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US20080219843A1 - Centrifugal impeller with forward and reverse flow paths - Google Patents

Centrifugal impeller with forward and reverse flow paths Download PDF

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Publication number
US20080219843A1
US20080219843A1 US12/122,686 US12268608A US2008219843A1 US 20080219843 A1 US20080219843 A1 US 20080219843A1 US 12268608 A US12268608 A US 12268608A US 2008219843 A1 US2008219843 A1 US 2008219843A1
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US
United States
Prior art keywords
impeller
flow path
rearward
flow
flow paths
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US12/122,686
Inventor
Alfred Paul Matheny
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Florida Turbine Technologies Inc
Original Assignee
Florida Turbine Technologies Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Florida Turbine Technologies Inc filed Critical Florida Turbine Technologies Inc
Priority to US12/122,686 priority Critical patent/US20080219843A1/en
Publication of US20080219843A1 publication Critical patent/US20080219843A1/en
Abandoned legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/025Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal comprising axial flow and radial flow stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/284Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
    • F04D29/286Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors

Definitions

  • the present invention relates to a centrifugal impeller having both a forward flow path and a rearward flow path for driving a fluid such as a gas or a liquid in two different directions, and more specifically to an impeller used in a small gas turbine engine in the compressor section.
  • Centrifugal impellers are well known in the air of pumps used to pump a fluid such as a liquid or a gas.
  • a centrifugal impeller a plurality of closed fluid paths is formed between an inner surface and an outer surface of the impeller.
  • a common inlet located upstream of the plurality of closed fluid paths allows for the fluid to enter the impeller and then be divided up into the plurality of flow paths.
  • Each flow path includes an exit to discharge the fluid from the impeller.
  • Rotation of the impeller acts to drive the fluid from the inlet, through the closed passages, and out the individual outlets.
  • the inventors of the present invention are not aware of any that disclose outlets in more than one direction.
  • Gas turbine engines are known to have a compressor to compress air to be delivered to a combustor, and a fan to provide a bypass to the combustor.
  • a fan for the bypass is a separate impeller than the compressor used to deliver pressurized air to the combustor.
  • the present invention is a centrifugal impeller with an alternating series of outlets, where one set of outlets directs air from the impeller in a forward direction, while the other set of outlets directs air toward in a rearward direction.
  • a radial distance from the centerline of the impeller to the outlet of one path differs from the radial distance of another oath in order to vary the pressure of the flow paths.
  • the forward flow path because the radial distance is greater, will have a higher outlet pressure, and thus a greater flow volume, than would the flow path having the shorter radial distance.
  • a second embodiment of the present invention would include an unequal number of flow paths in the forward direction than in the rearward. In this embodiment, an even greater difference in flow volume can be produced because of the greater number of flow paths leading in the preferred direction.
  • a number forward flow paths can be equal to a number of rearward flow paths, but the size of one of the flow parts can be larger to provide a greater flow volume in the direction having the greater number of flow paths.
  • the two path impeller of this invention is intended to be used in a gas turbine engine in which a forward flow from the impeller is supplied to the combustor and the rearward flow bypasses the combustor in the direction of the outlet of the turbine.
  • FIG. 1 shows a cross-sectional view of a small gas turbine engine with the centrifugal impeller mounted rearward of a combustor, with the front flow and the rear flow paths indicated by arrows.
  • FIG. 2 shows a portion of the outer surface of the impeller with two front flow exits and two rear flow exits, the flows being indicated by arrows.
  • FIG. 3 shows a cross-sectional view of the impeller with a forward directed flow path and a rearward directed flow path.
  • a gas turbine engine 10 includes an impeller 12 to compress air for delivery to a combustor 26 , guide vanes 14 and 16 , a turbine blade 18 on the impeller 12 to convert hot gas airflow from the combustor 26 into useful work, an exhaust guide vane 20 downstream from the turbine blades 18 , a bearing 28 to support the rotary elements of the engine, and an inlet 30 to the impeller 12 .
  • a centrifugal impeller 12 has an inlet and an outlet for fluid that is pumped by the impeller. Impellers can pump both a liquid and a gas using the same configuration of impeller design.
  • the impeller includes a centrally located inlet 31 , a plurality of flow paths within the body of the impeller and extending from the inlet 31 through the impeller body, and a plurality of outlets 32 and 34 equal in number to the number of flow paths through the body. In the first embodiment of the present invention shown in FIG. 2 , the outlets alternate between a front discharge direction 32 and a rear discharge direction 34 .
  • the front discharge outlets 32 have a guide wall section that directs the outlet flow toward the front of the impeller, while the rear discharge outlets 34 have similar shaped guide walls to direct the flow in the rearward direction.
  • the front discharge outlets 32 and the rear discharge outlets 34 have the same size and shape, and since the internal passages for both are the same volume capacity, the flow through the front discharge outlets is the same as the flow through the rear discharge outlets.
  • the impeller 12 includes a plurality of forward directed flow path 32 and a plurality of rearward directed flow paths 34 .
  • the number of forward flow paths 32 is equal to the number of rearward flow paths 34 .
  • Each flow path includes an inlet 31 and a separate flow path extending from the inlet 31 to the respective outlet 32 or 34 , a radial distance from the centerline to the outlet of the forward flow path is greater than a radial distance from the centerline to the outlet of the rearward flow path. Because of the difference in radial distances, the pressure in the forward flow path will be higher than the pressure in the rearward flow path. Thus, various forward to rearward pressure differences can be achieved by varying the radial distances.
  • Another structure to provide different flow rates would be to design the higher flow rate side with larger volume flow passages while maintaining the ratio of outlet passages at the one-to-one ratio.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A centrifugal impeller having an inlet and a plurality of outlets the outlets including at least one outlet in a forward direction of the Impeller and at least one outlet in a rearward direction of the impeller. A flow path distance of the outlet in the forward direction can be greater than a flow path distance of the outlet in the rearward direction in order to provide a greater pressure in the outlet having the greater flow path distance. In another embodiment, the flow path volume in the forward direction can be greater than the flow path volume in the rearward direction in order to provide a greater flow volume in the forward direction In another embodiment, the number of flow paths in the forward direction can be greater than the number of flow paths in the rearward direction in order to provide a greater flow volume in the forward direction. The impeller is also used in a gas turbine engine in which the impeller also includes a turbine blade, and the forward directing outlets deliver compressed air to a combustor while the rearward directed outlets bypass the combustor.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application is a DIVISIONAL of U.S. Regular patent application Ser. No. 11/133,094 filed on May 19, 2005 and entitled CENTRIFUGAL IMPELLER WITH FORWARD AND REVERSE FLOW PATHS.
