CN100507293C - 动力燃料贮箱 - Google Patents

动力燃料贮箱 Download PDF

Info

Publication number
CN100507293C
CN100507293C CNB2006100926551A CN200610092655A CN100507293C CN 100507293 C CN100507293 C CN 100507293C CN B2006100926551 A CNB2006100926551 A CN B2006100926551A CN 200610092655 A CN200610092655 A CN 200610092655A CN 100507293 C CN100507293 C CN 100507293C
Authority
CN
China
Prior art keywords
tank
power fuel
outlet
collecting container
fuel tank
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
CNB2006100926551A
Other languages
English (en)
Other versions
CN1903660A (zh
Inventor
凯·菲利普·贝赫鲁齐
马克·米夏埃利斯
加斯东·内特
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.)
EADS Space Transportation GmbH
Original Assignee
EADS Space Transportation GmbH
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 EADS Space Transportation GmbH filed Critical EADS Space Transportation GmbH
Publication of CN1903660A publication Critical patent/CN1903660A/zh
Application granted granted Critical
Publication of CN100507293C publication Critical patent/CN100507293C/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • 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
    • F17C13/00—Details of vessels or of the filling or discharging of vessels
    • F17C13/008—Details of vessels or of the filling or discharging of vessels for use under microgravity conditions
    • 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
    • F17C3/00—Vessels not under pressure
    • F17C3/12—Vessels not under pressure with provision for protection against corrosion, e.g. due to gaseous acid
    • 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
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01—Shape
    • F17C2201/0128—Shape spherical or elliptical
    • 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
    • F17C2201/00—Vessel construction, in particular geometry, arrangement or size
    • F17C2201/05—Size
    • F17C2201/056—Small (<1 m3)
    • 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
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/01—Pure fluids
    • F17C2221/014—Nitrogen
    • 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
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/01—Pure fluids
    • F17C2221/016—Noble gases (Ar, Kr, Xe)
    • F17C2221/017—Helium
    • 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
    • F17C2221/00—Handled fluid, in particular type of fluid
    • F17C2221/08—Ergols, e.g. hydrazine
    • 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
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107—Single phase
    • F17C2223/0123—Single phase gaseous, e.g. CNG, GNC
    • 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
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0107—Single phase
    • F17C2223/013—Single phase liquid
    • 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
    • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
    • F17C2223/035—High pressure (>10 bar)
    • 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
    • F17C2227/01—Propulsion of the fluid
    • F17C2227/0192—Propulsion of the fluid by using a working fluid
    • 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
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/01—Improving mechanical properties or manufacturing
    • F17C2260/011—Improving strength
    • 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
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/02—Improving properties related to fluid or fluid transfer
    • F17C2260/027—Making transfer independent of vessel orientation
    • 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
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/05—Improving chemical properties
    • F17C2260/053—Reducing corrosion
    • 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
    • F17C2260/00—Purposes of gas storage and gas handling
    • F17C2260/05—Improving chemical properties
    • F17C2260/056—Improving fluid characteristics
    • 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
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0186—Applications for fluid transport or storage in the air or in space
    • F17C2270/0194—Applications for fluid transport or storage in the air or in space for use under microgravity conditions, e.g. space
    • 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
    • F17C2270/00—Applications
    • F17C2270/01—Applications for fluid transport or storage
    • F17C2270/0186—Applications for fluid transport or storage in the air or in space
    • F17C2270/0197—Rockets
    • 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
    • Y10T137/2931—Diverse fluid containing pressure systems
    • 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
    • Y10T137/8593—Systems
    • Y10T137/86348—Tank with internally extending flow guide, pipe or conduit

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

本发明涉及一种表面张力贮箱，它用于贮存在空间飞行器中可贮存的动力燃料，如MMH、N2O4及胼，并且它用一种作为输送介质使用的驱动气体工作，在一个借助毛细的提升辅助作用的动力燃料取出装置及一个位于贮箱出口上的收集容器中进行动力燃料与驱动气体的分离。在此这样构造贮箱出口，使得在贮箱水平定向及贮箱填充度低的情况下液体可稳定地保持在动力燃料管道中，其方式是，贮箱出口设置有孔，这些孔使排出管与收集容器相连接。此外，相对于一个与贮箱的对称轴线垂直的平面成锐角地设置该收集容器的内腔。在贮箱的底部由水平到垂直重新取向期间及在宇宙中失重的条件下，该贮箱的构型保证收集容器始终被无气泡地再填充。

