AGMA 06FTM10-2006
直升机设施用双螺旋混合行星齿轮传动高接触比超安全高传动比的制造、装配和试验

Fabrication, Assembly and Test of a High Ratio, Ultra Safe, High Contact Ratio, Double Helical Planetary Transmission for Helicopter Applications


 

 

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标准号
AGMA 06FTM10-2006
发布日期
2006年
实施日期
废止日期
中国标准分类号
V22
发布单位
US-AGMA
适用范围
An ultra-safe, high ratio planetary transmission, for application as a helicopter main rotor drive, has been designed, fabricated and tested under the sponsorship of NRTC-RITA. The anticipated improvements offered by this new planetary transmission are reduced weight, reduced transmitted noise and improved fail-safety. This paper discusses the fabrication assembly and test results for the subject planetary transmission. The design and analysis of this transmission system have been discussed in a previous paper presented at the AGMA FTM in 2004. The ultra-safe, high ratio planetary transmission design utilizes a compound planetary configuration with a 17.5:1 reduction ratio which would replace a conventional two stage simple planetary transmission. The new design uses ultra-safe principles such as split-torque paths and high combined contact ratio gearing. Double helical gears in the planet/ ring meshes balance axial tooth forces so that axial bearing reactions are not required. The spur gear sun/planet meshes are staggered to achieve a compact spatial arrangement. Fabrication and assembly of the components for this transmission are complicated by their configuration. The grinding process for the helical gears must use small diameter wheels due to the proximity of the adjacent helix, since most the gears in this configuration are integrated designs. Assembly procedures also require special consideration because of the integrated design and helical gears. Test results are presented to support the goals of this project, including, concept verification, weight reduction, noise reduction and determination of the operating characteristics of the test transmission.




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