JP2009292466A - 低温液体または貯蔵可能な液状の燃料を貯蔵するためのタンク - Google Patents
低温液体または貯蔵可能な液状の燃料を貯蔵するためのタンク Download PDFInfo
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- 239000012530 fluid Substances 0.000 title abstract 3
- 238000000605 extraction Methods 0.000 claims abstract description 35
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- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 6
- 239000001301 oxygen Substances 0.000 claims description 6
- 229910052760 oxygen Inorganic materials 0.000 claims description 6
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- 229910052739 hydrogen Inorganic materials 0.000 claims description 2
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 claims 2
- WFPZPJSADLPSON-UHFFFAOYSA-N dinitrogen tetraoxide Chemical compound [O-][N+](=O)[N+]([O-])=O WFPZPJSADLPSON-UHFFFAOYSA-N 0.000 claims 2
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/08—Mounting arrangements for vessels
- F17C13/088—Mounting arrangements for vessels for use under microgravity conditions
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
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- 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
- B64G1/4021—Tank construction; Details thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17C2205/00—Vessel construction, in particular mounting arrangements, attachments or identifications means
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- F17C2205/0388—Arrangement of valves, regulators, filters
- F17C2205/0394—Arrangement of valves, regulators, filters in direct contact with the pressure vessel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
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- F17C2221/08—Ergols, e.g. hydrazine
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- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
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- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/01—Propulsion of the fluid
- F17C2227/0192—Propulsion of the fluid by using a working fluid
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- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2227/00—Transfer of fluids, i.e. method or means for transferring the fluid; Heat exchange with the fluid
- F17C2227/03—Heat exchange with the fluid
- F17C2227/0367—Localisation of heat exchange
- F17C2227/0369—Localisation of heat exchange in or on a vessel
- F17C2227/0376—Localisation of heat exchange in or on a vessel in wall contact
- F17C2227/0379—Localisation of heat exchange in or on a vessel in wall contact inside the vessel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
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- F17C2260/01—Improving mechanical properties or manufacturing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/01—Improving mechanical properties or manufacturing
- F17C2260/012—Reducing weight
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F17C2260/00—Purposes of gas storage and gas handling
- F17C2260/02—Improving properties related to fluid or fluid transfer
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
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- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
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- Y02E60/32—Hydrogen storage
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- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
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- Aviation & Aerospace Engineering (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
【解決手段】ほぼ筒状のケーシング(25)を備えたガス供給・取り出し装置(2)は、タンクの上部領域のタンクシェル(1)に直接配置され、且つタンクシェル(1)と直接結合されている。ケーシング(25)は、該ケーシング(25)の上部領域の周側に配置されラッパ状に拡大している開口部(3)の列と、ケーシング(25)の下部領域に配置されてラッパ状に拡大している少なくとも1つの他の開口部(9)とを備えている。さらにケーシング(25)は少なくとも1つの排出部に通じている取り出し管(29)を有している。
【選択図】図5
Description
・燃料を加熱することにより、燃料タンクから排出される液体を蒸発させる。この方法は、液体を蒸発させるために高いエネルギー量を必要とする。
・補助的に加速させることにより、減圧の時点で燃料がガス排出口にないようにする。これは、補助的な駆動システムを用いて加速に指向性を持たせねばならず、一般的には比較的高コストである。また、減圧の前にミッションプロファイルを適合させる必要がある。
・高加速度を伴う段階(図2):この段階には、図面に図示していないメインエンジンが点火して、加速度が矢印8の方向に発生するミッション段階が含まれている。この場合、液体は、図2のaに図示したように、タンクの下部領域にある。これに対し、図2のbに図示したようにタンクが回転すると、液体はタンクの外縁領域に堆積し、ガス供給・取り出し装置2に対し接続していない。
