SAE ARP 704A-1997
直升机发动机旋翼系统兼容性
Helicopter Engine-Rotor System Compatibility
SAE ARP 704A-1997 发布历史
This SAE Aerospace Recommended Practice (ARP) recommends a methodology to be used for the design, analysis and test evaluation of modern helicopter gas turbine propulsion system stability and transient response characteristics. This methodology utilizes the computational power of modern digital computers to more thoroughly analyze, simulate and bench-test the helicopter engine/rotor system speed control loop over the flight envelope. This up-front work results in significantly less effort expanded during flight test and delivers a more effective system into service. The methodology presented herein is recommended for modern digital electronic propulsion control systems and also for traditional analog and hydromechanical systems.
SAE ARP 704A-1997由美国机动车工程师协会 US-SAE 发布于 1997-05-01。
SAE ARP 704A-1997 在中国标准分类中归属于: V31 发动机辅助系统及其附件，在国际标准分类中归属于: 49.050 航空航天发动机和推进系统。
SAE ARP 704A-1997的历代版本如下：
- 1997年05月01日 SAE ARP 704A-1997 直升机发动机旋翼系统兼容性
- 适用范围
- This SAE Aerospace Recommended Practice (ARP) recommends a methodology to be used for the design, analysis and test evaluation of modern helicopter gas turbine propulsion system stability and transient response characteristics. This methodology utilizes the computational power of modern digital computers to more thoroughly analyze, simulate and bench-test the helicopter engine/rotor system speed control loop over the flight envelope. This up-front work results in significantly less effort expanded during flight test and delivers a more effective system into service. The methodology presented herein is recommended for modern digital electronic propulsion control systems and also for traditional analog and hydromechanical systems.