WO1999022117A1 - An air turbine motor - Google Patents

An air turbine motor Download PDF

Info

Publication number
WO1999022117A1
WO1999022117A1 PCT/AU1998/000890 AU9800890W WO9922117A1 WO 1999022117 A1 WO1999022117 A1 WO 1999022117A1 AU 9800890 W AU9800890 W AU 9800890W WO 9922117 A1 WO9922117 A1 WO 9922117A1
Authority
WO
WIPO (PCT)
Prior art keywords
air
elements
turbine
drive
motor
Prior art date
Application number
PCT/AU1998/000890
Other languages
English (en)
French (fr)
Inventor
Kenneth Douglas Horner
Original Assignee
Kenneth Douglas Horner
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 Kenneth Douglas Horner filed Critical Kenneth Douglas Horner
Priority to US09/530,146 priority Critical patent/US6312220B1/en
Priority to AU10102/99A priority patent/AU742776B2/en
Priority to EP98952402A priority patent/EP1027530B1/de
Priority to DE69835439T priority patent/DE69835439T2/de
Publication of WO1999022117A1 publication Critical patent/WO1999022117A1/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/06Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially radially
    • F01D1/08Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially radially having inward flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/02Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/06Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines traversed by the working-fluid substantially radially
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/06Adaptations for driving, or combinations with, hand-held tools or the like control thereof

