Aircraft landing gear main frame outer cylinder lining clamp

The utility model discloses an aircraft landing gear main frame outer cylinder lining clamp which comprises a chuck and a plurality of clamping jaws arranged on the chuck, the clamping jaws are evenly distributed in an outward radial shape with the center point of the chuck as the center, each clamping jaw is fixedly provided with an installation box, and a power source is arranged in each installation box. Each mounting box is provided with a clamping mechanism, a bushing body of the bushing is clamped and fixed through the clamping mechanisms, and each mounting box is further provided with a first recognition mechanism and a second recognition mechanism, the first recognition mechanism is used for pressure recognition in the bushing body clamping process to prevent insufficient clamping force, and the second recognition mechanism is used for preventing excessive clamping force. The clamp has a good clamping effect, in the process of clamping and fixing the bushing body, a first recognition mechanism for rec