Guided missile pylon device

Abstract

The invention discloses a missile pylon device, and relates to the technical field of assembly equipment, the missile pylon device comprises a base plate, one side of the base plate is provided with a chute, the chute is internally provided with a bidirectional driving mechanism, the bidirectional driving mechanism is provided with two lifting assemblies, the lifting assemblies are provided with bearing assemblies, the top of the base plate is provided with a hydraulic cylinder, and the top of the base plate is provided with a hydraulic cylinder. A lifting platform plate is fixed to the top end of the hydraulic cylinder, a circumferential adjusting mechanism is fixed to the top of the lifting platform plate, a first top plate and a second top plate are arranged on the two sides of the circumferential adjusting mechanism correspondingly, a U-shaped plate is fixed between the first top plate and the second top plate, and a plurality of notches are formed in the outer side of the second top plate; and a fixed shaft is rotationally mounted in the notch. The missile can be driven to complete the whole-circle direction adjusting work, the angle adjusting requirement for missile installation work is met, and after missile loading is completed, the supporting wheels can be used for limiting and supporting the side faces of the missile.

Description

technical field [0001] The invention relates to the technical field of assembly equipment, in particular to a missile hanger device. Background technique [0002] The application fields of pylons are very wide, whether it is in the field of daily life or even in the field of military industry, there are corresponding ones. At present, missile pylons are often equipped on the mounting equipment of aircraft weapons, but most of the common pylons are The simple bracket cannot effectively adjust the circumferential position of the missile, which brings inconvenience to the operator and has corresponding limitations. [0003] The existing Chinese utility model patent with the publication number CN210852937U discloses a missile pylon device, which includes a mounting base plate and a pylon main body, and the pylon main body is fixedly connected to the mounting base plate on the bottom side through a wing nut. The upper end of the frame body is provided with a bracket through a pi...

AI Technical Summary

Problems solved by technology

[0004] The above invention has some deficiencies during use. For example, after using the bracket to place the missile, push the bottom end of the bracket through the first lead screw and the second lead screw, so that the bracket and the missile will rotate in a circumferential direction as a whole. , where the circumferential rotation angle of the missile is limited, which cannot meet the needs of use. In addition, the positioning handle is used for positioning and clamping on the side of the missile. The contact surface is small. After the axial rotation is adjusted, the positioning handle is located under the side of the missile. The supporting force between the positioning handles will become larger, causing the surface of the missile to be concave

Images