CN105793159B - 用于为推进组件保留排出流体的装置 - Google Patents

用于为推进组件保留排出流体的装置 Download PDF

Info

Publication number
CN105793159B
CN105793159B CN201480065647.0A CN201480065647A CN105793159B CN 105793159 B CN105793159 B CN 105793159B CN 201480065647 A CN201480065647 A CN 201480065647A CN 105793159 B CN105793159 B CN 105793159B
Authority
CN
China
Prior art keywords
fluid
cavity
volume
propulsion assembly
upper wall
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.)
Active
Application number
CN201480065647.0A
Other languages
English (en)
Chinese (zh)
Other versions
CN105793159A (zh
Inventor
亚历山大·利昂
吉勒斯·布龙
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SAS filed Critical SNECMA SAS
Publication of CN105793159A publication Critical patent/CN105793159A/zh
Application granted granted Critical
Publication of CN105793159B publication Critical patent/CN105793159B/zh
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Warehouses Or Storage Devices (AREA)
CN201480065647.0A 2013-12-04 2014-12-02 用于为推进组件保留排出流体的装置 Active CN105793159B (zh)

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
CN105793159A CN105793159A (zh) 2016-07-20
CN105793159B true CN105793159B (zh) 2018-01-12

Family

ID=50137843

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201480065647.0A Active CN105793159B (zh) 2013-12-04 2014-12-02 用于为推进组件保留排出流体的装置

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
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
FR3082560B1 (fr) * 2018-06-14 2020-08-28 Safran Aircraft Engines Systeme embarque et procede pour le drainage d'un moteur d'aeronef
EP3798113B1 (en) 2019-09-30 2023-03-29 Rohr, Inc. Fluid drainage 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
BR112016012226A2 (enExample) 2017-08-08
US10301973B2 (en) 2019-05-28
CA2931310A1 (fr) 2015-06-11
EP3077289A1 (fr) 2016-10-12
WO2015082833A1 (fr) 2015-06-11
CN105793159A (zh) 2016-07-20
FR3014134B1 (fr) 2015-12-11
RU2667109C1 (ru) 2018-09-14
BR112016012226B1 (pt) 2022-07-05
US20170002689A1 (en) 2017-01-05
CA2931310C (fr) 2022-09-27
FR3014134A1 (fr) 2015-06-05

Similar Documents

Publication Publication Date Title
CN105793159B (zh) 用于为推进组件保留排出流体的装置
RU2670711C9 (ru) Патрубок для отвода дренажных жидкостей для силовой установки
US9194294B2 (en) Gas turbine engine oil tank
CN100554661C (zh) 带有冷却剂保养系统的机油-冷却剂-模块
US10532802B2 (en) Propulsion assembly comprising a box for retaining drained fluids
CN101903665B (zh) 具有射流排水阀的涡轮增压器
CN101493029A (zh) 涡轮增压器及气缸盖
WO2017033548A1 (ja) エンジン装置
CN202851107U (zh) 汽车曲轴箱通风防结冰系统
CN107076167A (zh) 具有轴向可移动挡板的阀组
BR112013012889B1 (pt) dispositivo de evacuação de óleo e turbomáquina que compreende um tal dispositivo
CN202597658U (zh) 防进水的汽车变速箱通气塞
CN206054705U (zh) 一种风力发电齿轮箱润滑系统过滤器
CN204851831U (zh) 闭式液压系统和包括该闭式液压系统的机器
CN221879511U (zh) 油烟分离收集装置和汽轮机系统
RU2674851C1 (ru) Усовершенствования в и относящиеся к узлу топливного насоса
CN218151441U (zh) 用于鼓风机的用水夹层油箱
US12221927B2 (en) Flammable fluid reservoir
RU2309364C2 (ru) Оборудование для подводного вождения танка
CN211116211U (zh) 一种排气系统余热回收装置及车辆排气系统
CN107339482B (zh) 一种防漏呼吸阀
CN206972779U (zh) 一种轴承排气装置
CN208734424U (zh) 一种发动机除气冷却系统
CN205401127U (zh) 真空泵
KR101781731B1 (ko) 자세 변화시 오일 누출이 방지되는 환기라인을 구비한 윤활 회로

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant