Invention Grant
- Patent Title: Multi-path rotary wing aircraft gearbox
- Patent Title (中): 多路旋翼飞机变速箱
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Application No.: US12295737Application Date: 2006-04-04
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Publication No.: US07918146B2Publication Date: 2011-04-05
- Inventor: Yuriy Gmirya
- Applicant: Yuriy Gmirya
- Applicant Address: US CT Stratford
- Assignee: Sikorsky Aircraft Corporation
- Current Assignee: Sikorsky Aircraft Corporation
- Current Assignee Address: US CT Stratford
- Agency: Carlson Gaskey & Olds PC
- International Application: PCT/US2006/012392 WO 20060404
- International Announcement: WO2007/114817 WO 20071011
- Main IPC: F16H37/06
- IPC: F16H37/06

Abstract:
A multi-path split torque gearbox system provides a multiple of three stage torque split power gear trains modules that each transmits torque from a high-speed engine to a main rotor shaft (36). The first stage bevel gear arrangement (30,32) provides a compact packaging arrangement that facilitates various engine mounting locations in all axes. At the second stage, quill shaft assemblies (40) provide equal load balance. At the third stage, each quill shaft assembly includes a multiple of pinion gears (48) in meshing engagement with the final output gear (28). Each torque split modules transfer the power from the high speed input shaft into a multiple of meshing engagements with the final output gear to provide significant torque transfer desired in a single rotor heavy lift rotary wing aircraft embodiment within a compact housing package.
Public/Granted literature
- US20090277299A1 MULTI-PATH ROTARY WING AIRCRAFT GEARBOX Public/Granted day:2009-11-12
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