Invention Grant
- Patent Title: Coaxial rotor system for helicopters
- Patent Title (中): 直升机同轴转子系统
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Application No.: US11985394Application Date: 2007-11-15
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Publication No.: US07931439B2Publication Date: 2011-04-26
- Inventor: Fuat Bahadir
- Applicant: Fuat Bahadir
- Agency: Stinson Morrison Hecker LLP
- Main IPC: F01D5/02
- IPC: F01D5/02

Abstract:
An improved coaxial rotor assembly for a helicopter includes an upper rotor system having a multiple of upper rotor blades each having outer tips and mounted on and extending outwards from a central rotor shaft and a lower rotor system having a multiple of lower rotor blades each having outer tips and mounted on and extending outwards from the central rotor shaft with the upper rotor system spaced an axial distance from the lower rotor system on the central rotor shaft. A rotor blade support ring extends circumferentially around each of the upper and lower rotor systems which movably engages and supports the outer tips of the upper and lower rotor blades in spaced apart relation such that the upper and lower rotor systems rotate in opposite directions and the rotor blade support ring means prevents contact between the upper and lower rotor systems during operation thereof.
Public/Granted literature
- US20090129929A1 Coaxial rotor system for helicopters Public/Granted day:2009-05-21
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