To provide a system and method for restraining a cargo.SOLUTION: An aircraft cargo restraint system 100 includes an attenuator member 102 fixed at two first attachment locations 104 within a cargo storage compartment 106 of a fuselage 108 of an aircraft 110. The cargo restraint system also includes a cargo restraint 116 configured to be coupled to the attenuator member at a second attachment location 122 of the attenuator member, located between the two first attachment locations. The cargo restraint is configured to restrain cargo loaded on a cargo deck 112 of the cargo storage compartment. The attenuator member is configured to deflect in response to a load applied to the attenuator member by the cargo restraint.SELECTED DRAWING: Figure 4

    【課題】貨物を拘束するためのシステム及び方法を提供する。【解決手段】航空機貨物拘束システム100は、航空機110の胴体108の貨物貯蔵室106内の2つの第1の取付け箇所104に固定された軽減部材102を含む。貨物拘束システムはまた、2つの第1の取付け箇所の間に位置する軽減部材の第2の取付け箇所122で軽減部材に結合される貨物拘束具116を含む。貨物拘束具は、貨物貯蔵室の貨物デッキ112に積載された貨物を拘束するように構成される。軽減部材は、貨物拘束具によって軽減部材に加えられる荷重に応じて撓むように構成される。【選択図】図4


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    Title :

    SYSTEM AND METHOD FOR RESTRAINING CARGO


    Additional title:

    貨物を拘束するためのシステム及び方法



    Publication date :

    2019-03-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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