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Integration of the RTM322 FADEC into the WAH-64 Apache

机译:将RTM322 FADEC集成到WAH-64 Apache中

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The Rolls-Royce Turbomeca RTM322 engine was selected to power the WAH-64 Apache Attack Helicopter, for the Army Air Corps, by the UK MoD in 1996. Integration of this new installation was to be conducted remotely, at the Boeing facility in Mesa, Arizona. It was recognised, from the outset, that engine control system integration with the rotor drive-train would be the high risk item in the overall programme. By their nature, helicopters have an established reputation for challenging dynamic system characteristics and the Apache is certainly no different. On top of this, the declared two year time-scale of this flagship 'Smart Procurement' programme was aggressive, to say the least. Despite extensive use of sophisticated computer simulations, it was anticipated that engine control optimisation would be necessary during the flight test programme. The traditional method of revising control laws was seen to be too time consuming so a new process, utilising the on-line development capability of the RTM322 control software, was defined. This was further exploited by building flexibility into the control algorithms so that desired functional options could be set up via a pc link. Gaining flight clearance for this process was a major achievement. The flight programme commenced in 1998 and, as anticipated, several control integration issues were soon identified. Each was addressed by implementing incremental software solutions using the defined process. This method enabled the baseline aircraft flight programme to progress without interruption. During 20 months of flight testing we used this software revision process 12 times, resulting in the delivery of an exemplary standard of engine control for the WAH-64 Apache, on time, in June 2000.
机译:罗尔斯·罗伊斯公司透博梅卡发动机RTM322在1996年整合入选功率WAH-64阿帕奇攻击直升机,陆军航空队,由英国国防部这种新安装的是要在梅萨波音设施远程进行,亚利桑那。从一开始就被认识到,发动机控制系统与转子传动系的集成将是整个程序中的高风险项目。通过他们的性质,直升机在挑战动态系统特征方面具有良好的声誉,并且Apache肯定没有任何不同。在此之上,这旗舰智能采购计划的宣布两年的时间范围是侵略性的。尽管使用复杂的计算机模拟广泛使用,但预计在飞行测试程序期间将需要发动机控制优化。传统的修订控制法律方法被认为是使用RTM322控制软件的在线开发能力的新过程的耗时。通过在控制算法中构建灵活性,进一步利用这一点,以便通过PC链路建立所需的功能选项。获得这个过程的飞行许可是一项重大成就。该航班计划于1998年开始,预计,几次控制一体化问题很快就会发现。每个都是通过使用定义的进程实现增量软件解决方案来解决的。这种方法使基线飞行计划的进展情况不会中断。在20个月的飞行测试期间,我们使用该软件修订过程12次,导致2000年6月,按时交付WAH-64 Apache的示例性发动机控制标准。

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