公开(公告)号：WO2014203237A2

公开(公告)日：2014-12-24

申请号：PCT/IL2014/050422

申请日：2014-05-14

Applicant: RAFAEL ADVANCED DEFENSE SYSTEMS LTD.

Inventor： SAROKA, Arie ,  SCHOENMANN, Amnon

CPC classification number: B64C1/14 ,  B64C3/40 ,  B64C7/00 ,  B64C9/02 ,  F42B10/14 ,  F42B10/38 ,  Y02T50/14 ,  Y02T50/32

Abstract: A shutter mechanism for covering a wing's spreading opening formed in an airborne body and a method for covering such opening while implementing the shutter mechanism, wherein the shutter comprises at least one flap assembly, and wherein from the instant that a deployed wing of the airborne body passed and moved over it, it is biased by traction of at least one springy element to an angular motion around an axis, unto a condition where the flap component of the assembly is positioned so that it is substantially conformal to the outline of the outer surface of the fuselage of the airborne body and while it covers the opening through which the wing passed in its motion; and from an instant that the wing returned and connected to the flap component of the assembly, the flap is biased to an angular motion counter the spring, to the state that the wing returns and is relocated on its top surface.

Abstract translation: 一种用于覆盖形成在空气传播体中的机翼传播开口的快门机构和一种在实现快门机构的同时覆盖这种开口的方法，其中快门包括至少一个挡板组件，并且其中从空中机体的部署翼 通过并在其上移动，它被至少一个弹性元件的牵引力偏压到围绕轴线的角运动，其中组件的折翼部件被定位成使得其基本上与外表面的轮廓一致 机身的机身，同时它覆盖机翼通过其运动的开口; 并且从翼返回并连接到组件的翼片部件的瞬间，翼片被偏压到与弹簧相反的角运动，到翼返回并被重新定位在其顶表面上的状态。