PROBLEM TO BE SOLVED: To provide systems and methods for starting an engine on an aircraft.SOLUTION: One example aspect of the present disclosure is directed to an integrated starter for starting an engine on an aircraft. The integrated starter includes an air turbine starter. The integrated starter includes a starter air valve integrated with the air turbine starter. The integrated starter includes a controller configured to control the starter air valve. The starter air valve can be movable between a first position and at least a second position to regulate the flow of fluid into the air turbine starter. An output torque of the air turbine starter can be dependent at least in part on the flow of fluid into the air turbine starter.SELECTED DRAWING: Figure 3

    【課題】航空機上のエンジンを始動させるためのシステムおよび方法を提供すること。【解決手段】本開示の一態様例は、航空機上のエンジンを始動させるための統合始動機を対象とする。統合始動機は空気タービン始動機を含む。統合始動機は、空気タービン始動機に統合された始動機空気弁を含む。統合始動機は、始動機空気弁を制御するように構成された制御器を含む。始動機空気弁は、空気タービン始動機内への流体の流れを調節するために第1の位置と少なくとも第2の位置との間を移動可能であり得る。空気タービン始動機の出力トルクは、少なくとも部分的に空気タービン始動機内への流体の流れに依存することができる。【選択図】図3


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    Title :

    INTEGRATED STARTER FOR AIRCRAFT


    Additional title:

    航空機用統合始動機



    Publication date :

    2018-04-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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