Multi-airplane-type airplane weight gravity center automatic measuring device

A technology for measuring devices and aircraft, which is applied in the testing of measuring devices, machine/structural components, static/dynamic balance testing, etc. It can solve the problem that data accuracy, efficiency, and versatility cannot meet development needs, and the skills of testers are relatively high. High, can not eliminate problems such as lateral force, to achieve the effect of easy operation, not easy to tip over, and easy to adjust

A technology for measuring devices and aircraft, which is applied in the testing of measuring devices, machine/structural components, static/dynamic balance testing, etc. It can solve the problem that data accuracy, efficiency, and versatility cannot meet development needs, and the skills of testers are relatively high. High, can not eliminate problems such as lateral force, to achieve the effect of easy operation, not easy to tip over, and easy to adjust

CN112304408AActive Publication Date: 2021-02-02贵州航天特种车有限责任公司

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  • Multi-airplane-type airplane weight gravity center automatic measuring device
  • Multi-airplane-type airplane weight gravity center automatic measuring device
  • Multi-airplane-type airplane weight gravity center automatic measuring device

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0028] like Figure 1 to Figure 7 As shown, a multi-type aircraft weight center of gravity automatic measurement device includes a front servo lift leveling device 1, an inclination sensor 2, a tool cart 3, a rear servo lift leveling device 4 and a computer 5, and the inclination sensor 2 is installed on On the aircraft fuselage pitch reference plane, an electric control cabinet is built in the tool trolley 3, measurement management software is installed on the computer 5, the computer 5 is electrically connected to the electric control cabinet, the front servo lifting leveling device 1 and the rear servo lifting leveling device 1 The leveling devices 4 are all provided with a signal converter 6, and the inclination sensor 2, the signal converter 6, and the electric control cabinet are electrically connected in sequence. The attitude state of the aircraft can be obtained directly through the inclination sensor 2. Compared with the prior art, the aircraft attitude is obtained b...

Embodiment 2

[0039] like Figure 8 As shown, on the basis of the structure of Embodiment 1, the structure of the front servo lifting and leveling device 1 has the following changes:

[0040] In this embodiment, an anti-lateral force mechanism 11 is also provided between the bracket 7 and the load cell 8 of the front servo lifting and leveling device 1, and when lifting the top socket of the aircraft head, the anti-rolling force is improved. At the same time, it has a certain automatic alignment function, which reduces the requirements for the tester's operating skills, makes the operation easier and safer, and improves the accuracy and efficiency of the test.

[0041] When the multi-type aircraft weight and center of gravity automatic measurement device provided by this application is working, the front servo lift leveling device supports the front top socket of the aircraft head, the rear servo lift leveling device supports the rear reinforcement frame of the aircraft fuselage, and the in...

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Abstract

The invention provides a multi-airplane-type airplane weight gravity center automatic measuring device which comprises a front servo lifting leveling device, an inclination angle sensor, a tool car and a rear servo lifting leveling device, wherein the inclination angle sensor is installed on an airplane body pitching reference plane, an electric control cabinet is arranged in the tool car, measurement management software is installed in a computer, the computer is electrically connected with the electric control cabinet, and the front servo lifting leveling device and the rear servo lifting leveling device are each provided with a signal converter and a lateral force resisting mechanism; the inclination angle sensor, the signal converters and the electric control cabinet are electrically connected in sequence. According to the multi-airplane-type airplane weight gravity center automatic measuring device, by arranging the inclination angle sensor, the attitude state of the airplane canbe directly obtained, response is faster, and the safety of the airplane during measurement is improved; the lateral force resisting mechanism is arranged; when the aircraft is lifted, the automatic adjustment function of the horizontal position is realized, the operation is easier and safer, and the test precision and efficiency are improved.

Description

technical field [0001] The invention belongs to the technical field of aircraft testing, and in particular relates to an automatic measurement device for weight and center of gravity of multi-type aircraft. Background technique [0002] The weight and center of gravity of the aircraft is an important parameter in aircraft manufacturing. It is necessary to measure the weight and center of gravity of the aircraft during the process of research and trial production of the aircraft, factory inspection, flight test preparation, overhaul and delivery. As the flight speed of medium-heavy aircraft turbojet continues to increase and the flight attitude continues to become more and more complex, higher and higher technical requirements are put forward for the measurement accuracy of the center of gravity of the aircraft, which requires a set of special measuring devices for measurement, such as the publication number is CN105444855A The Chinese patent provided a device for measuring a...

Claims

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Application Information

Patent Timeline
02 Feb 2021
Publication
CN112304408A
IPC
G01G19/07; G01M1/12
CPC
G01G19/07; G01M1/125
Inventors
尹华; 葛鹏