飞机油门台操纵特性与飞行控制系统匹配分析

Analysis of Match of Aircraft Throttle Control Characteristics and Flight Control System

摘要

飞机油门台作为飞行控制系统的重要组成部分，其操纵特性直接影响飞行性能和飞行安全。本文对飞机油门台的基本构造、功能以及操纵特性进行了详细分析，并探讨了影响操纵特性的因素，如环境条件、机械结构与控制精度等。同时，文章分析了油门台与飞行控制系统之间的匹配要求，包括协调性、响应匹配度以及飞行状态变化对匹配的影响。通过常用的匹配分析方法，如理论模型、仿真分析与实验验证，评估了油门台与飞行控制系统的匹配程度。最后，提出了优化油门台操纵特性与飞行控制系统匹配的策略，尤其关注未来技术在优化过程中的潜力与挑战。本文的研究为飞行控制系统设计与优化提供了理论依据与实践指导。

Abstract

As an essential component of the flight control system,the throttle control unit’s operating characteristics directly impact flight performance and safety.This paper provides a detailed analysis of the basic structure,function,and operating characteristics of the throttle control unit,and explores factors influencing these characteristics,such as environmental conditions,mechanical structure,and control precision.Additionally,the paper discusses the matching requirements between the throttle control unit and the flight control system,including coordination,response matching,and the effects of flight state variations on the match.Using common matching analysis methods,such as theoretical models,simulation analysis,and experimental validation,the degree of match between the throttle control unit and the flight control system is assessed.Finally,strategies for optimizing the throttle control unit’s operating characteristics and its match with the flight control system are proposed,with a particular focus on the potential and challenges of future technologies in the optimization process.This research provides theoretical foundations and practical guidance for the design and optimization of flight control systems.

关键词

飞机油门台 / 操纵特性 / 飞行控制系统 / 匹配分析 / 优化策略

Key words

throttle control unit / operating characteristics / flight control system / matching analysis / optimization strategies

参考文献

[1] 娄本山. 基于429总线的飞机油门操纵杆自动控制系统研制[D].导师:李霞. 哈尔滨工程大学, 2020.

[2] 丁忠伟. 某型直升机发动机油门操纵调整和故障排除[J]. 航空维修与工程, 2019,(10):100-102.

[3] 台春雷, 李丹丹, 韩梅. 某型飞机发动机操纵力控制工艺研究[J]. 飞机设计, 2017, 37(02):64-67.

[4] 王晓成, 乔茂, 张勇, 毛晓珺, 张铁军, 贺轶斐. 上海航空机械有限公司, 陆军装备部驻上海地区航空军事代表室. 一种直升机机械备份油门操纵技术[Z]. 项目立项编号:XCSL761SHJ12001A.鉴定单位:陆航驻上海地区军事代表室.鉴定日期:2013-09-11.

[5] 李应涛. 舰载飞机的进场动力补偿和自动油门控制系统设计[D].导师:徐利梅. 电子科技大学, 2007.