发明公开
EP2582581A2 ANGETRIEBENES FLUGGERÄT, INSBESONDERE ALS NURFLÜGLER UND/ODER MIT GERINGER RADARSIGNATUR AUSGEBILDETES FLUGGERÄT
有权
动力飞行仪器，特别是作为一个飞翼和/或低雷达信号飞行大队经过培训
- 专利标题： ANGETRIEBENES FLUGGERÄT, INSBESONDERE ALS NURFLÜGLER UND/ODER MIT GERINGER RADARSIGNATUR AUSGEBILDETES FLUGGERÄT
- 专利标题（英）： Driven aircraft, in particular an aircraft designed as a flying wing and/or having a low radar signature
- 专利标题（中）： 动力飞行仪器，特别是作为一个飞翼和/或低雷达信号飞行大队经过培训
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申请号： EP11785286.3申请日： 2011-06-14
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公开(公告)号： EP2582581A2公开(公告)日： 2013-04-24
- 发明人: BICHLER, Bartholomäus , DORNWALD, Jochen , WEDEKIND, Gerhard
- 申请人： EADS Deutschland GmbH
- 申请人地址： Willy-Messerschmitt-Strasse 1 85521 Ottobrunn DE
- 专利权人： EADS Deutschland GmbH
- 当前专利权人： EADS Deutschland GmbH
- 当前专利权人地址： Willy-Messerschmitt-Strasse 1 85521 Ottobrunn DE
- 优先权： DE102010023938 20100616
- 国际公布： WO2012010116 20120126
- 主分类号： B64D33/02
- IPC分类号： B64D33/02 ; B64C39/10 ; B64D27/16
摘要：
The invention relates to an aircraft (10), comprising a fuselage body, a wing body (12), and at least one drive flow passage (16), which extends from an air inlet (18) directed forward (+x) on the body surface (14) via a jet engine (20) through the body (12) to a propelling nozzle (22) that opens toward the rear (-x) on the body surface (14). In order to enable greater design freedom in regard to the shape of the body (12), in particular in the manner of a flying wing having improved flight properties compared to known aircrafts, and/or to achieve an extreme reduction in the radar signature of the aircraft (10), at least one part of the jet engine (20), in particular the entire jet engine (20), is arranged upstream of the air inlet (18) as viewed in the flying direction (+x) of the aircraft (10) and the drive flow passage (16) has curvature sections (24, 28) designed and arranged suitably therefor.
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