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Device for motion simulation and load measurement of weapon cabin door and method

A technology of load measurement and motion simulation, applied in the direction of measuring device, measuring fluid pressure, measuring fluid pressure through mechanical components, etc., can solve the problems of low measurement accuracy and poor consistency

Inactive Publication Date: 2013-05-15
AVIC SHENYANG AERODYNAMICS RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1. Low measurement accuracy;
[0004] 2. Only a few fixed angles can be used to measure the aerodynamic force;
[0005] 3. The consistency between the balance calibration state and the balance experiment state is poor

Method used

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  • Device for motion simulation and load measurement of weapon cabin door and method
  • Device for motion simulation and load measurement of weapon cabin door and method

Examples

Experimental program
Comparison scheme
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Embodiment Construction

[0022] A weapon cabin door motion simulation and load measuring device, comprising a simulated hull 6, a weapon cabin door 1, a U-shaped bracket 5, a dynamic balance 7, a motor 2 and a transmission gear set 3; it is characterized in that:

[0023] The weapon compartment door 1, the transmission gear set 3, and the motor 2 are installed on the set position of the U-shaped bracket 5; The bearings in the seat 10 and the second shaft seat 11 are supported; the output shaft 13 of the transmission gear set 3 is connected with the rear door shaft 9 through a coupling 14, and the input shaft 15 of the transmission gear set 3 is connected with the motor 2 through a coupling 12. The output shaft 4 is connected; the U-shaped support 5 is fixed on the dynamic balance 7; the integrated weapon cabin door 1, the transmission gear set 3, the motor 2, the U-shaped support 5 and the dynamic balance 7 are fixed in the simulated hull 6 to form a Complete door motion simulation and load measuremen...

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Abstract

The invention discloses a device for motion simulation and load measurement of a weapon cabin door. The device comprises a simulation boat body, the weapon cabin door, a U-shaped support frame, a movable balance, a motor and a transmission gear group. The weapon cabin door, the transmission gear group and the motor are respectively installed at a setting position of the U-shaped support frame, a front pivot and a rear pivot of the weapon cabin door are respectively supported by bearings in a first axle base and a second axle base in the U-shaped support frame, an output shaft of the transmission gear group is connected with the rear pivot through a coupler, and an input shaft of the transmission gear group is connected with an output shaft of the motor through a coupler. The U-shaped support frame is fixed on the movable balance, the weapon cabin door, the transmission gear group, the motor, and the U-shaped support and the movable balance are integrated and fixed in the simulation boat body so that the intact cabin door motion simulation and load measuring device is formed. The cabin door can be opened in a serial of fixed angles, and the device can measure instant aerodynamic force in the process that the cabin door is opened / closed with certain speed dynamically, and analytic investigation of cabin door dynamic aerodynamic characteristics is performed.

Description

technical field [0001] The invention relates to a device and method for motion simulation and load measurement of a weapon cabin door, in particular to a device and method for simulating the opening / closing process of an aircraft weapon cabin door and measuring the aerodynamic load acting on the cabin door. Background technique [0002] At present, the aerodynamic load of the hatch door of the weapon compartment is generally realized by changing the angle block. The method similar to the hinge moment measurement method is used to measure the aerodynamic force of the hatch door with a plate strain balance. The disadvantages of this method are: [0003] 1. Low measurement accuracy; [0004] 2. Only a few fixed angles can be used to measure the aerodynamic force; [0005] 3. The consistency between the balance calibration state and the balance experiment state is poor. Contents of the invention [0006] The purpose of the present invention is to provide a weapon cabin door ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01L7/00
Inventor 冯强张洋崔晓春李玲
Owner AVIC SHENYANG AERODYNAMICS RES INST
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