Aircraft bracket

The invention relates to an aircraft bracket. The aircraft bracket comprises triangular supports, a cross brace arranged between the two triangular supports, a jacking device arranged on the two triangular supports, and a supporting plate arranged on the jacking device. The shape of the top face of the supporting plate is matched with that of the bottom face of an aircraft. Felt is laid on the supporting plate. The jacking device comprises a left jack and a right jack which are arranged on the two triangular supports correspondingly. The two jacks are used for acting on the supporting plate simultaneously, the supporting plate is jacked up, an aircraft body is jacked up through a pulling handle, stability and reliability are achieved, the safety coefficient can be increased, meanwhile, thefelt is arranged on the supporting plate, on the one hand, damping can be achieved, and on the other hand, the supporting plate can be prevented from scratching the surface of the aircraft body. 本发明涉及种飞机托架，其包括三角支架、设置在两个三角支架之