发明申请
- 专利标题： MISSILE HAVING A TURBINE-COMPRESSING MEANS-UNIT
- 专利标题（中）： 具有涡轮压缩机构的MISSILE
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申请号： US14607894申请日： 2015-01-28
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公开(公告)号： US20150211445A1公开(公告)日： 2015-07-30
- 发明人: Guido Kurth , Christoph Bauer
- 申请人： Guido Kurth , Christoph Bauer
- 申请人地址： DE Aschau am Inn
- 专利权人： Bayern-Chemie Gesellschaft fur Flugchemische Antriebe mbH
- 当前专利权人： Bayern-Chemie Gesellschaft fur Flugchemische Antriebe mbH
- 当前专利权人地址： DE Aschau am Inn
- 优先权： DE102014000991.2 20140129
- 主分类号： F02K9/42
- IPC分类号： F02K9/42 ; F02K3/00 ; F42B15/10
摘要：
Missile having a jet engine (2) comprising at least one turbine (3) and at least one compressing means (4), wherein gas generated in at least one gas generator (7) of the missile (1) drives a turbine (3). The compressing means (4) and the turbine (3) are arranged opposite to the flight direction (6) adjacent to each other.
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