  • FEDERAL RESEARCH STATEMENT
  • None.
  • BACKGROUND OF THE INVENTION
  • 1. Field of the Invention
  • The present invention relates to a centrifugal impeller having both a forward flow path and a rearward flow path for driving a fluid such as a gas or a liquid in two different directions, and more specifically to an impeller used in a small gas turbine engine in the compressor section.
  • 2. Description of the Related Art Including Information Disclosed Under 37 CFR 1.97 and 1.98
  • Centrifugal impellers are well known in the air of pumps used to pump a fluid such as a liquid or a gas. In a centrifugal impeller, a plurality of closed fluid paths is formed between an inner surface and an outer surface of the impeller. A common inlet located upstream of the plurality of closed fluid paths allows for the fluid to enter the impeller and then be divided up into the plurality of flow paths. Each flow path includes an exit to discharge the fluid from the impeller. Rotation of the impeller acts to drive the fluid from the inlet, through the closed passages, and out the individual outlets. In all prior art impellers, the inventors of the present invention are not aware of any that disclose outlets in more than one direction.
  • Gas turbine engines are known to have a compressor to compress air to be delivered to a combustor, and a fan to provide a bypass to the combustor. In this arrangement, a fan for the bypass is a separate impeller than the compressor used to deliver pressurized air to the combustor.
  • It is a purpose of the present invention to provide for a centrifugal impeller that includes both a forward directed flow path and a rearward directed flow path.
  • It is another object of the present invention to provide for a gas turbine engine that has both a combustion flow path and a bypass flow path, in which the centrifugal impeller of the present invention provides for both the flow path into the combustion chamber and the flow path for the bypass of the fan.
  • SUMMARY OF THE INVENTION
  • The present invention is a centrifugal impeller with an alternating series of outlets, where one set of outlets directs air from the impeller in a forward direction, while the other set of outlets directs air toward in a rearward direction. A radial distance from the centerline of the impeller to the outlet of one path differs from the radial distance of another oath in order to vary the pressure of the flow paths. The forward flow path, because the radial distance is greater, will have a higher outlet pressure, and thus a greater flow volume, than would the flow path having the shorter radial distance.
  • A second embodiment of the present invention would include an unequal number of flow paths in the forward direction than in the rearward. In this embodiment, an even greater difference in flow volume can be produced because of the greater number of flow paths leading in the preferred direction.
  • In a third embodiment of the present invention, a number forward flow paths can be equal to a number of rearward flow paths, but the size of one of the flow parts can be larger to provide a greater flow volume in the direction having the greater number of flow paths.
  • The two path impeller of this invention is intended to be used in a gas turbine engine in which a forward flow from the impeller is supplied to the combustor and the rearward flow bypasses the combustor in the direction of the outlet of the turbine.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 shows a cross-sectional view of a small gas turbine engine with the centrifugal impeller mounted rearward of a combustor, with the front flow and the rear flow paths indicated by arrows.
  • FIG. 2 shows a portion of the outer surface of the impeller with two front flow exits and two rear flow exits, the flows being indicated by arrows.
  • FIG. 3 shows a cross-sectional view of the impeller with a forward directed flow path and a rearward directed flow path.
  • DETAILED DESCRIPTION OF THE INVENTION
  • A gas turbine engine 10 includes an impeller 12 to compress air for delivery to a combustor 26, guide vanes 14 and 16, a turbine blade 18 on the impeller 12 to convert hot gas airflow from the combustor 26 into useful work, an exhaust guide vane 20 downstream from the turbine blades 18, a bearing 28 to support the rotary elements of the engine, and an inlet 30 to the impeller 12.
  • A centrifugal impeller 12 has an inlet and an outlet for fluid that is pumped by the impeller. Impellers can pump both a liquid and a gas using the same configuration of impeller design. The impeller includes a centrally located inlet 31, a plurality of flow paths within the body of the impeller and extending from the inlet 31 through the impeller body, and a plurality of outlets 32 and 34 equal in number to the number of flow paths through the body. In the first embodiment of the present invention shown in FIG. 2, the outlets alternate between a front discharge direction 32 and a rear discharge direction 34. The front discharge outlets 32 have a guide wall section that directs the outlet flow toward the front of the impeller, while the rear discharge outlets 34 have similar shaped guide walls to direct the flow in the rearward direction. In the first embodiment shown in FIG. 2, the front discharge outlets 32 and the rear discharge outlets 34 have the same size and shape, and since the internal passages for both are the same volume capacity, the flow through the front discharge outlets is the same as the flow through the rear discharge outlets.
  • The present invention is best shown in FIG. 3 in which the impeller 12 includes a plurality of forward directed flow path 32 and a plurality of rearward directed flow paths 34. In the present embodiment, the number of forward flow paths 32 is equal to the number of rearward flow paths 34. Each flow path includes an inlet 31 and a separate flow path extending from the inlet 31 to the respective outlet 32 or 34, a radial distance from the centerline to the outlet of the forward flow path is greater than a radial distance from the centerline to the outlet of the rearward flow path. Because of the difference in radial distances, the pressure in the forward flow path will be higher than the pressure in the rearward flow path. Thus, various forward to rearward pressure differences can be achieved by varying the radial distances. Decrease the rearward flow path radial distance will increase the pressure ratio of the forward flow path versus the rear flow path. If the radial distances are equal, then the pressure ratio will be one (pressure of the forward flow path will be equal to the pressure of the rearward flow path).
  • Further embodiments of the present invention will have a different flow volume directed toward the front versus the flow directed toward the rear. This different flow volume rate is controlled by providing more outlets directed to the higher flow rate side than the number of outlets on the lower flow rate side. Another structure to provide different flow rates would be to design the higher flow rate side with larger volume flow passages while maintaining the ratio of outlet passages at the one-to-one ratio.

