PROBLEM TO BE SOLVED: To provide structural integration of attachments that accommodates a mismatch in the coefficient of thermal expansion (CTE) occurring in a lip skin and a bulkhead and reduces thermally induced fatigue, for nacelle and engine cowlings.SOLUTION: A structural system for accommodating the thermal expansion of a nacelle lip skin 24 and supporting structure has the lip skin 24 and a first angle element 62 attached to the lip skin 24. The first angle element 62 has a free edge 82 that is scalloped to accommodate thermal stresses. A bulkhead 60 is attached to the first angle element 62.SELECTED DRAWING: Figure 5

    【課題】ナセル及びエンジンカバーにおいて、ヘリ外板とバルクヘッドで発生する熱膨張係数(CTE)の不一致に対応し、熱的に誘導される疲労を軽減する取付具の構造一体化を提供する。【解決手段】ナセルのへり外板24と支持構造の熱膨張に対応するための構造システムは、へり外板24と、へり外板24に取り付けられた第1の角度要素62とを有する。第1の角度要素62は、熱応力に対応するために扇形になった自由エッジ82を有する。バルクヘッド60は第1の角度要素62に取り付けられる。【選択図】図5


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    Title :

    METHOD OF ATTACHING NACELLE STRUCTURE TO MINIMIZE FATIGUE LOADING


    Additional title:

    疲労荷重を最小限に抑えるためのナセル構造を取り付ける方法


    Contributors:

    Publication date :

    2016-09-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge



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