JP2016513033A - 極低温回路コンディショニングシステム - Google Patents
極低温回路コンディショニングシステム Download PDFInfo
- Publication number
- JP2016513033A JP2016513033A JP2015554127A JP2015554127A JP2016513033A JP 2016513033 A JP2016513033 A JP 2016513033A JP 2015554127 A JP2015554127 A JP 2015554127A JP 2015554127 A JP2015554127 A JP 2015554127A JP 2016513033 A JP2016513033 A JP 2016513033A
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- conditioning
- nitrogen
- circuit
- cryogenic
- 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.)
- Granted
Links
- 230000003750 conditioning effect Effects 0.000 title claims abstract description 47
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 97
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 49
- 239000003380 propellant Substances 0.000 claims description 15
- 238000001035 drying Methods 0.000 claims description 5
- 239000001307 helium Substances 0.000 claims description 5
- 229910052734 helium Inorganic materials 0.000 claims description 5
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 5
- 230000007246 mechanism Effects 0.000 claims description 4
- 238000000034 method Methods 0.000 claims description 3
- 150000002829 nitrogen Chemical class 0.000 abstract 1
- 239000003570 air Substances 0.000 description 17
- 239000007789 gas Substances 0.000 description 15
- 239000007788 liquid Substances 0.000 description 7
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 5
- 239000001301 oxygen Substances 0.000 description 5
- 229910052760 oxygen Inorganic materials 0.000 description 5
- 239000012530 fluid Substances 0.000 description 4
- 239000001257 hydrogen Substances 0.000 description 4
- 229910052739 hydrogen Inorganic materials 0.000 description 4
- 239000012080 ambient air Substances 0.000 description 3
- 238000000926 separation method Methods 0.000 description 3
- 238000010408 sweeping Methods 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 238000009825 accumulation Methods 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000001143 conditioned effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/401—Liquid propellant rocket engines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/402—Propellant tanks; Feeding propellants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
- F02K9/78—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D21/00—Defrosting; Preventing frosting; Removing condensed or defrost water
- F25D21/04—Preventing the formation of frost or condensate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/002—Launch systems
-
- 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
- F05D2260/608—Aeration, ventilation, dehumidification or moisture removal of closed spaces
Landscapes
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Thermal Sciences (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Separation By Low-Temperature Treatments (AREA)
- Separation Using Semi-Permeable Membranes (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims (12)
- 航空機の極低温回路内の機器(6、7、8)の飛行中コンディショニングを行うためのデバイスであって、前記航空機の外部から空気を取り込むための手段と、OBIGGSタイプの窒素分離器(3)を使用して前記空気から窒素を抽出するための手段と、前記機器の周りに前記窒素を分配するための手段(4、5)とを備えることを特徴とするデバイス。
- 前記分配手段は、昇圧手段を備える請求項1に記載のコンディショニングデバイス。
- 較正オフィリス(5)を備える管路回路(4)を使用して極低温回路内の様々な機器アイテムの周りに前記窒素を分配するための手段を備える請求項1または2に記載のコンディショニングデバイス。
- 前記コンディショニング窒素を受け取るために前記機器(6、7、8)をカプセル化するための手段(13)を備える請求項1、2、または3に記載のコンディショニングデバイス。
- 少なくとも前記航空機の大気飛行の段階中に前記極低温回路内の機器アイテムの周りにコンディショニング窒素を分配するのに適した請求項1〜4のいずれか一項に記載のコンディショニングデバイス。
- 前記取込み手段は、前記航空機に装備されたタービンエンジン(1)の圧縮器段(2)に位置される請求項1〜5のいずれか一項に記載のコンディショニングデバイス。
- 前記取込み手段は、前記航空機の外部から空気を直接引き込む請求項1〜5のいずれか一項に記載のコンディショニングデバイス。
