CN102137790B - 具有能量介质的分段式飞行器 - Google Patents

具有能量介质的分段式飞行器 Download PDF

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CN102137790B
CN102137790B CN200880130327.3A CN200880130327A CN102137790B CN 102137790 B CN102137790 B CN 102137790B CN 200880130327 A CN200880130327 A CN 200880130327A CN 102137790 B CN102137790 B CN 102137790B
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gas cell
energy medium
aircraft
filled
air
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CN102137790A (zh
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伯纳德·赫尔穆特·克勒普林
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Near Space Technology Group Co Ltd
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
    • B64B1/60—Gas-bags surrounded by separate containers of inert gas
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64B—LIGHTER-THAN AIR AIRCRAFT
    • B64B1/00—Lighter-than-air aircraft
    • B64B1/06—Rigid airships; Semi-rigid airships
    • B64B1/20—Rigid airships; Semi-rigid airships provided with wings or stabilising surfaces

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Tires In General (AREA)
  • Fuel Cell (AREA)

Abstract

本发明涉及具有填充有能量介质的气体单元的分段式飞行器。其特别涉及具有互连的气体单元和/或连续气体单元的飞行器，该气体单元填充有气态能量介质，该气态能量介质具有近似于空气的重量。该气态能量介质将能量提供给偏心地固定在分段处的可控驱动装置。从而由产生的推力和加压的外壳获得足够的动态提力，以使得本发明在装载规定的载荷时以稳定且可控的方式飞行。分段式互连空气单元内设置有分段式互连气体单元。该气体单元填充有能量介质，例如燃料气体（Kraftgas）（丙烷/丁烷混合物），该能量介质将能量提供给驱动装置。该驱动装置固定在头段下面并且驱动偏心设置的一对推进器，从而产生矢量推力。通风设备形成由外壳密封的容体的超压。因此，分段式飞行器具有灵活的形状稳定性，并通过与矢量推力相互作用产生动态升力。

Description

具有能量介质的分段式飞行器
技术领域
本发明涉及一种具有气体单元的分段式飞行器。
背景技术
已知，根据DE10053775A1的飞行器包括在互连外壳分段中的分离的气体单元，该气体单元包含轻于空气的提升介质，例如氦。
发明内容
本发明的目的是操作具有承载气体的飞行器，该承载气体作为燃料气体。
为了解决这个问题，提出了根据本发明的分段式飞行器。
本发明提供具有连续容体的分段式构造，而不是由分离的气体单元和外壳分段形成的分离的容体。形成的容体填充有气态能量介质，该气态能量介质具有近似空气的重量，从而通过该气态能量介质操作该分段式飞行器。通过连接到气体单元的可关闭或可打开的隔板，连续容体能够被充气。
与本领域的现有技术相比，本发明的完全改变的设计以及对飞行器的适合的性能量介质的使用，通过含有具有近似空气的重量的气态能量介质的互连的气体单元和/或连续的气体单元解决了上述问题。在分段中，偏心地装备的可控驱动装置可被提供能量。从而通过驱动装置提供的推力以及充压外壳的支持获得足够的动态升力。因此，带有规定载荷的本发明的飞行器以稳定且可控的方式飞行。
本发明的优点尤其包括需要更少的外壳材料和更少的用于能量供给的容器，这降低了结构质量。因此飞行器相对更小，且飞行器借助动态升力以稳定且可控的方式飞行。
附图说明
现在将参考附图仅以举例的方式描述本发明的具体实施例，其中：
图1是具有能量介质的分段式飞行器的第一实施例的侧向剖视图。
图2是图1所示实施例的俯视图。
具体实施方式
图1示出了填充有能量介质的分段式飞行器的优选实施例的侧向剖视图。
飞行器的外壳28内设置有彼此互联的分段式空气单元1，11-14。分段式空气单元1，11-14内设置有彼此互联的分段式气体单元2，21-24。
气体单元2，21-24由空气单元1，11-14中的构造的收缩部25-27以及与收缩部25-27相对设置的收缩部15-17形成。
例如，气体单元可以填充有作为能量介质并给驱动装置4提供能量的“能量气体”（Kraftgas）（丙烷和丁烷的混合物）。驱动装置4设置于飞行器的头段10下面，其驱动偏心放置的推力产生器，例如一对推进器。从而产生如箭头P1，P2所示的或其它方向的矢量推力。
通风设备5形成由外壳28密封的容体的超压。因此，飞行器具有灵活的形状稳定性，并且与矢量推力P1和P2相互作用以产生动态提力。此外，提供了用于着陆的着陆装置3。
图2示出了如本发明提出的具有能量介质的分段式飞行器的优选实施例的顶视图，在飞行器的头段10下面具有固定翼7和三角翼8。所述固定翼和三角翼增加了动态升力。固定翼7和三角翼8可选地是可分离的。本领域技术人员可选择性地在飞行器的后部9放置动板6以获得提高的飞行器的稳定性。

Claims (7)

