To provide an electronic component which enables posture control of an air vehicle to be performed after completion of production.SOLUTION: An electronic component 1 according to the invention may be attached to an air vehicle. The electronic component 1 includes: an arm part 20; an attachment part 10 for attachment to a body part of the air vehicle; and a connection part 30 which connects the arm part 20 to the attachment part 10 so that the arm part 20 and the attachment part 10 can be displaced in a predetermined range. The connection part 30 is connected to a position which corresponds to or substantially corresponds to a centroid of the arm part 20. Further, in a state where the electronic component is attached to the air vehicle, the connection part 30 corresponds to or substantially corresponds to a center of generation of lift force of the air vehicle.SELECTED DRAWING: Figure 3

    【課題】飛行体の姿勢制御を事後的にも行うことのできる電子部品を提供する。【解決手段】本発明による電子部品1は、飛行体に取り付け可能なものである。電子部品1は、アーム部20と、前記飛行体の本体部に取付けるための取付部10と、アーム部20と取付部10とが所定の範囲で変位可能となるようにこれらを接続する接続部30とを備えている。接続部30は、アーム部20の重心と一致又は略一致する位置に接続されている。更に、前記飛行体に取り付けられた状態で、接続部30は前記飛行体の揚力発生中心と一致又は略一致している。【選択図】図3


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    Title :

    ELECTRONIC COMPONENT AND AIR VEHICLE TO WHICH ELECTRONIC COMPONENT IS ATTACHED


    Additional title:

    電子部品及び当該電子部品を取り付けた飛行体


    Contributors:

    Publication date :

    2020-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H04N PICTORIAL COMMUNICATION, e.g. TELEVISION , Bildübertragung, z.B. Fernsehen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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