US2006177302A1PendingUtilityA1
Axial flow compressor
Individually held — no corporate assignee on recordPriority: Feb 4, 2005Filed: Feb 4, 2005Published: Aug 10, 2006
Est. expiryFeb 4, 2025(expired)· nominal 20-yr term from priority
Inventors:Henry K. Berry, Iii
F05D 2250/232F04D 29/522F01D 25/24F02C 6/12
30
PatentIndex Score
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Claims
Abstract
An axial flow compressor is disclosed. The axial flow compressor includes a tapered housing, having a first open end and a second open end forming a fluid channel therebetween; a shaft, disposed axially within the tapered housing from the first open end to the second open end; a plurality of rotors, mounted to the shaft within the tapered housing for compressing air within the tapered housing; and a plurality of stators, mounted within the tapered housing; wherein the plurality of rotors, plurality of stators and tapered housing are not in physical contact.
Claims
exact text as granted — not AI-modified1 . An axial flow compressor, comprising:
a tapered housing, having a first open end and a second open end forming a fluid channel therebetween; a shaft, capable of rotation, disposed axially within the tapered housing from the first open end to the second open end; a first plurality of rotors, radially mounted to the shaft within the tapered housing for compressing air within the tapered housing; and a first plurality of stators, mounted within the tapered housing; wherein the first plurality of rotors, first plurality of stators and tapered housing are not in physical contact.
2 . The axial flow compressor of claim 1 , wherein the first plurality of rotors include blades and the first plurality of stators include vanes.
3 . The axial flow compressor of claim 2 , wherein the blades include a leading edge and the vanes include a leading edge.
4 . The axial flow compressor of claim 3 , wherein the leading edge of the blades are mounted opposite to the direction of the leading edge of the vanes.
5 . The axial flow compressor of claim 2 , wherein the tapered housing is formed of aluminum.
6 . The axial flow compressor of claim 2 , wherein the stator vanes are formed of high-density carbon fiber.
7 . The axial flow compressor of claim 2 , wherein the rotor blades are formed of high-density carbon fiber.
8 . The axial flow compressor of claim 2 , wherein the axle is formed of high speed steel.
9 . The axial flow compressor of claim 1 , further comprising a second plurality of rotors and a second plurality of stators.
10 . The axial flow compressor of claim 9 , further comprising a third plurality of rotors and a third plurality of stators.
11 . The axial flow compressor of claim 10 , further comprising a fourth plurality of rotors and a fourth plurality of stators.
12 . The axial flow compressor of claim 1 , wherein the first open end of the tapered housing receives air via ram pressure recovery.
13 . The axial flow compressor of claim 12 , wherein the pressure inside the first open end of the tapered housing returns to ambient pressure by means of the ram pressure recovery.
14 . The axial flow compressor of claim 1 , wherein the tapered housing tapers to between 25% and 35% from the first open end to the second open end.
15 . The axial flow compressor of claim 14 , wherein the tapered housing tapers to 25% from the first open end to the second open end.
16 . The axial flow compressor of claim 14 , wherein the tapered housing tapers to 35% from the first open end to the second open end.Join the waitlist — get patent alerts
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