Definitions

  • This invention relates to air turbine motors.
  • the invention has been particularly developed for use in a pneumatic starter motor and will be primarily described with reference to this application.
  • the motor is however suitable for use in other applications where pneumatic motors are used due to the nature of the operating environment or otherwise.
  • Pneumatic starter motors are used for cranking internal combustion engines for starting purposes and are typically used for large engines and engines operating in environments where electric starting systems can be hazardous such as in mines.
  • Some known pneumatic starter motors have utilised a arrangement in which a flow of air generally parallel to the axis of rotation of a turbine wheel interacts with turbine elements to drive the wheel in rotation.
  • air is directed radially with respect to the axis of rotation of a turbine wheel to interact with radially oriented elements which drive the wheel in rotation. Whilst both arrangements have been used to provide satisfactory air motors for pneumatic starters and other applications, improvements in output and operating characteristics are continuously sought.
  • this invention provides an air turbine motor including a turbine wheel mounted for rotation about an axis, a first set of elements displaced around said turbine wheel and arranged to drive said turbine wheel in rotation about said axis in a first direction in response to an axial flow of air generally parallel to said axis, a second set of elements displaced around said turbine and arranged to drive said turbine wheel in rotation about said axis in said first direction in response to a radial flow of air generally perpendicular to said axis, and means to direct drive air to said first set of elements in an axially directed flow and to direct drive air to said second set of elements in a radially directed flow.
  • the drive air is firstly directed to the first or axially driven set of elements and is subsequently directed to the second or radially driven set of elements.
  • the axially driven set of elements is arranged around an outer circumferential edge of the turbine wheel and the radially driven set of elements is arranged on a face of said turbine wheel.
  • the radially driven set of elements are preferably arranged in two consecutive stages whereby the drive air passes through one stage and then the other stage.
  • the consecutive stages are preferably formed by arranging the elements in two concentric circular arrays.
  • the turbine wheel is preferably mounted between two stator arrangements.
  • the first of the stators directs drive air axially toward said axially driven elements whilst the second stator re-directs air emerging from said axially driven elements in a radial direction to said radially driven elements.
  • This preferred turbine stator configuration prevents a high side thrust loading on the turbine wheel. This is because the inlet air through the first stator exerts force which is opposite to the axial force developed by the air passing through the radially driven elements on the remote side of the turbine wheel. Additionally, the configuration allows a very compact and easily assembled air turbine motor to be produced.
  • the air turbine motor according to this invention has been found to provide a superior power output for a given drive air input. This allows a corresponding reduction in the size of the motor to produce a given power output.
  • the air turbine motor of this invention also as a higher stall torque, that is, torque at zero ⁇ m. This is particularly important for applications to pneumatic starter motors since start load is frequently very high.
  • Figure 1 is a schematic sectional view of an air turbine motor according to this invention
  • Figure 2 is an elevation of the turbine forming part of the air motor of Figure 1 ; and Figure 3 is a rear elevation of the turbine shown in Figure 2.
  • the air turbine motor 1 comprises a housing 2 in which a turbine wheel 3 is mounted for rotation between an air inlet stator 4 and a second stator 5.
  • An air inlet manifold 6 is provided in the housing in a known way.
  • Stator 4 has a series of sequentially arranged elements or vanes 7 which direct air flow from manifold 6 toward turbine wheel 3.
  • the outer circumference of turbine wheel 3 supports an array of axial turbine elements 8 evenly distributed around the circumference of the turbine wheel.
  • Two concentric rings of radial turbine elements 9, 10 are formed on a face 11 of wheel 3 remote from the inlet stator 4.
  • the second stator 5 is provided with circular arrays of elements or vanes 12, 13 which respectively fit between axial elements 8 and 9 and radial elements 9 and 10.
  • An exhaust manifold 14 is provide in housing 2.
  • Stators 4 and 5 support turbine wheel 3, for rotation about its axis.
  • the turbine 3 is supported by the interengaging formations and does not require the use of supporting bearings. This is made possible by the above configuration in which the turbine wheel 3 is similarly loaded in opposing axial directions by the drive air pressure thus avoiding any axially longitudinal loading.
  • Arrows 15 show the path of the air through the air turbine motor.
  • the air is admitted to manifold 6 by an appropriate control valve (not shown) in the known manner.
  • the air passes through elements 7 of stator 4 which direct the air generally axially into axially driven elements 8.
  • the air exiting elements 8 is turned through 90° by elements 12 of stator
  • the air exiting elements 9 is directed into the second stage of radially driven elements 10 (or third stage of the motor) by elements 13 of stator 5. The air then passes into exhaust manifold 14 for exhaust to the atmosphere in the usual manner.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Lens Barrels (AREA)
  • Control Of Electric Motors In General (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Valve Device For Special Equipments (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
PCT/AU1998/000890 1997-10-27 1998-10-27 An air turbine motor WO1999022117A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US09/530,146 US6312220B1 (en) 1997-10-27 1998-10-27 Air turbine motor
AU10102/99A AU742776B2 (en) 1997-10-27 1998-10-27 An air turbine motor
EP98952402A EP1027530B1 (de) 1997-10-27 1998-10-27 Pneumatischer Anlasser
DE69835439T DE69835439T2 (de) 1997-10-27 1998-10-27 Pneumatischer Anlasser

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AUPP0033A AUPP003397A0 (en) 1997-10-27 1997-10-27 An air turbine motor
AUPP0033 1997-10-27

Publications (1)

Publication Number Publication Date
WO1999022117A1 true WO1999022117A1 (en) 1999-05-06

Family

ID=3804309

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/AU1998/000890 WO1999022117A1 (en) 1997-10-27 1998-10-27 An air turbine motor

Country Status (5)

Country Link
EP (1) EP1027530B1 (de)
AT (1) ATE335124T1 (de)
AU (1) AUPP003397A0 (de)
DE (1) DE69835439T2 (de)
WO (1) WO1999022117A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9714637B1 (en) 2013-09-04 2017-07-25 Carl A. Stacey Pneumatic starter for a chainsaw

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU1094523A (en) * 1923-02-02 1923-07-03 Metropolitan-Vickers Electrical Company Limited Improvements relating to elastic fluid turbines

