BR112014000186A2 - válvula para controle da pressão interna em uma cabine de uma aeronave - Google Patents

válvula para controle da pressão interna em uma cabine de uma aeronave

Info

Publication number
BR112014000186A2
BR112014000186A2 BR112014000186A BR112014000186A BR112014000186A2 BR 112014000186 A2 BR112014000186 A2 BR 112014000186A2 BR 112014000186 A BR112014000186 A BR 112014000186A BR 112014000186 A BR112014000186 A BR 112014000186A BR 112014000186 A2 BR112014000186 A2 BR 112014000186A2
Authority
BR
Brazil
Prior art keywords
hinges
internal pressure
aircraft cabin
hinge
locking device
Prior art date
Application number
BR112014000186A
Other languages
English (en)
Other versions
BR112014000186B1 (pt
Inventor
Vranjes Dusan
Steinert Martin
Original Assignee
Nord-Micro Ag & Co Ohg
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 Nord-Micro Ag & Co Ohg filed Critical Nord-Micro Ag & Co Ohg
Publication of BR112014000186A2 publication Critical patent/BR112014000186A2/pt
Publication of BR112014000186B1 publication Critical patent/BR112014000186B1/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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • B64D13/04—Automatic control of pressure
    • 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
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
    • F16K1/16—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members
    • F16K1/18—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps
    • F16K1/22—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps with axis of rotation crossing the valve member, e.g. butterfly valves
    • F16K1/221—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps with axis of rotation crossing the valve member, e.g. butterfly valves specially adapted operating means therefor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K39/00—Devices for relieving the pressure on the sealing faces
    • F16K39/02—Devices for relieving the pressure on the sealing faces for lift valves
    • F16K39/028—Devices for relieving the pressure on the sealing faces for lift valves with pivoted closure members, e.g. butterfly valves

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lift Valve (AREA)
  • Check Valves (AREA)
  • Mechanically-Actuated Valves (AREA)
  • Safety Valves (AREA)

Abstract

resumo patente de invenção: "válvula para controle da pressão interna em uma cabine de uma aeronave". a presente invenção refere-se a uma válvula (10) para controle da pressão interna em uma cabine de uma aeronave, com uma primeira charneira (12) e uma segunda charneira (14), que estão sustentadas em uma carcaça (16), sendo que as charneiras (12, 14) controlam uma corrente de fluido (l) que modifica a pressão entre a vizinhança e a cabine por uma abertura (20) da válvula (10). a primeira charneira (12) está montada com distância de uma borda anterior da carcaça (16) e a segunda charneira (14), em uma borda posterior da carcaça (16). além disso, está previsto um dispositivo de fecho (26), que em uma posição de entrada das charneiras (12, 14) fecha uma abertura de saída (56), que é limitada pelas charneiras (12, 14). o dispositivo de fecho (26) está sustentado em uma das charneiras (12, 14) de modo giratoriamente móvel, e ao dispositivo de fecho (26) está associado um dispositivo de travamento (34). o dispositivo de travamento (34) coopera com o dispositivo de fecho (26) de tal modo que em um movimento giratório das charneiras (12, 14), o dispositivo de fecho (26) fecha a abertura de saída (56).
BR112014000186-3A 2012-03-16 2013-03-05 Válvula para controle da pressão interna em uma cabine de uma aeronave BR112014000186B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102012204217.2A DE102012204217B4 (de) 2012-03-16 2012-03-16 Ventil zur Steuerung des Innendrucks in einer Kabine eines Luftfahrzeugs
DE102012204217.2 2012-03-16
PCT/EP2013/054433 WO2013135534A1 (de) 2012-03-16 2013-03-05 Ventil zur steuerung des innendrucks in einer kabine eines luftfahrzeugs

Publications (2)

Publication Number Publication Date
BR112014000186A2 true BR112014000186A2 (pt) 2017-02-07
BR112014000186B1 BR112014000186B1 (pt) 2021-10-26

Family

ID=47884289

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014000186-3A BR112014000186B1 (pt) 2012-03-16 2013-03-05 Válvula para controle da pressão interna em uma cabine de uma aeronave

Country Status (7)

