Rocket transportation device and launching device
A technology for transport devices and rockets, which is applied to rocket launchers, offensive equipment, weapon types, etc., can solve problems such as the inability to meet low-cost, high-reliability and rapid launch, large investment in fixed facilities, and inability to flexibly adapt to launch site conditions.
Active Publication Date: 2022-02-01
北京中科宇航技术有限公司
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Problems solved by technology
Such facilities cannot meet the needs of low-cost, high-reliability and rapid launch of commercial spaceflight, and the investment in fixed facilities is large, which cannot flexibly adapt to the launch site conditions of different space launch sites
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[0062] Embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.
[0063] Such as figure 1 , figure 2 , image 3 and Figure 4 As shown, the rocket transportation device provided by the embodiment of the present application includes a base frame 100, a vertical frame 200, a plurality of load equalizing devices 300, two upper clamps 400, two lower clamps 500, a support ring 600, and two locking arrow pins. 30 and 40 for two lock arrow sets. Wherein, the first end of the erecting frame 200 is hinged with the first end of the base frame 100; the erecting frame 200 includes a plurality of cr...
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The present application discloses a rocket transportation device and a launching device, wherein the rocket transportation device includes an underframe, an erection frame, a plurality of load equalizing devices, two upper clamps, two lower clamps, a support ring, two locking arrow pins and Two lock arrow sets. The load equalizing device is used to carry the main body of the rocket; the two upper clamps are used to hold the upper part of the rocket; the support ring is detachably fixed on the bottom end of the rocket, and the two lower clamps are respectively fixed on the two sides of the vertical frame near the first end. side, the two locking arrow pins are fixed on both sides of the support ring, and the two locking arrow sleeves are respectively set on the two lower clamps, or the two locking arrow sleeves are fixed on both sides of the support ring, and the two locking arrow pins are respectively set On both lower clamps; arrow lock pins inserted into lock holsters to lock rockets. In this application, the rocket is hoisted into the arc-shaped groove of the load equalizing device, and then the rocket is fixed by the upper and lower clamps. The structure of the entire rocket transportation device is simple, which greatly reduces the workload of workers.
Description
technical field [0001] The invention relates to the field of rocket transportation and launching, in particular to a rocket transportation device and a launching device. Background technique [0002] With the continuous development of aerospace technology, rockets, as the core part of aerospace tools, have also been greatly developed. At present, all rockets need to be disassembled and transported to the launch site, and can only be transferred to the launch site for launch after the general assembly and testing of the technical workshop at the launch site. Can be ignited to launch. Due to the large weight and volume of the rocket after final assembly, the current industry generally adopts the method of vertical final assembly in the technical workshop, and then vertical transfer to the launching point of the launch site. This method requires a relatively high technical workshop, and requires huge transfer equipment to complete reloading and pre-launch filling, leveling, a...
Claims
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IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 王永刚王寿军滕瑶杨毅强刘金程胡小伟李涛周龙胡月梅
Owner 北京中科宇航技术有限公司