• 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 comprising a structure, two or more wings (2, 5), one or more engines (4, 16), and some braces (3, 6), each of which joins a wing with a point of the structure by below the point of unión of the wing with the structure, where the braces are apt to rotate around its longitudinal axis. The braces fulfill a double function: of element of structural reinforcement for the wings and, simultaneously, of sustentation element when rotating along its longitudinal axis its angle of incidence varies and generates a variable aerodynamic lift force. The aircraft may also have fusiform balloons with a gas lighter than air, thus combining the aerodynamic lift of the wings and the braces with the aerostatic lift of the fusiform balloon. Preferably the aircraft is of modular construction. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2611024A1
    申请号:ES201531562
    申请日:2015-10-30
    公开日:2017-05-04
    发明作者:Conrado Vilalta Casals；Antonio QUINTANA SANS
    申请人:Conrado Vilalta Casals；Antonio QUINTANA SANS；
    IPC主号:
    专利说明:

    image 1
    image2
    image3
    image4
    image5
    image6
    image7
    image8
    image9
    image10
    image11
    image12
    image13
    image14
    权利要求:
    Claims (1)
    [1]
    image 1
    image2
    image3
    类似技术:
    公开号 | 公开日 | 专利标题
    BR112018009344A2|2018-11-13|air vehicle with folding components
    JP2019189225A5|2021-02-04|
    EP3119673A4|2017-11-15|Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
    WO2016035068A3|2016-09-01|Tilt winged multi rotor
    EA201491528A1|2015-01-30|AERIAL VERTICAL TAKE-OFF AIRCRAFT AND LANDING WITH TWO WING DESIGNS
    EA201300348A1|2013-08-30|TRANSFORMABLE AIRCRAFT VERTICAL TAKEOFF AND LANDING WITH A TURNING WING
    CN103847954B|2015-10-07|Telescopic wing
    WO2015080785A3|2015-08-06|Extended thrust reverser cascade
    EP3604122A4|2021-01-13|Aircraft with super high aspect ratio based on self-unfolding folding wing technology
    WO2015007259A3|2015-03-19|Changeable wing profile
    EP3119674A4|2018-02-14|Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
    ES2512915A1|2014-10-24|Deformable wing including a mobile upper surface
    ES2611024A1|2017-05-04|Aircraft |
    RU2013115878A|2014-10-20|METHOD FOR MANAGING, STABILIZING AND CREATING AN ADDITIONAL AIRCRAFT LIFTING POWER
    ES2525956B1|2015-10-09|Biaeronave for air transport in general with ability to perform take-off and landing operations with each other in flight
    RU2015130993A|2017-01-30|ASYMMETRIC WING HELICOPTER
    RU2015149094A|2017-05-22|Application of a method of flight with asymmetric thrust for landing an aircraft in crosswind
    ES1271359Y|2021-10-04|AERODYNAMIC FLYING PROJECTILE
    RU2013144784A|2015-04-27|HELICOPTER
    RU137260U1|2014-02-10|FLYING PLATE FOR ATMOSPHERIC FLIGHTS
    RU2601998C1|2016-11-10|Tandem type airframe
    WO2015143098A3|2015-11-26|Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
    ES1136192U|2015-02-16|Airplane with flight control devices |
    ES2555162A1|2015-12-29|Airplane with double counter-clockwise propellers, and domes |
    BR112019000583A2|2019-04-24|aircraft wing, aircraft and use of an upgrade part to produce the wing
    同族专利:
    公开号 | 公开日
    ES2611024B1|2018-03-02|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US5823468A|1995-10-24|1998-10-20|Bothe; Hans-Jurgen|Hybrid aircraft|
    US6626398B1|2001-05-10|2003-09-30|Mission Technologies, Inc.|Unmanned biplane for airborne reconnaissance and surveillance having staggered and gapped wings|
    US20140339356A1|2010-03-23|2014-11-20|Athene Works Limited|Aerial vehicle and method of flight|
    US20120074264A1|2010-09-24|2012-03-29|Heaton Clifford D|Airplane wing|
    US20150248711A1|2012-09-27|2015-09-03|Solar Ship Inc.|Autonomous self-powered airborne communication and media station, and method of using it for displaying, broadcasting and relaying data|ES2711840A1|2017-11-03|2019-05-07|Torres Martinez M|SIMPLIFIED OPERATION AIRCRAFT |
    法律状态:
    2018-03-02| FG2A| Definitive protection|Ref document number: 2611024 Country of ref document: ES Kind code of ref document: B1 Effective date: 20180302 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201531562A|ES2611024B1|2015-10-30|2015-10-30|AIRCRAFT|ES201531562A| ES2611024B1|2015-10-30|2015-10-30|AIRCRAFT|
    [返回顶部]