Very high speed radial inflow hydraulic turbine

• US 5,471,965 A
• Filed: 11/23/1994
• Issued: 12/05/1995
• Est. Priority Date: 12/24/1990
• Status: Expired due to Term

• Current Assignee: Davorin D. Kapich
• Original Assignee: Davorin D. Kapich
• Inventors: Kapich, Davorin D.
• Primary Examiner(s): KOCZO JR, MICHAEL
• Application Number:
  US08/344,231
• Time in Patent Office: 377 Days
• Field of Search: 60/607, 60/608, 123/565, 415/202
• US Class Current: 123/565
• CPC Class Codes: F02B 2275/32 Miller cycle
• CPC Class Codes: F02B 39/08 Non-mechanical drives, e.g. fluid drives having variable gear ratio
• CPC Class Codes: F02B 39/14 Lubrication of pumps; Safety measures therefor
• CPC Class Codes: F03B 1/00 Engines of impulse type, i.e. turbines with jets of high-velocity liquid impinging on blades or like rotors, e.g. Pelton wheels; Parts or details peculiar thereto
• CPC Class Codes: F04D 25/04 the pump being fluid-driven pumps driven by exhaust gases F02B37/00, F02B39/00; turbochargers F02C6/12
• CPC Class Codes: Y02E 10/20 Hydro energy
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A very high speed radial inflow hydraulic turbine drive. Inflow nozzles drilled in a nozzle body intersect a circular nozzle body exit surface, the centerline of each nozzle forming an angle of between 8 and 25 degrees with the tangent of the exit circle at the point of intersection. The turbine wheel of the drive is small. Its diameter measured at the tips of the blades is less than 2 inches. In a preferred embodiment, built and tested by Applicant, the wheel is only 0.80 inch diameter. This embodiment was tested with a turbine hydraulic fluid pressure drop of 700 psi and flow of 19.5 GPM. The 0.8 inch turbine produced 5.9 HP at 62,000 RPM driving the compressor portion of a TO4B-V turbocharger. The compressed air flow was measured at 11.3 pounds per minute (161.4 inlet CFM) at a pressure ratio of 1.41. During the test the acceleration of the supercharger was measured from idle to 62,000 RPM in about 1/2 second. This preferred embodiment utilizes a plastic-metal turbine wheel in which the plastic portion of the wheel other than the blades is solidly anchored within a metal containing wheel. In other preferred embodiments the turbine drive drives superchargers for supercharging internal combustion engines such as bus and truck turbodiesel engines. The superchargers provided by the present invention produce immediate response to engine demand for increased combustion air and will dramatically reduce smoke emission during low speed acceleration of these bus and truck engines as well as greatly improve engine efficiency.

Claims

1. A hydraulic supercharger system comprising:

(a) a hydraulic pump,

(b) a supercharger comprising;

i) a shaft defining a shaft axis and supported by supercharger bearings,

ii) a high speed hydraulic radial inflow turbine drive comprising;

(1) a turbine nozzle body defining a turbine nozzle body outlet surface and comprising a hydraulic fluid cavity and a plurality of nozzles, each of said nozzles providing a passageway for hydraulic fluid to pass inwardly from said hydraulic fluid cavity to said outlet surface and defining a nozzle centerline, where each of said nozzle centerlines;

(A) intersects said turbine nozzle body outlet surface at a point of intersection on a circle which is concentric about said shaft axis and defines a nozzle exit circle and

(B) forms an angle of 8 to 30 degrees with a tangent to said nozzle exit circle at said point of intersection,

(2) a radial in-flow hydraulic turbine wheel assembly comprising a plurality of radial flow turbine blades on a blade circle having a diameter of less than 2 inches;

said turbine wheel assembly being arranged in relation to said shaft and said turbine body outlet surface such that hydraulic fluid discharged from said nozzles impinges on said blades to cause rotation of said turbine wheel and said shaft,

iii) a compressor driven by said hydraulic turbine drive,

(c) a hydraulic venturi unit defining a main inlet, an outlet and a low pressure throat section,

(d) an expansion tank,

(e) a main hydraulic piping means providing a hydraulic circulation loop for hydraulic fluid to flow from said pump, to drive said hydraulic turbine drive, to said main inlet of said venturi unit, through said venturi unit, to said venturi outlet and back to said pump,

(f) a supercharger bypass system comprising a controlled bypass valve and a piping means to permit a portion of said hydraulic fluid flow to bypass said supercharger turbine drive, and

(g) a lubrication piping means providing a lubrication route for a portion of said hydraulic fluid flow from said turbine drive to said bearings, to said expansion tank and to said low pressure throat section of said venturi unit.