1.一种分段式飞行器，包括气体单元，其中，设置在单独分段的内部的所述气体单元是互连的且/或形成连续的容体，所述气体单元包含气态能量介质并且设置在空气单元内，所述空气单元设置在飞行器的外壳内；其中进一步地，所述气体单元由构造的收缩部形成为分段式气体单元，所述空气单元具有相对于所述气体单元的收缩部而设置的收缩部。
2.根据权利要求1所述的飞行器，其中，所述气体单元(2，21-24)通过可关闭且可打开的隔板可彼此分离。
3.根据权利要求1或2所述的飞行器，其中，由所述气体单元(2，21-24)形成的所述容体填充有气态能量介质，所述气态能量介质具有空气的重量。
4.根据权利要求1或2所述的飞行器，其中，由所述气体单元(2，21-24)形成的所述容体填充有空气。
5.根据权利要求1或2所述的飞行器，其中，由所述气体单元(2，21-24)形成的所述容体部分地填充有能量介质且/或部分地填充有比空气轻的提升气体且/或部分地填充有空气。
6.根据权利要求1所述的飞行器，其中，所述飞行器可适应地通过外部充压外壳(28)和/或单独或成对地设置在至少一个所述分段下面和/或上面的至少一个翼(7)产生动态升力，以及通过来自推力产生器的推力(P1，P2)来产生动态提力。
7.根据权利要求1所述的飞行器，其中，偏心的驱动组件(4)设置于至少一个所述分段(2，21-24)之下，所述驱动组件(4)的燃料是在所述气体单元(2，21-24)中的所述气态能量介质。
CN200880130327.3A 2008-07-11 2008-07-28 具有能量介质的分段式飞行器 Active CN102137790B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102008002939A DE102008002939A1 (de) 2008-07-11 2008-07-11 Segmentiertes Luftfahrzeug mit Energiemedium
EP102008002939.4 2008-07-11
PCT/EP2008/059879 WO2010003468A2 (de) 2008-07-11 2008-07-28 Segmentiertes luftfahrzeug mit energiemedium

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CN102137790B true CN102137790B (zh) 2015-03-04

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US (1) US20110108661A1 (zh)
EP (1) EP2300312B1 (zh)
CN (1) CN102137790B (zh)
CA (1) CA2730416A1 (zh)
DE (1) DE102008002939A1 (zh)
ES (1) ES2399485T3 (zh)
HK (1) HK1159039A1 (zh)
WO (1) WO2010003468A2 (zh)

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US2451815A (en) * 1941-07-16 1948-10-19 Wingfoot Corp Airship
US4032085A (en) * 1973-03-21 1977-06-28 Papst Hermann E R Dirigible, especially non-rigid dirigible
US6148609A (en) * 1999-05-27 2000-11-21 Provitola; Anthony Italo Turbo-rocket thruster
EP1175332A2 (en) * 1999-04-28 2002-01-30 Anthony I. Provitola Airship/spacecraft
DE10053775A1 (de) * 2000-10-30 2002-05-08 Frank Epperlein Luftfahrzeug

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US3079106A (en) * 1961-04-17 1963-02-26 Gen Mills Inc Boundary layer control for gas filled balloons and airships
US4773617A (en) * 1987-03-05 1988-09-27 Mccampbell Burton L Lighter-than-air craft
JPH04169397A (ja) * 1990-10-31 1992-06-17 Sosuke Omiya 飛行船
AU2502192A (en) * 1991-09-09 1993-04-05 Av-Intel Inc. Dirigible airship
CZ294021B6 (cs) * 1996-06-10 2004-09-15 Cherokee Ltd Stavebnicová modulární jednotka vzducholodi a vzducholoď z nich postavená
WO2002012060A2 (en) * 2000-08-08 2002-02-14 Southwest Research Institute Multiple-lobed hull airships
JP3522711B2 (ja) * 2001-05-11 2004-04-26 川崎重工業株式会社 飛行船
KR20080097489A (ko) * 2004-09-17 2008-11-05 닛폰 바루카 고교 가부시키가이샤 복합 실링재
US7552893B2 (en) * 2005-09-28 2009-06-30 21St Century Airship Technologies Inc. Airship & method of operation
US7500637B2 (en) * 2005-09-30 2009-03-10 Lockheed Martin Corporation Airship with lifting gas cell system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2451815A (en) * 1941-07-16 1948-10-19 Wingfoot Corp Airship
US4032085A (en) * 1973-03-21 1977-06-28 Papst Hermann E R Dirigible, especially non-rigid dirigible
EP1175332A2 (en) * 1999-04-28 2002-01-30 Anthony I. Provitola Airship/spacecraft
US6148609A (en) * 1999-05-27 2000-11-21 Provitola; Anthony Italo Turbo-rocket thruster
DE10053775A1 (de) * 2000-10-30 2002-05-08 Frank Epperlein Luftfahrzeug

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EP2300312B1 (de) 2012-11-14
WO2010003468A2 (de) 2010-01-14
CN102137790A (zh) 2011-07-27
HK1159039A1 (zh) 2012-07-27
US20110108661A1 (en) 2011-05-12
WO2010003468A4 (de) 2010-09-16
CA2730416A1 (en) 2010-01-14
EP2300312A2 (de) 2011-03-30
WO2010003468A3 (de) 2010-07-22
DE102008002939A1 (de) 2010-01-14
ES2399485T3 (es) 2013-04-01

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