Submitting Campus
Daytona Beach
Department
Aerospace Engineering
Document Type
Patent
Publication/Presentation Date
9-25-2014
Abstract/Description
A multi-stage axial compressor for counter rotation. A first series of rotor blade assemblies are mounted on and rotate with the driveshaft, each rotor blade assembly of the first series comprising a rotating stage of the multi-stage axial compressor. A second series of rotor blade assemblies provide a counter-rotating stage of the multi-stage axial compressor. An accessory drive links the second series of rotor blade assemblies to the driveshaft and causes counter-rotation of the second series of rotor blade assemblies.
Patent Number
US 2014/0286749 Al
Assignee
Embry-Riddle Aeronautical University
Application Number
13/800,836
Date Filed
3-13-2013
Scholarly Commons Citation
Gehlot, V., & Attia, M. S. (2014). Multi-Stage Axial Compressor with Counter-Rotation Using Accessory Drive. , (). Retrieved from https://commons.erau.edu/publication/2186
