BR112016012226B1 - Dispositivo para a retenção de fluidos drenados de um conjunto de propulsão e conjunto de propulsão compreendendo tal dispositivo - Google Patents

Dispositivo para a retenção de fluidos drenados de um conjunto de propulsão e conjunto de propulsão compreendendo tal dispositivo Download PDF

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Publication number
BR112016012226B1
BR112016012226B1 BR112016012226-7A BR112016012226A BR112016012226B1 BR 112016012226 B1 BR112016012226 B1 BR 112016012226B1 BR 112016012226 A BR112016012226 A BR 112016012226A BR 112016012226 B1 BR112016012226 B1 BR 112016012226B1
Authority
BR
Brazil
Prior art keywords
cavity
fluids
volume
wall
propulsion assembly
Prior art date
Application number
BR112016012226-7A
Other languages
English (en)
Portuguese (pt)
Other versions
BR112016012226A2 (enExample
Inventor
Alexandre LEON
Gilles Brun
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BR112016012226A2 publication Critical patent/BR112016012226A2/pt
Publication of BR112016012226B1 publication Critical patent/BR112016012226B1/pt

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/32—Collecting of condensation water; Drainage ; Removing solid particles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
    • B64C1/1407—Doors; surrounding frames
    • B64C1/1453—Drain masts
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/75—Shape given by its similarity to a letter, e.g. T-shaped
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/602—Drainage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Warehouses Or Storage Devices (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)
BR112016012226-7A 2013-12-04 2014-12-02 Dispositivo para a retenção de fluidos drenados de um conjunto de propulsão e conjunto de propulsão compreendendo tal dispositivo BR112016012226B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1362079 2013-12-04
FR1362079A FR3014134B1 (fr) 2013-12-04 2013-12-04 Dispositif de retention de fluides draines pour un ensemble propulsif
PCT/FR2014/053136 WO2015082833A1 (fr) 2013-12-04 2014-12-02 Dispositif de retention de fluides draines pour un ensemble propulsif

Publications (2)

Publication Number Publication Date
BR112016012226A2 BR112016012226A2 (enExample) 2017-08-08
BR112016012226B1 true BR112016012226B1 (pt) 2022-07-05

Family

ID=50137843

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016012226-7A BR112016012226B1 (pt) 2013-12-04 2014-12-02 Dispositivo para a retenção de fluidos drenados de um conjunto de propulsão e conjunto de propulsão compreendendo tal dispositivo

Country Status (8)

Country Link
US (1) US10301973B2 (enExample)
EP (1) EP3077289A1 (enExample)
CN (1) CN105793159B (enExample)
BR (1) BR112016012226B1 (enExample)
CA (1) CA2931310C (enExample)
FR (1) FR3014134B1 (enExample)
RU (1) RU2667109C1 (enExample)
WO (1) WO2015082833A1 (enExample)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10808577B2 (en) * 2017-03-28 2020-10-20 The Boeing Company Aerodynamic drainage device
FR3082508B1 (fr) * 2018-06-14 2021-12-03 Safran Aircraft Engines Reservoir embarque de drainage d'un moteur d'aeronef
FR3082560B1 (fr) * 2018-06-14 2020-08-28 Safran Aircraft Engines Systeme embarque et procede pour le drainage d'un moteur d'aeronef
FR3082507B1 (fr) 2018-06-14 2022-01-28 Safran Aircraft Engines Dispositif et procede de vidange et surveillance de fluide draine d'un moteur d'aeronef
US11591935B2 (en) 2019-09-30 2023-02-28 Rohr, Inc. Fluid drain system for an aircraft propulsion system
US11268637B2 (en) 2019-11-05 2022-03-08 Rohr, Inc. Drain mast seal assembly with seal wedge(s)
IT202100003647A1 (it) * 2021-02-17 2022-08-17 Nuovo Pignone Tecnologie Srl Serbatoio di contenimento di allagamento
CN114215645B (zh) * 2021-11-29 2023-04-18 中国航发沈阳发动机研究所 一种航空发动机放油磁塞体结构
US12320269B1 (en) 2024-04-08 2025-06-03 Rohr, Inc. Drain system for propulsion system

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4149372A (en) * 1976-12-16 1979-04-17 United Technologies Corporation Fuel reclaiming system
US4506851A (en) * 1981-09-30 1985-03-26 The Boeing Company Drain apparatus for aircraft
RU1132619C (ru) * 1983-08-16 1994-05-15 Акционерное общество "Авиадвигатель" Топливная дренажная система двухконтурного турбореактивного двигателя
US4715561A (en) * 1986-11-03 1987-12-29 East/West Industries, Inc. Drain assembly for aircraft
US5095617A (en) * 1989-02-28 1992-03-17 United Technologies Corporation Method for forming a drain assembly
US5054282A (en) * 1989-02-28 1991-10-08 United Technologies Corporation Drain assembly
US5104069A (en) * 1990-10-29 1992-04-14 The Boeing Company Apparatus and method for ejecting matter from an aircraft
US5285636A (en) * 1992-10-28 1994-02-15 General Electric Company Diagnostic drain mast for a gas turbine engine
US5980756A (en) * 1996-09-20 1999-11-09 Tracy; Thomas R. Treatment method and system for aircraft toilet waste water
RU2141049C1 (ru) * 1998-02-23 1999-11-10 Открытое акционерное общество "Авиадвигатель" Топливная дренажная система газотурбинного двигателя
US5996938A (en) * 1998-03-13 1999-12-07 Alliedsignal Inc. APU compartment drain system
US6578361B1 (en) * 2001-08-30 2003-06-17 General Electric Co. Methods and apparatus for determining engine cavity leakage
US6571562B2 (en) * 2001-10-08 2003-06-03 Honeywell International Inc. Witness drain valve
FR2864031B1 (fr) * 2003-12-18 2006-03-31 Airbus France Drain notamment pour mat support de reacteur
US7651055B2 (en) * 2005-05-05 2010-01-26 Honeywell International Inc. Non-streaking drainmast
GB2446147B (en) * 2007-01-30 2009-02-18 Rolls Royce Plc Aeroengine drain assembly
GB0704725D0 (en) * 2007-03-12 2007-04-18 Airbus Uk Ltd Water Scavenging System
FR2928207B1 (fr) * 2008-02-29 2010-03-26 Hispano Suiza Sa Installation d'echangeur thermique
ES2614905T3 (es) * 2012-01-26 2017-06-02 Airbus Operations, S.L. Mástil de drenaje del compartimento de la unidad de potencia auxiliar de una aeronave

Also Published As

Publication number Publication date
US10301973B2 (en) 2019-05-28
FR3014134B1 (fr) 2015-12-11
CN105793159A (zh) 2016-07-20
RU2667109C1 (ru) 2018-09-14
CA2931310A1 (fr) 2015-06-11
CA2931310C (fr) 2022-09-27
CN105793159B (zh) 2018-01-12
BR112016012226A2 (enExample) 2017-08-08
FR3014134A1 (fr) 2015-06-05
WO2015082833A1 (fr) 2015-06-11
US20170002689A1 (en) 2017-01-05
EP3077289A1 (fr) 2016-10-12

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
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 02/12/2014, OBSERVADAS AS CONDICOES LEGAIS