Measuring tool and method for centroid position of missile-borne telemetry cabin

A technology for measuring tooling and measuring methods, which is applied in the field of telemetry cabins on bombs, to achieve the effects of saving manpower and material resources, simple measuring methods, and easy assembly

Inactive Publication Date: 2018-11-13
SHANGHAI SPACEFLIGHT ELECTRONICS & COMM EQUIP RES INST
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] The purpose of the present invention is to provide a measuring tool and measuring method for the position of the center of mass of the telemetry cabin on the bomb, so as to solve the problem that there is no method in the prior art that has high measurement accuracy and simple operation, and is also applicable to telemetry cabins of various types and specifications. Technical issues with products etc.

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  • Measuring tool and method for centroid position of missile-borne telemetry cabin
  • Measuring tool and method for centroid position of missile-borne telemetry cabin
  • Measuring tool and method for centroid position of missile-borne telemetry cabin

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Embodiment Construction

[0056] The following will combine Figure 1 to Figure 4 The measuring tool and measuring method for the position of the center of mass of the telemetry cabin on the bomb provided by the present invention are described in detail. This embodiment is implemented on the premise of the technical solution of the present invention, and the detailed implementation and specific operation process are given. However, The protection scope of the present invention is not limited to the following embodiments, those skilled in the art can modify and embellish it within the scope of not changing the spirit and content of the present invention.

[0057] Please refer to figure 1 , a measuring tool for the position of the center of mass of the telemetry cabin, comprising a front bracket 1 and a rear bracket 2 for placing the telemetry cabin under test, the front bracket 1 is located at the front of the tool, and the rear bracket 2 is located at the rear of the tool, the front bracket 1 and the ...

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Abstract

The invention relates to a measuring tool and method for a centroid position of a missile-borne telemetry cabin. The tool comprises a front bracket and a rear bracket which allow the to-be-measured telemetry cabin to be placed and are connected by two cross beams to define an enclosure frame, wherein the front end surface of the front bracket is fixedly connected with a stop bar through at least one pillar. The tool is simple in structure, high in strength, easy to process, assemble and carry, and applicable to telemetry cabin products of various models and specifications. The measuring methodfor the centroid position of the telemetry cabin by the tool is simple and accurate, simple to operate and relatively high in measurement accuracy, various manpower and material resources in the centroid measurement process can be reduced, and measurement efficiency and accuracy are improved.

Description

technical field [0001] The invention relates to a bomb-on telemetry cabin, in particular to a measuring tool and a measuring method for the centroid position of the bomb-on telemetry cabin. Background technique [0002] At present, the measurement of the center of mass of the telemetry cabin on the missile mainly adopts the method of suspension method measurement, the method of dynamic balancer and special tooling measurement, and the method of "two-point force measurement to determine the longitudinal center of mass": [0003] The suspension method is simple to measure, but the accuracy is poor, and it is not suitable for cabins with large masses; [0004] The method of measuring the dynamic balance instrument with special tooling has high measurement accuracy, but the equipment is overkill, and the operation requirements are high, the measurement time is long, and the tooling needs to be redesigned every time for cabins of different sizes, which is time-consuming and labor...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01B21/00
CPCG01B21/00
Inventor 丁帅吴晟耿盛韦鲍中华陈蔚涵
Owner SHANGHAI SPACEFLIGHT ELECTRONICS & COMM EQUIP RES INST
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