Structure and aircraft are measured to shock -absorbing structure , inertia that has a shock -absorbing function

• Main Authors: CHE JIANMING, CHEN ZHIMING, CAI WEI
• Format: Patent
• Language: English
• Published: 11.11.2015
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; BLASTING; COSMONAUTICS; ENGINEERING ELEMENTS AND UNITS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS; GYROSCOPIC INSTRUMENTS; HEATING; LIGHTING; MEANS FOR DAMPING VIBRATION; MEASURING; MEASURING DISTANCES, LEVELS OR BEARINGS; MECHANICAL ENGINEERING; NAVIGATION; PARACHUTES; PERFORMING OPERATIONS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY; PHYSICS; SHOCK-ABSORBERS; SPRINGS; SURVEYING; TESTING; THERMAL INSULATION IN GENERAL; TRANSPORTING; WEAPONS

The utility model relates to a structure and aircraft are measured to shock -absorbing structure, inertia that has a shock -absorbing function, shock -absorbing structure is arranged in carrying out the shock attenuation to the inertia measuring unit of aircraft, shock -absorbing structure includes: first spring assembly, first spring assembly contain set up in inertia measuring unit's top end with a plurality of springs between the frame construction's of aircraft the top, the second spring assembly, the second spring assembly contain set up in inertia measuring unit's bottom end with a plurality of springs between frame construction's the bottom. Through this disclosed technical scheme, can be for a long time, the separation vibrations are to inertia measuring unit's influence steadily.