2. A system as in claim 1 and further comprising an oil cooler located within said hydraulic circulation loop.

3. A system as in claim 1 wherein said pump is driven by a combustion engine and said compressor provides compressed air to said engine.

4. A system as in claim 1 wherein said expansion tank is pressurized by exhaust air from said compressor.

5. A system as in claim 2 wherein said expansion tank is vented to so as to maintain the tank at atmospheric pressure.

6. A system as in claim 3 and further comprising a turbocharger driven by exhaust from said engine wherein said compressed air from said supercharger is further compressed by said turbocharger.

7. A system as in claim 1 wherein said turbine wheel is comprised of plastic, said plurality of blades being comprised of plastic, and a metal confinement means for confining substantially all of said plastic turbine wheel except said plurality of turbine blades.

8. A hydraulic system for a motor vehicle driven by an internal combustion engine comprising:

(a) a hydraulic pump,

(b) a supercharger,

(c) an electric generator,

(d) an air conditioning compressor, wherein said supercharger, said electric generator and said air conditioning compressor are each driven by a high speed radial inflow hydraulic turbine comprising;

i) a shaft defining a shaft axis and supported by bearings,

ii) a turbine nozzle body defining a turbine nozzle body outlet surface and comprising a hydraulic fluid cavity and a plurality of nozzles, each of said nozzles providing a passageway for hydraulic fluid to pass inwardly from said hydraulic fluid cavity to said outlet surface and defining a nozzle centerline, where each of said nozzle centerlines;

(A) intersects said turbine nozzle body outlet surface at a point of intersection on a circle which is concentric about said shaft axis and defines a nozzle exit circle and

(B) forms an angle of 8 to 30 degrees with a tangent to said nozzle exit circle at said point of intersection,

iii) a radial inflow hydraulic turbine wheel assembly comprising a plurality of radial flow turbine blades on a blade circle having a diameter of less than 2 inches;

said turbine wheel assembly being arranged in relation to said shaft and said turbine body outlet surface such that hydraulic fluid discharged from said nozzles impinges on said blades to cause rotation of said turbine wheel and said shaft,

(e) a venturi unit defining a venturi main inlet, and a venturi outlet,

(f) a main hydraulic piping means providing a hydraulic circulation loop for hydraulic fluid to flow from said pump, to drive said hydraulic turbine drives, to said venturi main inlet, through said venturi unit, to said venturi outlet and back to said pump,

(f) a supercharger bypass system comprising a controlled bypass valve and a piping means to permit a portion of said hydraulic fluid flow to bypass said supercharger turbine drive.

9. A very high speed radial inflow hydraulic turbine drive comprising:

(a) a shaft defining a shaft axis;

(b) a turbine nozzle body defining a turbine nozzle body outlet surface and comprising a hydraulic fluid cavity and a plurality of nozzles, each of said nozzles providing a passageway for hydraulic fluid to pass inwardly from said hydraulic fluid cavity to said outlet surface and defining a nozzle centerline, where each of said nozzle centerlines;

(1) intersects said turbine nozzle body outlet surface at a point of intersection on a circle which is concentric about said shaft axis and defines a nozzle exit circle of less than 2.2 inches and

(2) forms an angle of 8 to 30 degrees with a tangent to said nozzle exit circle at said point of intersection;

(c) a radial in-flow hydraulic turbine wheel assembly comprising a plurality of radial flow turbine blades with the blade tips defining a blade circle having a diameter of less than 2 inches;

said turbine wheel assembly being arranged in relation to said shaft and said turbine body outlet surface such that hydraulic fluid discharged from said nozzles impinges on said blades to cause rotation of said turbine wheel and said shaft;

wherein said turbine wheel is comprised of plastic, said plurality of blades being comprised of plastic, and a metal confinement means for confining substantially all of said plastic turbine wheel except said plurality of turbine blades.