Description

动力燃料贮箱
技术领域
本发明涉及一种动力燃料贮箱、尤其是用于贮存用于空间飞行器的运行的侵蚀性液体的贮箱，该动力燃料贮箱具有一种作为输送介质使用的驱动气体及至少一个动力燃料取出装置，所述动力燃料取出装置由至少各一个收集容器和一个贮箱出口组成，在该动力燃料取出装置中在利用表面张力的情况下引起动力燃料与驱动气体的分离，其中，所述取出装置以可再填充的储存器的形式被设置在该动力燃料贮箱的底部上并且通过输送管道与该动力燃料贮箱的内部相连接。
背景技术
在空间飞行器如人造卫星或轨道站中，无论对于在宇宙中用于姿态调节的驱动机构还是对于用来执行远地点动作的驱动机构，通常使用液态的动力燃料，所述动力燃料在合适的容器中被携带并且通常在使用驱动气体的情况下从所述容器输送到相应驱动机构的燃烧室或反应室中。作为驱动气体通常使用惰性气体如氦(He)或氮(N2)，所述惰性气体在压力下被压到动力燃料容器中并且由此将动力燃料压到通到对应驱动机构的管道系统中。在此重要的是，作为输送介质使用的输送气体与到达驱动机构中的动力燃料之间完全且可靠地分离，因为动力燃料在点火时必须绝对地不夹带杂质气体。由DE 100 40755 C2已公开一种开始所述类型的、基于这种原理的贮箱。
此外由US 5 293 895公开了一种动力燃料贮箱，其中在出口处排出管借助多个孔与一个收集容器相连接。
一种使液体与气体相互分离的标准措施是使用一些滤筛，这些滤筛阻断气体的通过，直至达到一个确定的压力差。但在具有小的动力燃料输送流的较小人造卫星中，在一定情况下可不使用这种相对昂贵的滤筛。此外，对这种贮箱的一个特殊且常见的要求是：已被填充的动力燃料贮箱能够被组合在人造卫星中水平运输到发射场地，尤其当在贮箱填充度方面不期望任何限制时。在运输期间出现的力由于动力学效应可超过由地球引力产生的力的多倍。因此在这种类型的迄今公知的贮箱中，或者向着较小填充度的方向来限制贮箱填充度，使得贮箱出口始终被液体包围，或者贮箱出口通过很窄的通道来限制，但该通道在取出动力燃料时产生相对高的压力损失。通常预先规定在此情况下最大允许的压力损失。
对这种贮箱的另一个要求是这样的可能性：包含这种贮箱的人造卫星应以垂直于贮箱出口的取向被运送到轨道中。尤其在运送在侧面水平安装在一个中央的承载结构上的多个小人造卫星的情况下产生这种可能性。在火箭发射时出现的高的动负载产生这样的后果：露出的滤筛及开口通常不再具有保持能力，即不能抑制驱动气体进入到出口中。当动力燃料贮箱未被完全填充及敏感部件如滤筛及开口从液体伸出时，这导致失灵。驱动气体则可在负荷高时通过滤筛及开口到达贮箱出口，这也可导致驱动机构的失灵。因此，以贮箱的水平取向发射火箭时不可采用开始所述类型的迄今公知的贮箱。
发明内容
本发明的任务在于，这样构造一种动力燃料贮箱、尤其是用于贮存用于空间飞行器的运行的侵蚀性液体的贮箱，使得即使在经过暂时的水平定向后以及在贮箱填充度低的情况下动力燃料也稳定地保持在动力燃料管道中，并且由此始终保证位于贮箱中的收集容器被无气泡地填充或重新填充。
本发明这样来解决该任务：提出了一种动力燃料贮箱，用于贮存用于空间飞行器的运行的侵蚀性液体，该动力燃料贮箱具有一种作为输送介质使用的驱动气体及至少一个动力燃料取出装置，所述动力燃料取出装置由至少各一个收集容器和一个贮箱出口组成，在所述动力燃料取出装置中在利用表面张力的情况下引起动力燃料与驱动气体的分离，其中，所述取出装置以可再填充的储存器的形式被设置在该动力燃料贮箱的底部上并且通过输送管道与该动力燃料贮箱的内部相连接，其特征在于：贮箱出口设置有孔，这些孔使排出管与收集容器相连接，并且，位于这些孔对面的区域设置有一些槽。
