The comprehensive installation and adjustment method for the airplane system pipeline comprises the following steps: firstly, carrying out model construction on a space in which the system pipeline is positioned by adopting an airplane narrow space environment model configuration method for installation and adjustment of the system pipeline; before the system pipeline is formally installed and fixed, a guide pipe is grabbed from a to-be-installed area and transported to an onboard installation area through an airplane system pipeline automatic grabbing and transporting method; before the system pipeline is formally installed and fixed, the pipe type calibration is continued according to the actual situation by adopting a secondary bending correction method for the system pipeline of the airplane; when the installation quality of the system pipeline is guaranteed and no liquid or gas leakage is determined, the dynamic gap of the system pipeline is detected by adopting an aircraft system pipeline dynamic gap measuring method; when the system pipeline is in a normal working state, the working temperature of the pipeline is controlled and adjusted in real time by adopting an aircraft system pipeline working temperature control method; a system pipeline is provided with an emergency release system besides normal work, and when the system is debugged, the harmful oil gas is treated by adopting a control method for the harmful oil gas of the airplane emergency release system.

    飞机系统管路综合装调方法包括:系统管路的装调先采用飞机狭小空间环境模型构型方法对系统管路所处空间进行模型构建;系统管路正式装机固定前,采用飞机系统管路自动抓取及运输方法将导管从待安装区域抓取并运输至机上安装区域;系统管路正式装机固定前,采用飞机系统管路二次弯曲校形方法,根据实际情况继续管型校准;在保证系统管路安装质量且确定无液气泄漏时,采用飞机系统管路动态间隙测量方法对系统管路动态间隙进行检测;系统管路正常进行工作状态下,采用飞机系统管路工作温度控制方法对管路工作温度进行实时控制与调节;系统管路除正常工作外,设置应急放系统,进行系统调试时,采用飞机应急放系统有害油气控制方法对有害油气进行处理。


    Access

    Download


    Export, share and cite



    Title :

    Comprehensive assembling and adjusting method for aircraft system pipeline


    Additional title:

    飞机系统管路综合装调方法


    Contributors:
    LI ZHE (author) / LIU YUNAN (author) / LIU HAITAO (author) / GUO LEI (author) / JIANG CHUANNAN (author) / LI WENLONG (author)

    Publication date :

    2024-02-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B01D SEPARATION , Trennen / G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G06V



    Aircraft force comprehensive adjusting device

    CUI HAIDONG / MA LI / XU ZHE et al. | European Patent Office | 2025

    Free access

    Assembling posture adjusting platform for aircraft landing gear

    WANG DONG / DANG XING / XU WENLI et al. | European Patent Office | 2024

    Free access

    Aircraft part assembling equipment with universal adjusting function

    ZHAO PING / GUO XINGDONG | European Patent Office | 2020

    Free access

    Support method for assembling, adjusting and positioning aircraft body component

    MAO XINYU / GE XIAODONG / HAN JIAWEI | European Patent Office | 2020

    Free access

    Multi-angle free adjusting and assembling device for aircraft wing

    HE HUAIBIN | European Patent Office | 2021

    Free access