- 前記回路内で前記分離器の下流に乾燥手段(9)を備える請求項1〜7のいずれか一項に記載のコンディショニングデバイス。
- 前記航空機の外部にあって、窒素またはヘリウムを循環させるための地上デバイスを補完的に備えることを特徴とする請求項1〜8のいずれか一項に記載のコンディショニングデバイス。
- 1つまたは複数の極低温推進剤を使用するロケットエンジン(100)を備える航空機であって、請求項1〜9のいずれか一項に記載のコンディショニングデバイスを備えることを特徴とする航空機。
- スペースプレーンタイプであり、エアロビックタービンエンジン(1)とロケットエンジン(100)との2段式推進機構を有することを特徴とする請求項10に記載の航空機。
- 航空機の極低温回路内の機器のコンディショニングを行うための方法であって、前記航空機に接続された外部コンディショニング回路を使用して、地上で前記航空機の極低温回路内の機器のコンディショニングを行う第1のステップと、請求項1〜9のいずれか一項に記載のデバイスを使用して、前記機器の飛行中コンディショニングを行う第2のステップとを含むことを特徴とする方法。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1350561 | 2013-01-22 | ||
FR1350561A FR3001261B1 (fr) | 2013-01-22 | 2013-01-22 | Systeme de conditionnement de circuits cryogeniques |
PCT/EP2014/051099 WO2014114628A1 (fr) | 2013-01-22 | 2014-01-21 | Système de conditionnement de circuits cryogéniques |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2016513033A true JP2016513033A (ja) | 2016-05-12 |
JP6290259B2 JP6290259B2 (ja) | 2018-03-07 |
Family
ID=49546471
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015554127A Active JP6290259B2 (ja) | 2013-01-22 | 2014-01-21 | 極低温回路コンディショニングシステム |
Country Status (10)
Country | Link |
---|---|
US (1) | US10480455B2 (ja) |
EP (1) | EP2948665B1 (ja) |
JP (1) | JP6290259B2 (ja) |
CN (1) | CN104937252B (ja) |
BR (1) | BR112015017469A2 (ja) |
ES (1) | ES2816951T3 (ja) |
FR (1) | FR3001261B1 (ja) |
RU (1) | RU2648481C2 (ja) |
SG (1) | SG11201505625QA (ja) |
WO (1) | WO2014114628A1 (ja) |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3093348A (en) * | 1960-10-06 | 1963-06-11 | Garrett Corp | Hypersonic aircraft |
JPS63113169A (ja) * | 1986-10-14 | 1988-05-18 | ゼネラル・エレクトリック・カンパニイ | 推進装置、及び燃焼器ライナ及びノズルのどライナを作る方法 |
US5048597A (en) * | 1989-12-18 | 1991-09-17 | Rockwell International Corporation | Leak-safe hydrogen/air heat exchanger in an ACE system |
US20020088504A1 (en) * | 2001-01-05 | 2002-07-11 | Sauer Richard A. | Aircraft fuel inerting system for an airport |
US20070054610A1 (en) * | 2005-01-21 | 2007-03-08 | Jensen Bryan D | Three flow architecture and method for aircraft OBIGGS |
US20080060523A1 (en) * | 2006-09-12 | 2008-03-13 | Honeywell International Inc. | Enhanced obiggs |
JP2008509842A (ja) * | 2004-08-16 | 2008-04-03 | エアバス・ドイチュラント・ゲーエムベーハー | 航空機への空気供給 |
US20080199376A1 (en) * | 2005-07-08 | 2008-08-21 | Phyre Technologies Inc. | Catalytic Reactive Component Reduction System and Methods for the Use Thereof |
JP2010506789A (ja) * | 2006-10-20 | 2010-03-04 | アストリウム・エス・エー・エス | 航空力学的および宇宙的飛行を行う飛行機およびそれに関係した操縦方法 |
WO2012045035A2 (en) * | 2010-09-30 | 2012-04-05 | General Electric Company | Fuel storage system |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB831231A (en) * | 1957-07-09 | 1960-03-23 | British Oxygen Co Ltd | Storage of liquefied gases |
US5499656A (en) * | 1993-12-23 | 1996-03-19 | Hughes Aircraft Company | Integrated storage and transfer system and method for spacecraft propulsion systems |
US6655168B2 (en) * | 2001-07-05 | 2003-12-02 | Shimadzu Corporation | Aircraft air conditioner |
RU2238422C2 (ru) * | 2002-11-10 | 2004-10-20 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" | Двигательная установка первой ступени ракеты-носителя воздушно-космической системы |
US20070157614A1 (en) * | 2003-01-21 | 2007-07-12 | Goldman Arnold J | Hybrid Generation with Alternative Fuel Sources |
RU2267023C2 (ru) * | 2004-02-11 | 2005-12-27 | Федеральное государственное унитарное предприятие "Конструкторское бюро общего машиностроения им. В.П. Бармина" | Способ заправки гелием бортовых баллонов ракет-носителей и космических аппаратов и система заправки гелием бортовых баллонов ракет-носителей и космических аппаратов |
