Supersonic compressor
Abstract
A supersonic compressor including a rotor to deliver a gas at supersonic conditions to a diffuser. The diffuser includes a plurality of aerodynamic ducts that have converging and diverging portions, for deceleration of gas to subsonic conditions and then for expansion of subsonic gas, to change kinetic energy of the gas to static pressure. The aerodynamic ducts include vortex generating structures for controlling boundary layer, and structures for changing the effective contraction ratio to enable starting even when the aerodynamic ducts are designed for high pressure ratios, and structures for boundary layer control. In an embodiment, aerodynamic ducts are provided having an aspect ratio of in excess of two to one, when viewed in cross-section orthogonal to flow direction at an entrance to the aerodynamic duct.
- Inventors:
- Issue Date:
- Research Org.:
- Dresser-Rand Company, Olean, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1246895
- Patent Number(s):
- 9309893
- Application Number:
- 13/542,678
- Assignee:
- Dresser-Rand Company (Olean, NY)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F03 - MACHINES OR ENGINES FOR LIQUIDS F03D - WIND MOTORS
F - MECHANICAL ENGINEERING F04 - POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS F04D - NON-POSITIVE-DISPLACEMENT PUMPS
- DOE Contract Number:
- FE0000493
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2012 Jul 06
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING; 71 CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS
Citation Formats
Roberts, II, William Byron, Lawlor, Shawn P., and Breidenthal, Robert E. Supersonic compressor. United States: N. p., 2016.
Web.
Roberts, II, William Byron, Lawlor, Shawn P., & Breidenthal, Robert E. Supersonic compressor. United States.
Roberts, II, William Byron, Lawlor, Shawn P., and Breidenthal, Robert E. Tue .
"Supersonic compressor". United States. https://www.osti.gov/servlets/purl/1246895.
@article{osti_1246895,
title = {Supersonic compressor},
author = {Roberts, II, William Byron and Lawlor, Shawn P. and Breidenthal, Robert E.},
abstractNote = {A supersonic compressor including a rotor to deliver a gas at supersonic conditions to a diffuser. The diffuser includes a plurality of aerodynamic ducts that have converging and diverging portions, for deceleration of gas to subsonic conditions and then for expansion of subsonic gas, to change kinetic energy of the gas to static pressure. The aerodynamic ducts include vortex generating structures for controlling boundary layer, and structures for changing the effective contraction ratio to enable starting even when the aerodynamic ducts are designed for high pressure ratios, and structures for boundary layer control. In an embodiment, aerodynamic ducts are provided having an aspect ratio of in excess of two to one, when viewed in cross-section orthogonal to flow direction at an entrance to the aerodynamic duct.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2016},
month = {4}
}
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