The invention discloses an inherent frequency measuring device for 600 DEG C high-temperature thermal vibration
coupling test of a high-speed
cruise missile airfoil surface. The device comprises a
missile airfoil
surface structure test piece, a
quartz lamp heating array, a
vibration exciter, a
ceramic extension rod, an acceleration
transducer, a computer and a heat insulation baffle plate. In the high-temperature thermal vibration
coupling test of the
cruise missile airfoil surface, the missile airfoil surface is quickly heated by using the
quartz lamp heating array and generates
random vibration through the
vibration exciter at the same time to form a 600 DEG C high-temperature thermal vibration
coupling test environment. The rigid
ceramic extension rod with high rigidity and high
temperature resistance is arranged on the missile airfoil surface to guide the vibration signals on the missile airfoil surface out of the high-temperature thermal field, and the high-temperature resistant lightweight
ceramic fiber heat insulation baffle plate is used for implementing thermal
diffusion prevention shielding for the
radiation thermal field. The normal temperature acceleration
transducer arranged at the cold end of the ceramic extension rod dynamically tracks and measures the vibration signals guided to the missile airfoil structure of the normal temperature zone to acquire the change rule of the inherent frequency of the missile airfoil surface under the high-temperature thermal vibration coupling test environment; and the device provides an effective dynamic high-temperature thermal vibration coupling test means for researching and manufacturing high-speed
cruise missiles.