JP5925561B2 - 流量装置及び該流量装置を使用する方法及びシステム - Google Patents

流量装置及び該流量装置を使用する方法及びシステム Download PDF

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Publication number
JP5925561B2
JP5925561B2 JP2012084401A JP2012084401A JP5925561B2 JP 5925561 B2 JP5925561 B2 JP 5925561B2 JP 2012084401 A JP2012084401 A JP 2012084401A JP 2012084401 A JP2012084401 A JP 2012084401A JP 5925561 B2 JP5925561 B2 JP 5925561B2
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JP
Japan
Prior art keywords
cantilever
opening
outer periphery
flow device
tabs
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 - Fee Related
Application number
JP2012084401A
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English (en)
Japanese (ja)
Other versions
JP2012229690A5 (enExample
JP2012229690A (ja
Inventor
ダニエール・スコット・ハッメル
ダニエル・ジャン−ルイ・ラボリー
ブラッドリー・ジェームズ・ホルツクロウ
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.)
General Electric Co
Original Assignee
General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2012229690A publication Critical patent/JP2012229690A/ja
Publication of JP2012229690A5 publication Critical patent/JP2012229690A5/ja
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Publication of JP5925561B2 publication Critical patent/JP5925561B2/ja
Expired - Fee Related legal-status Critical Current
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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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/1624—Destructible or deformable element controlled
    • Y10T137/1632—Destructible element

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pipe Accessories (AREA)
  • Safety Valves (AREA)
JP2012084401A 2011-04-06 2012-04-03 流量装置及び該流量装置を使用する方法及びシステム Expired - Fee Related JP5925561B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/080,864 US8387950B2 (en) 2011-04-06 2011-04-06 Flow device and method and system using the flow device
US13/080,864 2011-04-06

Publications (3)

Publication Number Publication Date
JP2012229690A JP2012229690A (ja) 2012-11-22
JP2012229690A5 JP2012229690A5 (enExample) 2015-05-14
JP5925561B2 true JP5925561B2 (ja) 2016-05-25

Family

ID=46022045

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012084401A Expired - Fee Related JP5925561B2 (ja) 2011-04-06 2012-04-03 流量装置及び該流量装置を使用する方法及びシステム

Country Status (4)

Country Link
US (1) US8387950B2 (enExample)
EP (1) EP2508426B1 (enExample)
JP (1) JP5925561B2 (enExample)
CA (1) CA2773964C (enExample)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9879599B2 (en) * 2012-09-27 2018-01-30 United Technologies Corporation Nacelle anti-ice valve utilized as compressor stability bleed valve during starting
FR3007738B1 (fr) 2013-06-28 2015-07-31 Aircelle Sa Dispositif de degivrage et de conditionnement pour aeronef
US9764847B2 (en) * 2013-10-18 2017-09-19 The Boeing Company Anti-icing system for aircraft
WO2015130384A2 (en) * 2013-12-16 2015-09-03 United Technologies Corporation Fan nacelle inlet flow control
US20150216076A1 (en) * 2014-01-30 2015-07-30 International Business Machines Corporation Resilient deformable air valve
US10144520B2 (en) * 2014-04-14 2018-12-04 Rohr, Inc. De-icing system with thermal management
ITUB20151085A1 (it) * 2015-05-28 2016-11-28 Alenia Aermacchi Spa Gondola per motore aeronautico con sistema antighiaccio utilizzante un fluido bifase.
US10487740B2 (en) * 2015-06-17 2019-11-26 Hamilton Sundstrand Corporation Multi-flapper check valve without center supports
CN105539861A (zh) * 2015-12-11 2016-05-04 中国航空工业集团公司西安飞机设计研究所 一种根据气压差进气的活门装置
US10634060B2 (en) * 2016-11-20 2020-04-28 Mra Systems, Llc Engine door with burst seal
BE1025263B1 (fr) * 2017-05-31 2019-01-07 Safran Aero Boosters S.A. Compresseur degivrant de turbomachine et procede de degivrage
DE102018112244A1 (de) * 2018-05-22 2019-11-28 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk
US11220344B2 (en) * 2018-12-17 2022-01-11 Rohr, Inc. Anti-ice double walled duct system
US12416368B2 (en) * 2019-01-28 2025-09-16 Mohammad Mohsen Saadat Blade type check valve
FR3116082B1 (fr) * 2020-11-09 2022-09-30 Safran Aircraft Engines Turboréacteur à double flux pourvu de moyens de communication d’air
US11808290B1 (en) * 2020-12-18 2023-11-07 University Of South Florida Fluid flow conditioning apparatus

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2593315A (en) * 1946-10-31 1952-04-15 Dole Valve Co Flow control device
US3571977A (en) 1969-06-27 1971-03-23 Boeing Co Access and pressure release door latch mechanism
US3698598A (en) * 1971-07-26 1972-10-17 Black Sivalls & Bryson Inc Safety pressure relief device
US4688745A (en) * 1986-01-24 1987-08-25 Rohr Industries, Inc. Swirl anti-ice system
JPS63128391U (enExample) * 1987-02-16 1988-08-22
US5284012A (en) 1991-05-16 1994-02-08 General Electric Company Nacelle cooling and ventilation system
GB2265001A (en) 1992-03-12 1993-09-15 Hunter International A backdraught shutter for a ventilating fan
EP0847510B1 (fr) 1995-09-01 2003-04-16 Climes Conseil, Claude Liardet Valve
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
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
WO2003074947A1 (en) * 2002-03-07 2003-09-12 Fujitsu Limited Backflow preventer and electronic apparatus
US7275560B2 (en) 2004-09-29 2007-10-02 A.J. Manufacturing, Inc. Pressure relief door for air duct work
EP2210157B1 (de) * 2007-11-15 2013-01-02 Belimo Holding AG Durchflussbegrenzer
US7740075B2 (en) 2008-07-09 2010-06-22 Schlumberger Technology Corporation Pressure relief actuated valves

Also Published As

Publication number Publication date
US8387950B2 (en) 2013-03-05
EP2508426B1 (en) 2014-07-02
CA2773964C (en) 2014-12-16
JP2012229690A (ja) 2012-11-22
EP2508426A1 (en) 2012-10-10
CA2773964A1 (en) 2012-10-06
US20120255274A1 (en) 2012-10-11

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