A loading positioning locking device
A positioning locking and loading technology, which is applied to offensive equipment, ammunition supply, weapon accessories, etc., can solve the problems of long time required, unfavorable weapon automation, and reduced personnel utilization, and achieves the effect of easy manufacture and simple structure
Active Publication Date: 2021-06-11
NANJING UNIV OF SCI & TECH
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Problems solved by technology
The disadvantage of this loading technology is that it requires manual assistance in the loading process, which increases the complexity of ammunition loading and reduces the utilization rate of personnel; the 122mm rocket launcher "Cyclone" developed by Russia with box-type loading technology adopts the loading method of ammunition loading vehicles, The characteristic is that the ammunition vehicle needs to complete the tasks of unloading and loading. Compared with the overall hoisting, the disadvantage is that it takes longer and the ammunition loading is more complicated, which is not conducive to the automation of weapons.
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[0016] The external equipment involved in the present invention refers to barrel-packed devices for launching aircraft such as missiles and unmanned aerial vehicles.
[0017] combine figure 1 , a loading positioning locking device, including a frame, a first pin fixing seat 1, a second pin fixing seat 3, two wedge blocks 2, a rotating rod 4, a first hydraulic cylinder 5, a first hydraulic cylinder hinge Seat 6, two pin shaft guide seats 7, two positioning shafts with shoulders 8, second hydraulic cylinder 10, second hydraulic cylinder hinge support 9, two parallelogram linkages 11, two wedge clamping Block 12, two sliders 13.
[0018] The first pin fixing base 1, the second pin fixing base 3 and the two wedge blocks 2 are fixed on the outer wall of the external equipment. The first pin fixing seat 1 and the second pin fixing seat 3 are fixed on the outer wall of the external equipment according to image 3 The upper and lower sides of the direction shown are misplaced, that...
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The invention provides a loading, positioning and locking device, which includes a frame, two pin shaft fixing seats, two wedge blocks, a rotating rod, two sliding blocks, two positioning shafts, and two parallelogram linkage mechanisms; The pin shaft fixing seat is fixed on the outer wall of the external equipment, and the two wedge blocks are fixed on the outer wall of the external equipment. The active rod is installed on the frame through the rotating shaft and chute is provided at both ends. The active rod and the telescopic rod of the hydraulic cylinder Flexible connection, each slider is set in the corresponding chute, each positioning shaft is fixedly connected with the corresponding slider, the hydraulic cylinder drives the active rod to rotate and drives the slider to slide in the chute, and the slider drives the corresponding positioning shaft to do The linear motion extends into or breaks away from the corresponding pin fixing seat, and the hinge point of each parallelogram linkage mechanism is set on the frame to rotate. Each parallelogram linkage mechanism is flexibly connected with the corresponding hydraulic cylinder telescopic rod, and the parallelogram linkage A wedge-shaped clamping block matched with the wedge-shaped block is arranged on the rod mechanism.
Description
technical field [0001] The invention relates to a filling device technology, in particular to a filling positioning and locking device. Background technique [0002] Today's rocket launchers mostly use the overall hoisting and ammunition loading vehicle loading methods, while the more advanced rocket launchers mostly use the overall hoisting method. For example, a multiple rocket launcher M270 jointly developed by the United States, Britain, France, and Germany adopts the loading method of integral hoisting. It takes about 5 minutes and requires 1 to 3 people to assist in the filling process. The disadvantage of this loading technology is that it requires manual assistance in the loading process, which increases the complexity of ammunition loading and reduces the utilization rate of personnel; the 122mm rocket launcher "Cyclone" developed by Russia with box-type loading technology adopts the loading method of ammunition loading vehicles, The characteristic is that the amm...
Claims
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IPC IPC(8): F41A9/38
CPCF41A9/38
Inventor 蒯腾飞任杰乐贵高王鑫唐亮赵昌方邢成龙
Owner NANJING UNIV OF SCI & TECH