Invention Grant
- Patent Title: Torque split gearbox for rotary wing aircraft
- Patent Title (中): 旋翼飞机用扭矩分动齿轮箱
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Application No.: US14017674Application Date: 2013-09-04
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Publication No.: US09278760B2Publication Date: 2016-03-08
- Inventor: Todd A. Garcia
- Applicant: Sikorsky Aircraft Corporation
- Applicant Address: US CT Stratford
- Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee: SIKORSKY AIRCRAFT CORPORATION
- Current Assignee Address: US CT Stratford
- Agency: Cantor Colburn LLP
- Main IPC: B64D35/06
- IPC: B64D35/06 ; B64C27/10 ; B64C27/12

Abstract:
A gearbox system for a dual coaxial counter rotating rotor assembly includes an input shaft to input a first torque into the gearbox system and a transfer shaft operably connected to the input shaft to transfer the first torque therethrough. Two gear sets are operably connected to the transfer shaft. Each gear set includes a first output gear to transfer a second torque acting in a first direction to a first rotor of a rotor assembly and a second output gear to transfer the second torque acting in a second direction opposite the first direction to a second rotor of the rotor assembly. The second torque transferred by each gear set of the two gear sets is substantially equal.
Public/Granted literature
- US20150060596A1 TORQUE SPLIT GEARBOX FOR ROTARY WING AIRCRAFT Public/Granted day:2015-03-05
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