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Researchers

  • Richard (Pat) Anderson
  • Charles Eastlake
  • Glenn Greiner
  • Matt Gonitzke

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Details

Project TitleHybrid Clutch Assembly for an Aircraft
Track Code2012-006
Short Description

A hybrid clutch assembly inserted between an internal combustion engine and the propeller of an aircraft to provide a hybrid-powered aircraft.

Abstract

A hybrid clutch assembly inserted between an internal combustion engine and the propeller of an aircraft to provide a hybrid-powered aircraft. The hybrid clutch assembly allows a direct current (DC) electric motor to be attached to the hybrid clutch assembly using drive belts. The hybrid clutch assembly allows the internal combustion engine to transmit power to the aircraft's propeller and freely spin the DC motor. The DC motor can transmit power to the aircraft's propeller without turning the internal combustion engine. The hybrid clutch assembly independently allows either the internal combustion engine or the DC motor in parallel to power the aircraft's propeller. The hybrid clutch assembly includes a hybrid clutch, a drive belt housing, a hybrid clutch assembly shaft, and an adapter plate. The hybrid clutch connects to the drive belt housing a hybrid clutch assembly shaft. The adapter plate enables connection of the hybrid clutch to the internal combustion engine propeller flange. The drive belt housing enables connection of the hybrid clutch to the propeller. The DC motor is connected to the drive belt housing drive belts.

 
TagsNone
 
Posted DateOct 1, 2014 10:08 AM

Researcher

Name
Richard (Pat) Anderson
Charles Eastlake
Glenn Greiner
Matt Gonitzke

Manager

Name
Stephanie Miller

Files

File Name Description
US 9,254,922 U.S. Issued Patent Download
US2014/0060995 U.S. Patent Application Publication Download
WO2014/137365 PCT Application Publication Download