PROBLEM TO BE SOLVED: To provide an efficient system and method of absorbing shocks within a power drive unit (PDU) of an aircraft.SOLUTION: A shock absorber assembly 200 is configured to be operatively connected to a drive shaft of a power drive unit (PDU) of an aircraft. The shock absorber assembly may include a first hub 204, a second hub, and a bull gear 201 having at least a portion sandwiched between the first and second hubs. The bull gear is configured to rotate independently of the first and second hubs by a controlled distance in response to a mechanical malfunction of the PDU.SELECTED DRAWING: Figure 2

    【課題】航空機の動力駆動装置(PDU)内部のショックを吸収する効率的なシステム及び方法を提供する【解決手段】ショックアブソーバーアセンブリ200が、航空機の動力駆動装置(PDU)の駆動軸に動作的に接続されるように構成される。ショックアブソーバーアセンブリは、第一のハブ204、第二のハブ、及び少なくとも一部分が第一のハブと第二のハブの間に挟まれたブルギア201を含み得る。ブルギアは、PDUの機械的誤作動に応じて制御された距離だけ、第一のハブ及び第二のハブから独立して回転するように構成される。【選択図】図2


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    Title :

    SHOCK ABSORBER ASSEMBLY FOR POWER DRIVE UNIT OF VEHICLE


    Additional title:

    車両の動力駆動装置用のショックアブソーバーアセンブリ


    Contributors:

    Publication date :

    2016-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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