• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Aircraft of low wing load, comprising a bearing surface (1) with a wing-shaped configuration, stabilizers of the airfoil (1), and means of propulsion (5) of the aircraft, where the airfoil ( 1) comprises an upper cover (11), a lower cover (12), and two longitudinal beams (6) arranged between the upper (11) and lower (12) covers, and because the bearing surface (1) has a longer length that its width, obtaining an aircraft with a low relation between the weight of the aircraft and the airfoil, lower aerodynamic drag and lower energy consumption, allowing for shorter take-off and landing distances, with adequate stability. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2585245A1
    申请号:ES201630351
    申请日:2016-03-23
    公开日:2016-10-04
    发明作者:Manuel Torres Martinez
    申请人:Manuel Torres Martinez；
    IPC主号:
    专利说明:

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    权利要求:
    Claims (1)
    [1]
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    同族专利:
    公开号 | 公开日
    ES2585245B1|2017-03-17|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    GB427186A|1933-10-17|1935-04-17|Petters Ltd|Improvements in or relating to tailless aeroplanes|
    US1980246A|1933-12-08|1934-11-13|Austin Gene|Airplane sky sled|
    US2108093A|1935-04-30|1938-02-15|Charles H Zimmerman|Aircraft|
    US2561291A|1947-06-26|1951-07-17|Scott C Rethorst|Roadable aircraft|
    US4440361A|1980-11-18|1984-04-03|Mcgann Rodney|Aircraft structure|
    US8292220B1|2009-03-19|2012-10-23|Northrop Grumman Corporation|Flying wing aircraft with modular missionized elements|
    US8353478B1|2009-03-25|2013-01-15|The Boeing Company|Blended wing aircraft|
    US20130206920A1|2010-06-16|2013-08-15|Eads Deutschland Gmbh|Driven Aircraft, in Particular to an Aircraft Designed as a Flying Wing and/or Having a Low Radar Signature|
    US20160009391A1|2013-11-04|2016-01-14|Eric Walter Friesel|Stable Low Aspect Ratio Flying Wing|
    CN104029820A|2014-06-11|2014-09-10|青岛宇泰新能源科技有限公司|Solar flying saucer capable of flying for long time|
    法律状态:
    2017-03-17| FG2A| Definitive protection|Ref document number: 2585245 Country of ref document: ES Kind code of ref document: B1 Effective date: 20170317 |
    2021-09-30| FD2A| Announcement of lapse in spain|Effective date: 20210930 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201630351A|ES2585245B1|2016-03-23|2016-03-23|LOW LOAD AIRCRAFT AIRCRAFT|ES201630351A| ES2585245B1|2016-03-23|2016-03-23|LOW LOAD AIRCRAFT AIRCRAFT|
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