Invention Grant
US07083142B2 Compact co-axial rotor system for a rotary wing aircraft and a control system thereof
有权
用于旋翼飞机的紧凑型同轴转子系统及其控制系统
- Patent Title: Compact co-axial rotor system for a rotary wing aircraft and a control system thereof
- Patent Title (中): 用于旋翼飞机的紧凑型同轴转子系统及其控制系统
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Application No.: US10830160Application Date: 2004-04-21
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Publication No.: US07083142B2Publication Date: 2006-08-01
- Inventor: Mark Winfield Scott
- Applicant: Mark Winfield Scott
- Applicant Address: US CT Stratford
- Assignee: Sikorsky Aircraft Corporation
- Current Assignee: Sikorsky Aircraft Corporation
- Current Assignee Address: US CT Stratford
- Agency: Carlson, Gaskey & Olds
- Main IPC: B64C11/34
- IPC: B64C11/34
Abstract:
A dual, counter rotating, coaxial rotor system provides an upper and lower rotor system, with a reduced axial rotor separation distance along a common axis by way of rotor tip position sensing and rotor position controls to avoid tip contact.
Public/Granted literature
- US20050236518A1 Compact co-axial rotor system for a rotary wing aircraft and a control system therefor Public/Granted day:2005-10-27
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