根据本发明的贮箱的制造成本在此比传统的贮箱实际上没有提高，由此在成本保持相同的情况下可获得在底部上的处理方面及在火箭发射期间的灵活性的显著提高。这里根据本发明的动力燃料贮箱同时被证实：该动力燃料贮箱无需滤筛即可实现可靠的且无气泡的输送。
为了改善在毛细的泵作用下的填充而提出：相对于一个与贮箱的对称轴线垂直的平面成锐角地构造收集容器的内腔。
附图说明
下面借助于附图中所示的实施例来详细描述根据本发明的动力燃料贮箱。附图表示：
图1一个动力燃料贮箱的立体图，
图2根据图1的动力燃料贮箱在贮箱出口的区域中的一个细节图，
图3沿图2中的剖线的一个截面图，及
图4在纵轴线的区域中剖切根据图1的动力燃料贮箱的一个垂直截面图，该动力燃料贮箱在该情况中被设置用于在水平位置中发射。
具体实施方式
图1中所示的动力燃料贮箱是一种表面张力贮箱，用于容纳及贮存侵蚀性的、可贮存的动力燃料，如MMH、N2O4及肼，该表面张力贮箱具有一个设置在贮箱底部上的动力燃料取出装置，在该动力燃料取出装置中在利用表面张力的情况下引起动力燃料与驱动气体分离。在该贮箱中，四个导向板1沿着贮箱壁2被导向并且通到动力燃料贮箱的底部上的收集容器3中。动力燃料可被驱动气体从容器3经过排出管4排出到图中未示出的燃烧室或反应室中。作为驱动气体在此通常使用惰性气体氦(He)或氮(N2)，惰性气体将动力燃料压到图中未示出的、通到相应驱动机构的管道系统中。
如图2及图3中所示，贮箱出口4上的收集容器3的下部分9被构造成车削件，由此尤其可使制造成本保持很低。从一个设置在中央的排出管10起，三个各具有约2mm直径的通道11在一侧使所述收集容器的内部12与排出管10相连接。在此情况下即使当连接通道11逆着重力加速度向上指向时，也可实现在水平状态中填充。贮箱出口中的连接或打开通道11在此被这样倾斜地设置，使得在用动力燃料首次填充贮箱期间没有驱动气体气泡被封入。
收集容器的内腔12在其几何结构上相对于一个与贮箱的对称轴线或纵向轴线13垂直的平面成一个锐角15地这样构造，使得该内腔无论当贮箱从水平位置转动到垂直位置中——例如在以小的贮箱填充度水平运输后，还是在失重状态中，都由于毛细作用而重新自动地、完全地且无气泡地填充。该快速的填充附加地通过在一侧开出的槽14来支持，由此，该内腔在失重下由于起作用的毛细力而非常快速地填充。由于该收集容器内腔12构造有锐角15，在毛细的泵作用下显著地改善了填充过程。
用动力燃料填充贮箱通常在贮箱垂直取向的情况下进行，即贮箱的纵向轴线13在此情况下平行于地球引力的方向延伸，其中整个贮箱出口4及收集容器3完全被动力燃料填充。如果动力燃料贮箱接着这样绕贮箱横向轴线倾翻，使得所述三个开口11逆着起作用的加速度取向，则即使在贮箱填充度小的情况下也可水平地运输该贮箱。在图4所示的布置中，根据图1的被填充的动力燃料贮箱为了接着例如被组合在一个人造卫星中地运输到发射场地被水平地安置。被填充的贮箱的贮箱出口4在此情况下与在该图中用箭头表示的重力加速度g的方向垂直地取向，由此，动力燃料5尤其在填充度小的情况下不再浸润出口4，而是它的液面以一个距离h位于这个出口4的下方。
在出口中使用多个通道11附加地导致了：与迄今公知的这种类型的贮箱相比在动力燃料排出期间贮箱出口4上压力损失显著地减小。出口的改型除了允许就水平运输及水平发射而言扩大了应用领域外，还允许在可容许的最大压力损失方面具有较大的裕量并且贮箱在底部更快速填充和排空。

