一种座舱操纵试验件在铁鸟试验台上的安装定位方法

By adopting a full-scale coordinate system design and modular connection on the iron bird test bench, combined with laser tracker positioning and three-way connection lugs, the problem of inconsistent installation of cockpit control test components was solved, achieving high-precision installation and functional assurance.

CN117719695BActive Publication Date: 2026-07-17CHINA SPECIAL TYPE FLIER RES INST

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
CHINA SPECIAL TYPE FLIER RES INST
Filing Date
2023-12-29
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

In the existing technology, there is a lack of a unified and reasonable scheme for the installation and positioning of cockpit control test components on iron bird test benches, resulting in different installation methods that are difficult to meet high precision requirements.

Method used

Using the whole-aircraft coordinate system as a reference, the iron bird nose support frame and simulated cockpit support platform are designed. Precise positioning is achieved through connecting flanges and laser trackers, and fixed connection is achieved by combining modular design and three-way connecting lugs to ensure installation accuracy.

Benefits of technology

It achieved precise positioning of the cockpit control test component on the iron bird test stand, ensuring installation accuracy and functional performance, reducing design docking errors and omissions, and shortening the test stand construction cycle.

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Abstract

本发明公开了一种座舱操纵试验件在铁鸟试验台上的安装定位方法,包括:设计地面综合试验台,确定以飞机全机坐标系为基准,对铁鸟机头台架、模拟座舱支撑平台和座舱操纵试验件过渡件的结构和安装位置分别进行设计;在座舱操纵试验件过渡件与平台结构框架之间设计有专用连接组件;实施对座舱操纵试验件在该地面综合试验台上的定位安装,包括:以飞机坐标原点O为绝对原点,建立全机坐标系,依次对铁鸟机头台架、模拟座舱支撑平台和座舱操纵试验件过渡件进行安装。本发明的技术方案解决了由于各类地面综合试验台使用的试验件比例和结构组成不同,且安装方式各不相同,从而导致尚且没有形成统一且合理的安装定位方案的问题。
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