SAE AIR 4869A-2009
封闭式涡轮风扇/涡轮喷射发动机测试腔的设计研究
Design Considerations for Enclosed Turbofan/Turbojet Engine Test Cells
SAE AIR 4869A-2009 发布历史
This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in upgrading their existing or acquiring new test cell facilities. There are several purposes served by this document: a. to provide guidelines for the design of state-of-the-art ground-level enclosed test facilities for turbofan and turbojet engine testing applications; b. to address the major test cell/engine aerodynamic and acoustic characteristics which can influence the operation of a gas turbine engine and its performance stability in a test cell; and c. to consider acoustic environmental impact and methods to control it.
SAE AIR 4869A-2009由美国机动车工程师协会 US-SAE 发布于 2009-05-13。
SAE AIR 4869A-2009 在中国标准分类中归属于: V30 发动机总体，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 AIR 4869A-2009 发布之时，引用了标准
- ISO 7196-1995 声学 次声测量用的频率计权特性
- SAE AIR 5306-2000 气体涡轮机试验室的进口空气流斜面
SAE AIR 4869A-2009的历代版本如下：
- 2009年05月13日 SAE AIR 4869A-2009 封闭式涡轮风扇/涡轮喷射发动机测试腔的设计研究
SAE AIR 4869A-2009 封闭式涡轮风扇/涡轮喷射发动机测试腔的设计研究 由 SAE AIR 4869-1995 变更而来。
- 标准号
- SAE AIR 4869A-2009
- 发布日期
- 2009年05月13日
- 实施日期
- 废止日期
- 无
- 中国标准分类号
- V30
- 国际标准分类号
- 49.050
- 发布单位
- US-SAE
- 引用标准
- ISO 7196-1995 SAE AIR 1419-1983 SAE AIR 5306-2000 SAE ARP 741 SAE ARP 1420-1978 AIAA 82-1239 AIAA 82-1272 AIAA 84-0594 AIAA 85-0382 AIAA 86-1732 AIAA 93-2542 CEAS/AIAA 95-128
- 被代替标准
- SAE AIR 4869-1995
- 适用范围
- This SAE Aerospace Information Report (AIR) has been written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in upgrading their existing or acquiring new test cell facilities. There are several purposes served by this document: a. to provide guidelines for the design of state-of-the-art ground-level enclosed test facilities for turbofan and turbojet engine testing applications; b. to address the major test cell/engine aerodynamic and acoustic characteristics which can influence the operation of a gas turbine engine and its performance stability in a test cell; and c. to consider acoustic environmental impact and methods to control it.