con sistema antighiaccio utilizzante un fluido bifase.
US10189572B2 (en) * 2016-05-02 2019-01-29 The Boeing Company Systems and methods for preventing ice formation on portions of an aircraft
US10458275B2 (en) * 2017-01-06 2019-10-29 Rohr, Inc. Nacelle inner lip skin with heat transfer augmentation features
US10655539B2 (en) * 2017-10-16 2020-05-19 Rolls-Royce North America Technologies Inc. Aircraft anti-icing system
US11408341B2 (en) * 2018-11-05 2022-08-09 Rohr, Inc. Anti-icing system for an aircraft nacelle
US11220344B2 (en) * 2018-12-17 2022-01-11 Rohr, Inc. Anti-ice double walled duct system
US10989116B2 (en) * 2019-03-05 2021-04-27 Rohr, Inc. Inlet anti-ice double walled duct with supply line seal

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2556736A (en) * 1945-06-22 1951-06-12 Curtiss Wright Corp Deicing system for aircraft
GB622627A (en) * 1947-04-02 1949-05-04 Armstrong Siddeley Motors Ltd Means for preventing an internal-combustion turbine unit from icing
DE1281270B (de) * 1966-04-12 1968-10-24 Dowty Rotol Ltd Kombinierte Enteisungs- und Druckfluessigkeitskuehl-Einrichtung fuer einen Schaufelrotor
FR2168938B1 (pt) * 1972-01-27 1974-12-13 Snecma
US4482114A (en) * 1981-01-26 1984-11-13 The Boeing Company Integrated thermal anti-icing and environmental control system
US4615499A (en) * 1983-08-12 1986-10-07 The Boeing Company Wing slat anti-ice air duct system
AU581684B2 (en) * 1984-10-08 1989-03-02 Short Brothers Plc Duct for hot air
IL78786A0 (en) * 1985-06-03 1986-08-31 Short Brothers Plc Duct for hot air
US5011098A (en) * 1988-12-30 1991-04-30 The Boeing Company Thermal anti-icing system for aircraft
US5257498A (en) * 1992-04-23 1993-11-02 United Technologies Corporation Efficient anti-ice exhaust vent

Also Published As

Publication number Publication date
JPH06502825A (ja) 1994-03-31
DE69207889D1 (de) 1996-03-07
AU2592792A (en) 1993-04-27
EP0558726A1 (en) 1993-09-08
WO1993006005A1 (en) 1993-04-01
GB9120113D0 (en) 1992-09-23
US5400984A (en) 1995-03-28
EP0558726B1 (en) 1996-01-24
GB2259679A (en) 1993-03-24
GB2259679B (en) 1994-10-05
CA2095530A1 (en) 1993-03-21
IL103208A (en) 1995-11-27
AU655077B2 (en) 1994-12-01
GB9219706D0 (en) 1992-10-28

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Legal Events

Date Code Title Description
FF Decision: intention to grant
KE Notification for payement of fee for the delivery of letter patents of an application granted by virtue of law 5772/71
FA11 Dismissal: dismissal - article 38, par. 2 of industrial property law