Claims (8)

1. A centrifugal impeller, comprising:
a common inlet;
a plurality of flow paths in communication with the common inlet;
a plurality of outlets, each outlet associated with a respective flow path; and,
at least one of the plurality of outlets being arranged to direct fluid flow substantially in a forward direction of the impeller, and at least one of the plurality of outlets being arranged to direct fluid flow substantially in a rearward direction of the impeller.
2. The centrifugal impeller of claim 1, and further comprising;
the at least one outlet in the forward direction has a flow path distance through the impeller greater than a flow path distance through the impeller of the outlet in the rearward direction.
3. The centrifugal impeller of claim 1, and further comprising:
a number of forward flow paths is equal to a number of rearward flow paths.
4. The centrifugal impeller of claim 1, and further comprising:
a number of forward flow paths is greater than a number of rearward flow paths.
5. The centrifugal impeller of claim 1, and further comprising:
a number of forward flow paths is less than a number of rearward flow paths.
6. The centrifugal impeller of claim 1, and further comprising:
a size of the forward flow path is greater than a size of the rearward flow path such that a greater volume of fluid flows in the forward flow path than does in the rearward flow path.
7. The centrifugal impeller of claim 1, and further comprising:
the forward flow paths and the rearward flow paths are all formed in the same rotor disk and discharge near the outer disk end.
8. The centrifugal impeller of claim 1, and further comprising:
the forward flow paths are separated within the rotor disk by the rearward flow paths.
US12/122,686 2005-05-19 2008-05-17 Centrifugal impeller with forward and reverse flow paths Abandoned US20080219843A1 (en)