・当初は、すなわち地上でのミッション開始時には、タンクは液体7で十分に充填されており、よってガス供給・取り出し装置2も液体7で十分に充填されている。最初の主点火の間にリザーバーは空になる。燃料取り出し段階により、ガスが装置によってタンク内に導入されることによって液体の代わりにガスが充填される。リザーバーのサイズは、最初の点火が終了したら下部開口部9が液体と接続しないように選定されている。このときシステム内には液体がほとんどない。
・たとえば衛星を放出する間の、低下速度を伴う弾道飛行段階(図3):このとき液体はタンク内でカオス的運動状態にあり、散発的にラッパ状の開口部3と9を湿らす。
2 ガス供給・取り出し装置
3 開口部
9 開口部
12 ダブルフィルタスリーブ(ダブルフィルタ)
14 穴付き板
24 毛細板
25 ケーシング
29 毛細板(取り出し管)
30 カバー(バッフルプレート)
31 穴
32 カバー(バッフルプレート)
Claims (4)
- 宇宙航行機を作動させるための低温液体または貯蔵可能な液状の燃料を貯蔵するためのタンクであって、搬送媒体として用いる駆動ガスと、タンクシェルを有する再充填可能なリザーバーの形態のガス供給・取り出し装置とを備え、表面張力を利用してフィルタリングすることにより駆動ガスを液体から分離させるようにした前記タンクにおいて、
ほぼ筒状のケーシング(25)を備えたガス供給・取り出し装置(2)が、タンクの上部領域のタンクシェル(1)に直接配置され、且つタンクシェル(1)と直接結合され、ケーシング(25)が、該ケーシング(25)の上部領域の周側に配置されラッパ状に拡大している、バッフルプレート(30)により覆われる開口部(3)の列と、ケーシング(25)の下部領域に配置されてラッパ状に拡大している、バッフルプレート(32)により覆われる少なくとも1つの他の開口部(9)とを備え、且つケーシング(25)が少なくとも1つの排出部に通じている取り出し管(29)を有し、前記開口部(3,9)のそれぞれが、直列に交互に配置されて該開口部(3,9)内へ突出している板(14)を備え、且つダブルフィルタ(12)を介してケーシング(25)の内部と連通し、ケーシング(25)の内壁に、ケーシング(25)の長手軸線に平行に延在する板(24)が配置され、下部のラッパ状の開口部(9)を覆うために設けられる皿状の水平方向のバッフルプレート(32)が1個または複数個の穴(31)を有していることを特徴とするタンク。 - 液体水素または液体酸素のような低温液体を収容するために形成されていることを特徴とする、請求項1に記載のタンク。
- モノメチルヒドラジン(MMH)またはヒドラジン(N2H4)のような貯蔵可能な燃料を収容するために形成されていることを特徴とする、請求項1または2に記載のタンク。
- 四酸化二窒素(N2O4)のような酸素担体を収容するために形成されていることを特徴とする、請求項1または2に記載のタンク。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008026320A DE102008026320B3 (de) | 2008-06-03 | 2008-06-03 | Tank zur Lagerung kryogener Flüssigkeiten und lagerfähiger Treibstoffe |
DE102008026320.6 | 2008-06-03 |
Publications (2)
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US (1) | US8025721B2 (ja) |
EP (1) | EP2130768B1 (ja) |
JP (1) | JP5463078B2 (ja) |
CN (1) | CN101596939B (ja) |
AT (1) | ATE466769T1 (ja) |
DE (2) | DE102008026320B3 (ja) |
ES (1) | ES2342861T3 (ja) |
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DE102007005539B3 (de) * | 2007-02-03 | 2008-08-14 | Astrium Gmbh | Tank zur Lagerung kryogener Flüssigkeiten oder lagerfähiger flüssiger Treibstoffe |
US8114202B2 (en) * | 2009-03-09 | 2012-02-14 | Crane Environmental, Inc. | Deaerator spray nozzle and related methods |
CN103057729A (zh) * | 2012-12-26 | 2013-04-24 | 北京空间飞行器总体设计部 | 一种航天器推进系统氦气瓶的固定装置 |
DE102014011101A1 (de) | 2014-07-24 | 2016-01-28 | Astrium Gmbh | Einspritzelement für eine Raketenbrennkammer |
JP6590502B2 (ja) * | 2015-03-31 | 2019-10-16 | 三菱重工業株式会社 | 宇宙航行体用の推進薬タンク及び宇宙航行体 |
EP3296216B1 (en) | 2016-09-14 | 2020-06-24 | ArianeGroup GmbH | Obviating liquid instrusion into a gas supply line |
CN106564624A (zh) * | 2016-10-20 | 2017-04-19 | 上海空间推进研究所 | 轻质高性能推进剂管理装置 |
CN109455428A (zh) * | 2018-12-18 | 2019-03-12 | 江苏建友工程机械有限公司 | 一种用于液氧的二次减压排出型存储装置 |
EP4150243A1 (en) | 2020-05-12 | 2023-03-22 | Universal Hydrogen Co. | Fuel storage module assembly |
US11420757B2 (en) | 2020-08-21 | 2022-08-23 | Universal Hydrogen Co. | Systems and methods for multi-module control of a hydrogen powered hybrid electric powertrain |
CA3199672A1 (en) | 2020-10-30 | 2022-05-05 | Universal Hydrogen Co. | Systems and methods for storing liquid hydrogen |
CN112459925B (zh) * | 2020-11-02 | 2022-03-04 | 中国运载火箭技术研究院 | 一种内置隔板式贮箱 |
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- 2009-05-08 DE DE502009000017T patent/DE502009000017D1/de active Active
- 2009-05-08 AT AT09006252T patent/ATE466769T1/de active
- 2009-05-08 ES ES09006252T patent/ES2342861T3/es active Active
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- 2009-06-02 JP JP2009133034A patent/JP5463078B2/ja not_active Expired - Fee Related
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Also Published As
Publication number | Publication date |
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EP2130768B1 (de) | 2010-05-05 |
CN101596939A (zh) | 2009-12-09 |
US20090293729A1 (en) | 2009-12-03 |
JP5463078B2 (ja) | 2014-04-09 |
EP2130768A1 (de) | 2009-12-09 |
US8025721B2 (en) | 2011-09-27 |
ATE466769T1 (de) | 2010-05-15 |
ES2342861T3 (es) | 2010-07-15 |
DE102008026320B3 (de) | 2009-12-03 |
DE502009000017D1 (de) | 2010-06-17 |
CN101596939B (zh) | 2012-02-22 |
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