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。
Comprehensive assembling and adjusting method for aircraft system pipeline
飞机系统管路综合装调方法
2024-02-02
Patent
Elektronische Ressource
Chinesisch
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 part assembling equipment with universal adjusting function
Europäisches Patentamt | 2020
|Support method for assembling, adjusting and positioning aircraft body component
Europäisches Patentamt | 2020
|Multi-angle free adjusting and assembling device for aircraft wing
Europäisches Patentamt | 2021
|Adjustable supporting device of small aircraft assembling tool and pose adjusting method
Europäisches Patentamt | 2020
|System for achieving intelligent aircraft assembling and assembling method
Europäisches Patentamt | 2020
|