Vibration absorbing structure, inertia measurement structure with vibration absorbing function and aircraft

• Main Authors: CHE JIANMING, CHEN ZHIMING, CAI WEI
• Format: Patent
• Language: English
• Published: 14.10.2015
• 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; HEATING; LIGHTING; MEANS FOR DAMPING VIBRATION; MECHANICAL ENGINEERING; PARACHUTES; PERFORMING OPERATIONS; SHOCK-ABSORBERS; SPRINGS; THERMAL INSULATION IN GENERAL; TRANSPORTING; WEAPONS

The invention relates to a vibration absorbing structure, an inertia measurement structure with the vibration absorbing function and an aircraft. The vibration absorbing structure is used for absorbing vibration of an inertia measurement unit in the aircraft and comprises a spring stabilizing assembly and a damping body, wherein the spring stabilizing assembly is arranged between the inertia measurement unit and a frame structure of the aircraft so as to make the inertia measurement unit keep tending to be stable in a preset state, and the damping body is arranged between the inertia measurement unit and the frame structure of the aircraft so as to absorb vibration energy output by the aircraft to the inertia measurement unit. By means of the technical scheme, influences of vibration on the inertia measurement unit can be stopped stably for a long time.