基本信息:
- 专利标题： High-Altitude Aerial Vehicle
- 专利标题（中）：高空飞行器
- 申请号：US13310125 申请日：2011-12-02
- 公开(公告)号：US20120138733A1 公开(公告)日：2012-06-07
- 发明人： Manfred Hiebl , Hans-Wolfgang Pongratz
- 申请人： Manfred Hiebl , Hans-Wolfgang Pongratz
- 申请人地址： DE Ottobrunn
- 专利权人： EADS Deutschland GmbH
- 当前专利权人： EADS Deutschland GmbH
- 当前专利权人地址： DE Ottobrunn
- 优先权： DE102010053372.6 20101203
- 主分类号： B64B1/02
- IPC分类号： B64B1/02 ; B64B1/40
摘要：
A high-altitude aerial vehicle, in particular an aerial vehicle for the stratosphere that is designed as a non-rigid aerial vehicle with a hull, that has an at least partially inflated envelope with a buoyant gas other than air, which is lighter than air, in particular hydrogen. The hull is provided with at least a first chamber for the buoyant gas and at least a second chamber that can be inflated with air. Between the first and second chambers a flexible partition wall is provided that is preferably formed by a flexible membrane. Inflating of the second chamber, preferably with hot air depending on the flight altitude, can be controlled or regulated in such a way that the envelope of hull is always tautly inflated.
摘要（中）：
高空飞行器，特别是用于平流层的空中飞行器，其被设计为具有船体的非刚性空中飞行器，其具有至少部分充气的信封，其具有比空气轻的空气的浮力气体，其比空气轻 ，特别是氢。 船体设置有至少一个用于浮力气体的第一室和至少一个可以用空气充气的第二室。 在第一和第二腔室之间设置有优选由柔性膜形成的柔性分隔壁。 可以以这样一种方式来控制或调节第二室的膨胀，优选地依赖于飞行高度的热空气，使得船体的外壳总是被张紧地膨胀。