Aero-engine accessory sinusoidal vibration endurance test time calculation method

The invention provides an aero-engine accessory sinusoidal vibration endurance test time calculation method, and belongs to the technical field of aero-engines, and the method comprises the steps: determining the structural parameters of an aero-engine and the range of high and low pressure rotating...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GAO YANG, SUN XIAOHUAN, XU KAICHI, WANG ZHIHUI, WANG YI, WU XIN, LIU HAINIAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR MEASURING PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING
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