Claims (2)

1.动力燃料贮箱，用于贮存用于空间飞行器的运行的侵蚀性液体，该动力燃料贮箱具有一种作为输送介质使用的驱动气体及至少一个动力燃料取出装置，所述动力燃料取出装置由至少各一个收集容器和一个贮箱出口组成，在所述动力燃料取出装置中在利用表面张力的情况下引起动力燃料与驱动气体的分离，其中，所述取出装置以可再填充的储存器的形式被设置在该动力燃料贮箱的底部上并且通过输送管道与该动力燃料贮箱的内部相连接，其特征在于：所述贮箱出口设置有孔(11)，这些孔使排出管(10)与该收集容器(3)相连接，并且，位于这些孔(11)对面的区域设置有一些槽(14)。
2.根据权利要求1的动力燃料贮箱，其特征在于：相对于一个与该贮箱的对称轴线(13)垂直的平面成锐角(15)地构造该收集容器的内腔(12)。
CNB2006100926551A 2005-07-28 2006-06-13 动力燃料贮箱 Expired - Fee Related CN100507293C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE200510035356 DE102005035356B3 (de) 2005-07-28 2005-07-28 Treibstofftank
DE102005035356.8 2005-07-28

Publications (2)

Publication Number Publication Date
CN1903660A CN1903660A (zh) 2007-01-31
CN100507293C true CN100507293C (zh) 2009-07-01

Family

ID=36587363

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2006100926551A Expired - Fee Related CN100507293C (zh) 2005-07-28 2006-06-13 动力燃料贮箱

Country Status (6)

Country Link
US (1) US7395832B2 (zh)
EP (1) EP1748248B1 (zh)
JP (1) JP4585994B2 (zh)
CN (1) CN100507293C (zh)
BR (1) BRPI0601953B1 (zh)
DE (1) DE102005035356B3 (zh)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005044534B3 (de) * 2005-09-17 2007-06-06 Astrium Gmbh Treibstofftank für kryogene Flüssigkeiten
DE102005062092B3 (de) * 2005-12-22 2007-03-29 Eads Space Transportation Gmbh Treibstofftank
DE102007005539B3 (de) * 2007-02-03 2008-08-14 Astrium Gmbh Tank zur Lagerung kryogener Flüssigkeiten oder lagerfähiger flüssiger Treibstoffe
US7559509B1 (en) * 2007-02-12 2009-07-14 Thomas C. Taylor Large cryogenic tank logistics for in-space vehicles
US8899974B2 (en) * 2007-09-19 2014-12-02 The Aerospace Corporation Particulate mitigating propellant management tank device
DE102008026320B3 (de) * 2008-06-03 2009-12-03 Astrium Gmbh Tank zur Lagerung kryogener Flüssigkeiten und lagerfähiger Treibstoffe
DE102009019002B3 (de) * 2009-04-16 2010-11-25 Astrium Gmbh Blasenfalle für Treibstofftanks in Raumflugkörpern
US8245889B1 (en) 2009-11-03 2012-08-21 Jon Starns Portable pumpless fuel delivery system
US8534489B2 (en) 2011-03-21 2013-09-17 Hamilton Sundstrand Space Systems International, Inc. Demisable fuel supply system
US8511504B2 (en) 2011-03-21 2013-08-20 Hamilton Sundstrand Corporation Demisable fuel supply system
US10479532B2 (en) * 2015-05-07 2019-11-19 Keystone Engineering Company Stress relieved welds in positive expulsion fuel tanks with rolling metal diaphragms
US11092111B1 (en) 2018-12-10 2021-08-17 United Launch Alliance, L.L.C. Vapor retention device

