Launching vehicle with locking mechanism and auxiliary erecting device

A locking mechanism and a technology for launching vehicles, applied in the field of launching vehicles, can solve the problems of high structural rigidity requirements, reduced connection accuracy, inconvenient operation, etc., and achieve the effects of reducing transportation costs, reducing burdens, and reducing cylinder diameters

Pending Publication Date: 2022-01-21
BEIJING ONESPACE TECH CO LTD +4
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] Aiming at the deficiencies in the prior art, the present invention provides a launching vehicle with a locking mechanism and an auxiliary erecting device, which solves the problems of manual loading and unloading of the erecting arm and the launching platform in the prior art. Decreased connection accuracy, high structural rigidity and high cost during rocket erection

Method used

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  • Launching vehicle with locking mechanism and auxiliary erecting device
  • Launching vehicle with locking mechanism and auxiliary erecting device
  • Launching vehicle with locking mechanism and auxiliary erecting device

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Embodiment Construction

[0022] The technical solutions in the present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0023] Such as figure 1 and Figure 7 As shown, a kind of launching car with locking mechanism and auxiliary erecting device includes locking mechanism and auxiliary erecting device, and one end of said auxiliary erecting device is hinged with vehicle frame 2 through spring lower hinge seat 601, said The other end of the auxiliary erecting device is a movable end, and the movable end is covered with a spring upper hinge seat 602, and the spring upper hinge seat 602 is hinged with the erecting arm 3, and the locking mechanism is installed on the erecting arm 3 Above, the locking mechanism is used to fixedly connect the vertical arm 3 and the launching platform 4 .

[0024] Such as Figure 8 and Figure 9 As shown, the locking mechanism includes a locking cylinder 801, a locking pin 802 and a socket 804, the locking cylinder...

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Abstract

The invention provides a launching vehicle with a locking mechanism and an auxiliary erecting device. The launching vehicle comprises the locking mechanism and the auxiliary erecting device, wherein one end of the auxiliary erecting device is hinged to a frame through a spring lower hinged support; the other end of the auxiliary erecting device is a movable end; the movable end is sleeved with a spring upper hinged support; the spring upper hinged support is hinged to an erecting arm; the locking mechanism is installed on the erecting arm; and the locking mechanism is used for fixedly connecting the erecting arm and a launching pad. The launching vehicle solves the problems that the mode of manually assembling and disassembling the erecting arm and the launching pad is inconvenient to operate, the connecting precision is reduced, the requirement for structural rigidity in the rocket erecting process is high, and the cost is high, the process of manually connecting the launching pad and the erecting arm is replaced with the locking mechanism, the operation is convenient, the connecting precision is guaranteed, and the cost of each component in the rocket erecting process is reduced by utilizing the auxiliary erecting device.

Description

technical field [0001] The invention relates to the technical field of rocket launching devices, in particular to a launching vehicle with a locking mechanism and an auxiliary erecting device. Background technique [0002] The launch pad is used to support and fix the carrier, adjust the verticality, aim at the azimuth, install the fire pipeline, ignition line and ignition launch, etc. When launching, the gas flow passes through the flame exhaust hole in the center of the launching platform, and is discharged to both sides through the diversion groove under the platform. There are two types of launch pads: fixed and movable. The main difference between the two is that the fixed launch pad is directly fixed on the launch station and cannot be moved; the movable launch pad can move freely between the technical area and the launch area. The mobile launch pad can be designed to travel on roads, or it can be designed to travel on railroad tracks. [0003] Existing rocket launch...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 邢盟陈超舒畅马超
Owner BEIJING ONESPACE TECH CO LTD
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