Invention Grant
- Patent Title: Variable ratio gearbox for a rotary wing aircraft tail rotor
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Application No.: US15679840Application Date: 2017-08-17
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Publication No.: US10745118B2Publication Date: 2020-08-18
- Inventor: Frederick L. Bourne , Timothy F. Lauder , Nicholas D. Lappos
- 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: B64C27/12
- IPC: B64C27/12 ; F16H3/44 ; B64C27/82 ; B64C27/10 ; F16H3/72

Abstract:
A rotary wing aircraft including a prime mover, a main rotor assembly having a first plurality of rotor blades operatively coupled to a main rotor shaft rotatable at a first speed ratio, a tail rotor assembly including a second plurality of rotor blades operatively coupled to a tail rotor shaft rotatable at a second speed ratio, and a variable ratio gearbox assembly mechanically connected to the tail rotor assembly. The variable ratio gearbox assembly operates to selectively vary the second speed ratio relative to the first speed ratio.
Public/Granted literature
- US20180086443A1 VARIABLE RATIO GEARBOX FOR A ROTARY WING AIRCRAFT TAIL ROTOR Public/Granted day:2018-03-29
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