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE262119C (de) *
GB237611A (de) * 1924-07-24 1925-10-15 International General Electric Company Incorporated
GB361772A (de) * 1930-03-24 1931-11-26 Aktiebolaget Milo
DE689593C (de) * 1934-01-21 1940-03-28 Phil Ulrich Meininghaus Dr Ing Kreiselmaschine, vorzugsweise Dampf- oder Gasturbine
DE720938C (de) * 1940-06-20 1942-05-20 Siemens Ag Radial beaufschlagte Kreiselmaschine, vorzugsweise Dampf- oder Gasturbine
DE869969C (de) * 1951-04-14 1953-03-09 Wagner Hochdruck Dampfturbinen Radial-Dampf- oder -Gasturbine
US4573870A (en) * 1984-10-26 1986-03-04 Elliott Turbomachinery Co., Inc. Solid turbine wheel with guided discharge
RU2008435C1 (ru) * 1991-02-11 1994-02-28 Нижегородский государственный технический университет Радиальная турбина

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU1094523A (en) * 1923-02-02 1923-07-03 Metropolitan-Vickers Electrical Company Limited Improvements relating to elastic fluid turbines

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
DERWENT ABSTRACT, Accession No. 80-G9015C/32, Class Q51; & SU 703670 A (LENINGRAD POLY) 15 December 1979. *
DERWENT ABSTRACT, Accession No. 83-734030/32, Class Q51; & SU 964197 A (LENGD KALININ POLY) 09 October 1982. *
DERWENT ABSTRACT, Accession No. 91-085835/12, Class Q51; & SU 1560731 A (LENGD KALININ POLY) 30 April 1990. *

Also Published As

Publication number Publication date
EP1027530B1 (de) 2006-08-02
DE69835439T2 (de) 2007-02-01
AUPP003397A0 (en) 1997-11-20
EP1027530A4 (de) 2004-05-12
EP1027530A1 (de) 2000-08-16
ATE335124T1 (de) 2006-08-15
DE69835439D1 (de) 2006-09-14

Similar Documents

Publication Publication Date Title
CN101153546B (zh) 双轴燃气涡轮
US8096126B2 (en) Motor-driven supercharger
US7661271B1 (en) Integrated electric gas turbine
EP1809875B1 (de) Mikroleistungserzeugungsvorrichtung
US3685287A (en) Re-entry type integrated gas turbine engine and method of operation
US20140150401A1 (en) Geared compressor for gas turbine engine
US10718271B2 (en) Hybrid amplification of high spool motoring via low spool power extraction and motoring of a differential geared generator
CN103649545A (zh) 电动增压压缩机、其装配方法及内燃机
US6312220B1 (en) Air turbine motor
KR102013371B1 (ko) 내부 전기 모터를 구비한 터보차저를 위한 베어링 시스템
CN109268143A (zh) 燃气轮机转子以及燃气轮机发电机
JP4095150B2 (ja) 最適化された圧縮システムをもつタービンエンジン
US20210054809A1 (en) Multistage gas turbine engine with differential drive of compressor
US20170321600A1 (en) System and method for a gas turbine power generation system with a high pressure compressor with an added forward stage
JP2008519580A (ja) 電気機械装置
US8727751B2 (en) Vacuum pumping arrangement
EP1027530B1 (de) Pneumatischer Anlasser
EP0811752B1 (de) Gasturbine mit von innen nach aussen durchströmtem radialrad
AU742776B2 (en) An air turbine motor
WO1998016722A3 (en) Orbiting engine
US5182904A (en) Gas turbine engine power unit
JP2010200456A (ja) モータロータ
US11867075B2 (en) Radial outward bearing support for a rotating structure of a turbine engine
US3690784A (en) Turbine
GB2613076A (en) Electric machine within a turbine engine

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): AU GB US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LU MC NL PT SE

DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 10102/99

Country of ref document: AU

WWE Wipo information: entry into national phase

Ref document number: 1998952402

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 09530146

Country of ref document: US

WWP Wipo information: published in national office

Ref document number: 1998952402

Country of ref document: EP

WWW Wipo information: withdrawn in national office

Ref document number: 10102/99

Country of ref document: AU

WWG Wipo information: grant in national office

Ref document number: 10102/99

Country of ref document: AU

WWG Wipo information: grant in national office

Ref document number: 1998952402

Country of ref document: EP