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA683854A (en) 1964-04-07 Clark George Liquid reservoirs for aircraft
US2163988A (en) 1937-10-21 1939-06-27 Stacey Cromwell Safety apparatus for motor vehicles
US2943815A (en) * 1954-11-19 1960-07-05 Sud Aviation Aerodynes, more particularly pilotless aerodynes
US3315845A (en) * 1965-09-27 1967-04-25 Bendix Corp Convoluted spherical barrier for liquid storage tank
US3854905A (en) 1972-04-24 1974-12-17 Rca Corp Storage system for two phase fluids
FR2484961A1 (fr) * 1980-06-20 1981-12-24 Europ Propulsion Reservoir a tension superficielle
DE3146262A1 (de) 1981-11-21 1983-05-26 Erno-Raumfahrttechnik Gmbh, 2800 Bremen "treibstofftank"
US4595398A (en) * 1984-05-21 1986-06-17 Mcdonnell Douglas Corporation Propellant acquisition device
US4790350A (en) * 1986-02-04 1988-12-13 Arnold Charles M Combat rapid assembly fuel tank
US4733531A (en) 1986-03-14 1988-03-29 Lockheed Missiles & Space Company, Inc. Liquid-propellant management system with capillary pumping vanes
US4743278A (en) 1986-06-16 1988-05-10 Ford Aerospace & Communications Corporation Passive propellant management system
US4768541A (en) * 1986-11-03 1988-09-06 Martin Marietta Corporation Means of expelling parallel tanks to low residuals
DE3837137A1 (de) 1988-11-02 1990-05-03 Erno Raumfahrttechnik Gmbh Treibstofftank zur lagerung aggressiver fluessigkeiten
FR2678895B1 (fr) * 1991-07-08 1993-11-12 Propulsion Ste Europeenne Reservoir a tension superficielle, a debits de sortie multiples.
US5279323A (en) * 1991-12-19 1994-01-18 Lockheed Missiles & Space Company, Inc. Liquid management apparatus for spacecraft
JP3511313B2 (ja) * 1994-06-29 2004-03-29 株式会社アイ・エイチ・アイ・エアロスペース ベーン型表面張力タンク
US6014987A (en) * 1998-05-11 2000-01-18 Lockheed Martin Corporation Anti-vortex baffle assembly with filter for a tank
DE10040755C2 (de) * 2000-08-19 2002-06-27 Astrium Gmbh Treibstofftank
JP2002137799A (ja) * 2000-10-31 2002-05-14 Ishikawajima Harima Heavy Ind Co Ltd 人工衛星用推薬タンク
DE10117557A1 (de) 2001-04-07 2002-10-17 Astrium Gmbh Behälter zur Lagerung kryogener Flüssigkeiten
DE102005062092B3 (de) 2005-12-22 2007-03-29 Eads Space Transportation Gmbh Treibstofftank

Also Published As

Publication number Publication date
EP1748248B1 (de) 2018-07-04
EP1748248A2 (de) 2007-01-31
CN1903660A (zh) 2007-01-31
BRPI0601953A (pt) 2007-03-13
BRPI0601953B1 (pt) 2018-01-23
JP2007030874A (ja) 2007-02-08
EP1748248A3 (de) 2017-04-19
JP4585994B2 (ja) 2010-11-24
US7395832B2 (en) 2008-07-08
DE102005035356B3 (de) 2006-10-19
US20070084509A1 (en) 2007-04-19

Similar Documents

Publication Publication Date Title
CN100507293C (zh) 动力燃料贮箱
JP4783720B2 (ja) 燃料タンク
CN101596939B (zh) 用于储存低温液体和能储存的动力燃料的容器
CN101862551B (zh) 用于空间飞行器中的动力燃料罐的气泡捕捉器
CN101268302B (zh) 用于低温液体的动力燃料容器
CN101294656B (zh) 用于储存低温液体或能储存的动力燃料的容器
US8043396B2 (en) Integrated plastic liner for propellant tanks for micro G conditions
US7118077B1 (en) Platform and system for mass storage and transfer in space
JP2019513608A (ja) 宇宙飛行体のための液体貯蔵タンクおよびシステムおよび推進システムならびに関連する方法
JP2005511425A (ja) 荷積柱を用いる方法および装置
JPH06206598A (ja) 再点火可能ロケットエンジンに燃料供給するための最適化システム
CN109606741B (zh) 航天器表面张力贮箱推进剂在轨补加系统
Asyushkin et al. Outcome of development and initial operational phases of Versatile Space Tugs of the Fregat type.
JP6338517B2 (ja) 可搬式液化天然ガス供給設備
DE10040755A1 (de) Treibstofftank
US20240284836A1 (en) System for sequestering green house gas to space and method for same
US20200039659A1 (en) Container for Receiving, Storing and Dispensing Liquids and/or Viscous Substances, in Particular Fuel, Propellant or Drinking Water, Method for Producing Same and Use Thereof
US9597686B1 (en) Serviceable microgravity fluid-handling system
US9808805B2 (en) Liquid reservoir for microgravity system
Collicott et al. Asymmetric Propellant Positioning in Symmetric Tanks and PMDs
RU2787259C1 (ru) Способ дозаправки жидким топливом космического объекта в космическом пространстве
Debreceni et al. Development of a titanium propellant tank
US11498705B1 (en) On orbit fluid propellant dispensing systems and methods
Debreceni et al. Tank for an advanced communications satellite
KR20140019857A (ko) 액체화물용 운반탱크

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090701

Termination date: 20180613