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Application Number Priority Date Filing Date Title
US12/122,686 US20080219843A1 (en) 2005-05-19 2008-05-17 Centrifugal impeller with forward and reverse flow paths

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US11/133,094 US20060263214A1 (en) 2005-05-19 2005-05-19 Centrifugal impeller with forward and reverse flow paths
US12/122,686 US20080219843A1 (en) 2005-05-19 2008-05-17 Centrifugal impeller with forward and reverse flow paths

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US12/636,756 Expired - Fee Related US8070453B1 (en) 2005-05-19 2009-12-13 Centrifugal impeller having forward and reverse flow paths

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10072570B2 (en) 2013-01-28 2018-09-11 United Technologies Corporation Reverse flow gas turbine engine core

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8935926B2 (en) * 2010-10-28 2015-01-20 United Technologies Corporation Centrifugal compressor with bleed flow splitter for a gas turbine engine
FR2975733B1 (en) * 2011-05-23 2015-12-18 Turbomeca CENTRIFUGAL COMPRESSOR WHEEL
CN108691807A (en) * 2017-04-10 2018-10-23 清华大学 Aero-engine, centrifugal compressor and its diffuser structure
JP7455706B2 (en) * 2020-09-04 2024-03-26 三菱重工業株式会社 pump equipment

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US1768241A (en) * 1927-03-10 1930-06-24 Auto Prime Pump Company Centrifugal-pump impeller
US3189320A (en) * 1963-04-29 1965-06-15 Westinghouse Electric Corp Method of cooling turbine rotors and discs
US4018043A (en) * 1975-09-19 1977-04-19 Avco Corporation Gas turbine engines with toroidal combustors
US4195473A (en) * 1977-09-26 1980-04-01 General Motors Corporation Gas turbine engine with stepped inlet compressor
US4448573A (en) * 1982-03-25 1984-05-15 General Electric Company Single-stage, multiple outlet centrifugal blower
US4693673A (en) * 1982-08-09 1987-09-15 Nee Victor W Ceiling fan
US6651431B1 (en) * 2002-08-28 2003-11-25 Ford Global Technologies, Llc Boosted internal combustion engines and air compressors used therein

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US3253406A (en) * 1966-05-31 Turbine propulsion unit
US1788241A (en) * 1928-06-01 1931-01-06 Briede & Rogovsky Machine for bending trouser hooks
US2694291A (en) * 1948-02-07 1954-11-16 Henning C Rosengart Rotor and combustion chamber arrangement for gas turbines
US3749520A (en) * 1971-10-04 1973-07-31 Gen Motors Corp Centrifugal compressor blading
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US1768241A (en) * 1927-03-10 1930-06-24 Auto Prime Pump Company Centrifugal-pump impeller
US3189320A (en) * 1963-04-29 1965-06-15 Westinghouse Electric Corp Method of cooling turbine rotors and discs
US4018043A (en) * 1975-09-19 1977-04-19 Avco Corporation Gas turbine engines with toroidal combustors
US4195473A (en) * 1977-09-26 1980-04-01 General Motors Corporation Gas turbine engine with stepped inlet compressor
US4448573A (en) * 1982-03-25 1984-05-15 General Electric Company Single-stage, multiple outlet centrifugal blower
US4693673A (en) * 1982-08-09 1987-09-15 Nee Victor W Ceiling fan
US6651431B1 (en) * 2002-08-28 2003-11-25 Ford Global Technologies, Llc Boosted internal combustion engines and air compressors used therein

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10072570B2 (en) 2013-01-28 2018-09-11 United Technologies Corporation Reverse flow gas turbine engine core

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US8070453B1 (en) 2011-12-06
US20060263214A1 (en) 2006-11-23

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