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    • 24. 发明公开
    • TESTING DEVICE AND METHOD FOR TESTING STRENGTH OF AIRCRAFT
    • TESTVORRICHTUNG UND VERFAHREN ZUM TESTEN DER FESTIGKEIT EINES FLUGZEUGS
    • EP3121583A1
    • 2017-01-25
    • EP14886567.8
    • 2014-12-24
    • Mitsubishi Aircraft Corporation
    • TABA, ShunsukeNAKAMURA, ToshioTSUKIGASE, KaoruKUMAGAI, KeisukeFUKUOKA, Toshiyasu
    • G01N3/10B64F5/00G01N3/36
    • G01N3/12B64C1/061B64C1/064B64C1/12B64F5/60G01M5/0075G01N3/08
    • Provided is a testing device for testing the strength of an aircraft using a curved specimen, the testing device being capable of safely and quickly generating desired stress by reliably applying inner pressure to the specimen, the testing device enabling the reliable observation of generated damage. A testing device (1) for applying inner pressure, which corresponds to the difference in pressure between the outside and inside of a portion to be tested, to a curved specimen (10) corresponding to a portion to be tested of the fuselage of an aircraft is provided with: a pressure container (22) for forming a cavity (23) between the pressure container (22) and the specimen (10); and a rod (25) for restraining the specimen (10) against the inner pressure. The pressure container (22) faces the outer surface of the specimen (10). Inner pressue is applied to the specimen (10) by reducing pressure within the cavity(23).
    • 提供了一种用于使用弯曲试样测试飞行器的强度的测试装置,该测试装置能够通过可靠地向试样施加内部压力而安全且快速地产生所需的应力,该测试装置能够可靠地观察所产生的损伤。 一种用于将对应于待测试部分的外部和内部之间的压力差的内部压力的内部压力应用于与飞行器的机身的被测试部分相对应的弯曲试样(10)的测试装置(1) 设置有:用于在压力容器(22)和样本(10)之间形成空腔(23)的压力容器(22); 以及用于限制样本(10)抵抗内部压力的杆(25)。 压力容器(22)面向试样(10)的外表面。 通过减小空腔(23)内的压力将内部压力施加到试样(10)上。