US20090227195A1 (en) * | 2008-03-07 | 2009-09-10 | Basf Catalysts Llc | Systems and Methods for Treating Aircraft Cabin Air |
US20100187364A1 (en) * | 2009-01-23 | 2010-07-29 | Bernard Friedrich Kutter | Cryogenic propellant depot and integral sunshield |
ES2399332T3 (es) * | 2010-02-01 | 2013-03-27 | Cryospace L'air Liquide Aerospatiale | Artículo de aislamiento criogénico de cerramiento espeicalmente destinado a proteger depósitos criotécnicos |
US9102416B1 (en) * | 2012-03-20 | 2015-08-11 | The Boeing Company | Inert gas generating system |
CA2895740A1 (en) * | 2012-12-28 | 2014-07-03 | General Electric Company | Aircraft and a retrofit cryogenic fuel system |
-
2013
- 2013-01-22 FR FR1350561A patent/FR3001261B1/fr not_active Expired - Fee Related
-
2014
- 2014-01-21 SG SG11201505625QA patent/SG11201505625QA/en unknown
- 2014-01-21 JP JP2015554127A patent/JP6290259B2/ja active Active
- 2014-01-21 EP EP14703284.1A patent/EP2948665B1/fr active Active
- 2014-01-21 CN CN201480005708.4A patent/CN104937252B/zh active Active
- 2014-01-21 ES ES14703284T patent/ES2816951T3/es active Active
- 2014-01-21 WO PCT/EP2014/051099 patent/WO2014114628A1/fr active Application Filing
- 2014-01-21 BR BR112015017469A patent/BR112015017469A2/pt not_active IP Right Cessation
- 2014-01-21 RU RU2015135597A patent/RU2648481C2/ru not_active IP Right Cessation
- 2014-01-21 US US14/762,239 patent/US10480455B2/en active Active
Patent Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
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US3093348A (en) * | 1960-10-06 | 1963-06-11 | Garrett Corp | Hypersonic aircraft |
JPS63113169A (ja) * | 1986-10-14 | 1988-05-18 | ゼネラル・エレクトリック・カンパニイ | 推進装置、及び燃焼器ライナ及びノズルのどライナを作る方法 |
US5048597A (en) * | 1989-12-18 | 1991-09-17 | Rockwell International Corporation | Leak-safe hydrogen/air heat exchanger in an ACE system |
JPH0436596A (ja) * | 1989-12-18 | 1992-02-06 | Rockwell Internatl Corp | 熱交換器ならびに空気収集および濃縮システム |
US20020088504A1 (en) * | 2001-01-05 | 2002-07-11 | Sauer Richard A. | Aircraft fuel inerting system for an airport |
US20080090510A1 (en) * | 2004-08-16 | 2008-04-17 | Airbus Deutschland Gmbh | Air Supply For An Aircraft |
JP2008509842A (ja) * | 2004-08-16 | 2008-04-03 | エアバス・ドイチュラント・ゲーエムベーハー | 航空機への空気供給 |
US20070054610A1 (en) * | 2005-01-21 | 2007-03-08 | Jensen Bryan D | Three flow architecture and method for aircraft OBIGGS |
US20080199376A1 (en) * | 2005-07-08 | 2008-08-21 | Phyre Technologies Inc. | Catalytic Reactive Component Reduction System and Methods for the Use Thereof |
JP2009501680A (ja) * | 2005-07-08 | 2009-01-22 | ファイア テクノロジーズ、インコーポレイテッド | 触媒反応成分低減システムおよびその使用法 |
US20080060523A1 (en) * | 2006-09-12 | 2008-03-13 | Honeywell International Inc. | Enhanced obiggs |
JP2010506789A (ja) * | 2006-10-20 | 2010-03-04 | アストリウム・エス・エー・エス | 航空力学的および宇宙的飛行を行う飛行機およびそれに関係した操縦方法 |
WO2012045035A2 (en) * | 2010-09-30 | 2012-04-05 | General Electric Company | Fuel storage system |
Also Published As
Publication number | Publication date |
---|---|
SG11201505625QA (en) | 2015-09-29 |
ES2816951T3 (es) | 2021-04-06 |
CN104937252A (zh) | 2015-09-23 |
EP2948665B1 (fr) | 2020-06-24 |
BR112015017469A2 (pt) | 2017-07-11 |
WO2014114628A1 (fr) | 2014-07-31 |
US20150345428A1 (en) | 2015-12-03 |
FR3001261B1 (fr) | 2015-02-27 |
US10480455B2 (en) | 2019-11-19 |
CN104937252B (zh) | 2018-11-13 |
RU2648481C2 (ru) | 2018-03-26 |
JP6290259B2 (ja) | 2018-03-07 |
RU2015135597A (ru) | 2017-03-10 |
EP2948665A1 (fr) | 2015-12-02 |
FR3001261A1 (fr) | 2014-07-25 |
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