Country Link
US (1) US9481469B2 (pt)
EP (1) EP2699476B1 (pt)
JP (1) JP5840790B2 (pt)
CN (1) CN103687789B (pt)
BR (1) BR112014000186B1 (pt)
DE (1) DE102012204217B4 (pt)
WO (1) WO2013135534A1 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012204217B4 (de) 2012-03-16 2015-02-12 Nord-Micro Ag & Co. Ohg Ventil zur Steuerung des Innendrucks in einer Kabine eines Luftfahrzeugs
EP2921408B1 (en) * 2014-03-21 2016-10-05 Airbus Operations GmbH Method and system for controlling the pressure in an aircraft cabin
FR3022883B1 (fr) 2014-06-27 2016-07-01 Airbus Operations Sas Avion equipe d'une trappe interieure d'evacuation avec une double commande d'ouverture
FR3022884B1 (fr) * 2014-06-27 2016-07-01 Airbus Operations Sas Avion equipe d'une trappe interieure d'evacuation integrant un systeme de regulation de pression
WO2016133261A1 (ko) * 2015-02-18 2016-08-25 삼성전자주식회사 공기조화기
JP2016153717A (ja) * 2015-02-18 2016-08-25 三星電子株式会社Ｓａｍｓｕｎｇ Ｅｌｅｃｔｒｏｎｉｃｓ Ｃｏ．，Ｌｔｄ． 天井埋込型室内機及びそれを用いた空気調和機
US9783306B2 (en) * 2015-10-13 2017-10-10 Honeywell International Inc. Bi-fold thrust recovery outflow valve with a ram air flap
CN106892082B (zh) * 2015-12-17 2020-12-04 东莞前沿技术研究院 用于浮空器的排气组件以及浮空器

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3426984A (en) * 1967-04-24 1969-02-11 United Aircraft Corp Aircraft pressurization outflow valve
US3544045A (en) * 1969-01-10 1970-12-01 Garrett Corp Thrust recovery outflow control valve
FR2632044B1 (fr) * 1988-05-27 1990-12-14 Abg Semca Vanne a ouverture autonome et aeronef comportant une telle vanne
DE19713125C2 (de) * 1997-03-27 1999-03-25 Nord Micro Elektronik Feinmech Verfahren zur Regulierung des Kabinendrucks in einem Fluggerät und Stufenventil hierfür
US6273136B1 (en) * 1998-03-25 2001-08-14 Nord-Micro Elektronik Feinmechanik Differential valve, specifically a cabin air discharge valve in an aircraft, and method for regulating cabin pressure
DE102008040184A1 (de) * 2008-07-04 2010-01-14 Airbus Deutschland Gmbh Verfahren zum Steuern eines Innendrucks in einem Luftfahrzeug
US8342920B2 (en) 2008-10-20 2013-01-01 Honeywell International Inc. Outflow valve having J-shaped bellmouth and cabin pressure control system employing the same
DE102009010150B4 (de) * 2009-02-23 2013-09-19 Airbus Operations Gmbh System und Verfahren zur Notbelüftung einer Flugzeugkabine
DE102010033827B4 (de) * 2010-08-09 2015-01-08 Nord-Micro Ag & Co. Ohg Ventil zur Steuerung des Innendrucks in einer Kabine eines Luftfahrzeugs
US9096320B2 (en) * 2010-09-09 2015-08-04 Honeywell International Inc. Cabin pressure thrust recovery outflow valve with single door
DE102012204217B4 (de) 2012-03-16 2015-02-12 Nord-Micro Ag & Co. Ohg Ventil zur Steuerung des Innendrucks in einer Kabine eines Luftfahrzeugs

Also Published As

Publication number Publication date
JP2014527941A (ja) 2014-10-23
US20140227956A1 (en) 2014-08-14
BR112014000186B1 (pt) 2021-10-26
EP2699476B1 (de) 2014-11-19
CN103687789B (zh) 2016-02-24
WO2013135534A1 (de) 2013-09-19
JP5840790B2 (ja) 2016-01-06
US9481469B2 (en) 2016-11-01
CN103687789A (zh) 2014-03-26
DE102012204217A1 (de) 2013-09-19
EP2699476A1 (de) 2014-02-26
DE102012204217B4 (de) 2015-02-12

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 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 05/03/2013, OBSERVADAS AS CONDICOES LEGAIS.