• 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:
    The air wedge for landing gear hatch is characterized by being a metal wedge-shaped air plate (3), located obliquely in the lower area of the fuselage (1) of an airplane, just in front of the the front edge of the gate (2) of the landing gear. By tilting it about eight degrees downwards, the air against the advance of the airplane will strike against its inclined plane, and will deviate from the landing gear gate (2), so that this air does not lower the temperature further, since rather cold, that the gate (2) receives from the existing atmosphere at the altitude for which the plane usually travels, which is usually about twelve thousand meters. (Machine-translation by Google Translate, not legally binding)
    公开号:ES2613227A1
    申请号:ES201500849
    申请日:2015-11-23
    公开日:2017-05-23
    发明作者:Fco. Javier Porras Vila
    申请人:Fco. Javier Porras Vila；
    IPC主号:
    专利说明:

    DEA / RE WEDGE FOR DEATERR / ZAJE TRAIN COMPUTEROBJECT OF THE INVENTION
    The main objective of the present invention is that of rt. '<To minimize the likelihood that problems will be encountered when deploying the Alerri Train7 ..air of an Airplane. One of the main problems is usually the Cold of the existing atmosphere in the usual Altitude of the Aircraft. which is usually about twelve thousand meters. This Frlo strikes the Gate (2). Y. from it: l. it is introduced inside the room where the pieces of the Train of Aterri7..aje are silhouetted, which tend to freeze. except for the heating that is put into the room. To this Cold, we must also add the one that adds the Air against the advance of the Plane that, when traveling about a thousand kilometers by
    10 hour contributes to the temperature that supports the Gate (2) of the Landing Gear. decrease even more than it would decrease in the event that the plane remained quiCIO, without moving. to that Allitude of twelve thousand meters. If the Cold of the atmosphere, at that Altitude, is (- / 0 "C). The Air against the advance can decrease it to (-40" C) or (-50 "C). Invention, by tlll1 O, this Air will be diverted. · by the Cui'la (3) -, of the Gate (2), which will mean that it
    15 Keep COII your (· / 0 "C), Cold this COlltr, .¡¡ which is much easier to fight.
    BACKGROUND OF I.A INVFJVCION
    I do not know background information for the present invention.
    DESCRIPTION OF THE INVENTION / ON The IC / 11a of air for gate (Iren de a / errizaje. Is an oblique metal plate. And.
    20 Wedge (3), which we will place ahead of the front edge of the Gate (2) of the Landing Gear. which is located in a hole in the lower area of the Fuselage (1) of an airplane. By delanle of her we polle the Cui'la of air (3), that will be in charge of diverting the air in control of the advance. pair,. 110 that falls against that Compuena (2). The Wedge (3) will be tilted down about eight gmdos. Approximately, and, it will serve that the air against the advance does not lower the temperature of the
    25 Compuena (2), more than the decrease of fomla natul "" 'dl the existing atmosphere at the usual Altitude of the Plane. which usually runs about twelve thousand meters from Alturd. Date of the invention: (20. 11 .15). DESCRIPTION OF /..THE FIGURES Figllra ,, "1: Side view of the Gate (2) of the Aterri Train 7 ..age located in a hole in the lower area of the Fuselage (1) of an Airplane. In front, we put the Cui a of air (3), which will be responsible for diverting the air in contm of the feed, pam that does not affect the gate (2). Figure 11 "/: 1) Fusclaje, 7..ona lower 2 ) Landing gear 3) Air wedge 35
    DE) 'CRII'C / 6N OF A PREFERRED REALlZAC / 6N MODE
    Air wedge for train gate, landing. It is characterized by being a metal plate in the shape of an air cui'ia (3), which is located obliquely in the lower 7-one of the fuselage (1) of an airplane. just ahead of the front edge of the Compuena (2) of the Landing Gear. The Cui'i.a (3) 5 will be made of the same material as the Fuselage (1). though. It can also be made of aluminum, or. of any metallic material Olro. When tilted eight gr'.Goes, approximately, downwards, the Air in with! R.! of the 3Vl.IIlCe of the Plane. Your indinished plane will affect contrJ. Y. It will deviate from the Compuen: 1 (2) of the Aterri.l.aje Train, pam that this Air does not diminish the temptation. already quite cold, that the Compuena (2) receives from the cxistelnte almósfcm in the Aghitude through which the Plane travels regularly.
    10 which is usually about twelve thousand meters.
    权利要求:
    Claims (1)
    [1]
    1) Air clutch to fill it with Iren de Lanching, characterized by being a metal plate in the wedge of air wedge (3). It is located in an oblique position in the lower zone of the Fuselage (1) of an Airplane, ahead of the previous arislll of the Compuena (2) of the Landing Train. La Compuena
    5 (2) is located in a hole in the lower area of the Fuselage (1) of the plane. and, in front of her we put the wedge of air (3). This wedge (3) will be inclined eight gmdos. down.
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    同族专利:
    公开号 | 公开日
    ES2613227B1|2018-02-27|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    CN101274667A|2008-04-01|2008-10-01|傅廷璜|Anti-ice-snow aerocraft|
    US20150210399A1|2012-02-27|2015-07-30|Borealis Technical Limited|Method for inflight deicing of landing gear and wheel bays in aircraft with onboard drive means|
    EP2692640A2|2012-07-31|2014-02-05|Goodrich Corporation|Ice protection system|
    CN104859846A|2014-02-26|2015-08-26|成都智利达科技有限公司|Safe automatic control device for undercarriage and undercarriage compartment|
    法律状态:
    2018-02-27| FG2A| Definitive protection|Ref document number: 2613227 Country of ref document: ES Kind code of ref document: B1 Effective date: 20180227 |
    优先权:
    申请号 | 申请日 | 专利标题
    ES201500849A|ES2613227B1|2015-11-23|2015-11-23|Air wedge for landing gear gate|ES201500849A| ES2613227B1|2015-11-23|2015-11-23|Air wedge for landing gear gate|
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