Variable inlet for a radial turbine

• US 4,729,715 A
• Filed: 07/16/1986
• Issued: 03/08/1988
• Est. Priority Date: 07/17/1985
• Status: Expired due to Fees

• Current Assignee: Geoffrey L. Wilde
• Original Assignee: Geoffrey L. Wilde
• Inventors: Wilde, Geoffrey L.
• Primary Examiner(s): Garrett, Robert E.
• Assistant Examiner(s): Pitko, Joseph M.
• Application Number:
  US06/886,221
• Time in Patent Office: 601 Days
• Field of Search: 415/126-128, 415/148, 415/150, 415/151, 415/157, 415/149 R, 415/158, 415/159, 415/162, 415/163, 415/160, 415/164, 415/165, 415/166, 415/205, 60/602, 60/606
• US Class Current: 415/150
• CPC Class Codes: F01D 17/146 by throttling the volute inlet of radial machines or engines

Abstract

A supercharger for an internal combustion engine has a turbine driven compressor. The turbine is driven by the exhaust gases and is mounted in a volute casing. The volute casing has an internal flow passage which has an inlet and the passage is arranged to receive and discharge a flow of motive gases. The passage is partly defined by one or more movable wall members. The or each wall member is movable to vary the passage area whilst allowing the whole of the flow of motive gas to flow through the passage. Two movable wall members can be provided operated by a common linkage and the volute casing can have two inlets to receive the exhaust gases from separate manifolds of an internal combustion engine.

Claims

1. A turbine apparatus comprising a volute casing having an internal flow passage for receiving and passing a driving medium to a turbine rotor connected to said passage, said passage having at least one inlet and one outlet, said passage being partly defined by at least one movable wall member, the wall member being movable to vary the area of the inlet between a first position in which the inlet area is at a maximum and further positions in which the inlet area is less than the maximum to allow the driving medium to flow over both surfaces of the wall member and to flow onto the surface of a turbine rotor at, at least, two locations angularly displaced with respect to one another when the movable wall member is located at any one of said further positions, said movable wall member having at least one opening defining a fixed area nozzle to allow the passage therethrough of a portion of the driving medium.

2. A volute casing according to claim 1 having two movable wall members, the wall members being movable to vary the flow passage area within the volute casing whilst allowing the whole of the flow of the motive gas to flow through the casing passge.

3. A volute casing according to claim 1 in which the wall member is pivotally mounted and is operable by a control mechanism.

4. A volute casing as claimed in claim 1 having a throttle valve located downstream of the outlet of the volute casing to provide control of the pressures at the inlet and outlet of the casing.

5. A volute casing as claimed in claim 1 in which the wall member has face seal means in contact with the internal surface of the volute casing.

6. A volute casing as claimed in claim 1 in which the wall member has a cooling channel arranged to receive a flow of cooling medium.

7. A volute casing as claimed in claim 1 having a bleed duct arranged to receive compressed air into the internal passage of the volute casing.

8. A volute casing as claimed in claim 1 in which the casing has two inlets each inlet being arranged to receive the exhaust gases from separate exhaust manifolds of an internal combustion engine.