Automotive turbine engine

• US 4,130,989 A
• Filed: 08/31/1977
• Issued: 12/26/1978
• Est. Priority Date: 11/19/1970
• Status: Expired due to Term

• Current Assignee: Manfred N. Wirth, Richard E. Wirth
• Original Assignee: Manfred N. Wirth, Richard E. Wirth
• Inventors: Wirth, Richard E., Wirth, Manfred N.
• Primary Examiner(s): Casaregola, Louis J.
• Application Number:
  US05/829,258
• Time in Patent Office: 482 Days
• Field of Search: 60/39.03, 60/39.12, 60/39.16, 60/39.17, 60/39.25, 60/39.29, 60/39.43, 60/39.52
• US Class Current: 60/39.52
• CPC Class Codes: F01D 17/165 for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line F01D17/167 takes precedence
• CPC Class Codes: F02C 3/36 Open cycles
• CPC Class Codes: F02C 6/20 Adaptations of gas-turbine plants for driving vehicles
• CPC Class Codes: F02C 9/16 Control of working fluid flow F02C9/48 takes precedence; control of air-intake flow F02C7/057
• CPC Class Codes: F23R 3/425 Combustion chambers comprising a tangential or helicoidal arrangement of the flame tubes
• CPC Class Codes: F23R 3/54 Reverse-flow combustion chambers

Abstract

Gas flow through a turbine is divided, with part of the flow directed to the compressor for the combustion chamber and part directed to the primary power turbine. Division of the gas flow is accomplished by a mixing wheel of novel design. Before passing to the primary power turbine the gas flow passes through a secondary power turbine that drives the compressor for the combustion chamber. Both the secondary power turbine and the compressor rotate independently of the main turbine rotor shaft. The power input to the secondary power turbine is varied in accordance with the pressure differential between the gas pressure at the outlet of the compressor for the combustion chamber and the outlet from the mixing wheel. If the speed of the main turbine shaft slows down more power is put into the secondary power turbine and the combustion chamber compressor is speeded up so as to produce a higher gas pressure than would otherwise be the case.

Claims

1. In a gas turbine, the combination of

(a) a mixing wheel comprising a radial flow centrifugal impeller;

(b) a combustion chamber adjacent the periphery of said mixing wheel.

(c) said mixing wheel having an annular inlet on one face thereof to receive compressed air,

(d) means including a first fixed opening controlling said annular inlet to admit compressed air to the mixing wheel for only a first arcuate portion of the wheel'"'"'s rotational travel.

(e) means including a second fixed opening for communicating the exhaust of said combustion chamber with the periphery of said mixing wheel for only a second arcuate portion of the wheel'"'"'s rotational travel so as to conduct the gases from the combustion chamber to said mixing wheel,

(f) means closing off said annular inlet and the periphery of said mixing wheel for only a third arcuate portion of the wheel'"'"'s rotational travel wherein said compressed air and combustion gases are mixed in the mixing wheel under constant volume, and

(d) mixture exit means occupying only a forth arcuate portion of the wheel'"'"'s rotational travel.