ATE411464T1 - Heisswandzündungseinsatz für eine flügelzellenmaschine - Google Patents

Heisswandzündungseinsatz für eine flügelzellenmaschine

Info

Publication number
ATE411464T1
ATE411464T1 AT01959428T AT01959428T ATE411464T1 AT E411464 T1 ATE411464 T1 AT E411464T1 AT 01959428 T AT01959428 T AT 01959428T AT 01959428 T AT01959428 T AT 01959428T AT E411464 T1 ATE411464 T1 AT E411464T1
Authority
AT
Austria
Prior art keywords
fuel
combustion
vane
hot wall
insert
Prior art date
Application number
AT01959428T
Other languages
English (en)
Inventor
Brian Mallen
Original Assignee
Mallen Res Ltd Partnership
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 Mallen Res Ltd Partnership filed Critical Mallen Res Ltd Partnership
Application granted granted Critical
Publication of ATE411464T1 publication Critical patent/ATE411464T1/de

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F01C1/3441—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
    • F01C1/3443—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation with a separation element located between the inlet and outlet opening
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00—Other engines
    • F02B75/02—Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Rotary Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Fuel Cell (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Outer Garments And Coats (AREA)
  • Professional, Industrial, Or Sporting Protective Garments (AREA)
  • Apparatus Associated With Microorganisms And Enzymes (AREA)
AT01959428T 2000-08-02 2001-08-02 Heisswandzündungseinsatz für eine flügelzellenmaschine ATE411464T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/631,882 US6321713B1 (en) 2000-08-02 2000-08-02 Hot wall combustion insert for a rotary vane pumping machine

Publications (1)

Publication Number Publication Date
ATE411464T1 true ATE411464T1 (de) 2008-10-15

Family

ID=24533163

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01959428T ATE411464T1 (de) 2000-08-02 2001-08-02 Heisswandzündungseinsatz für eine flügelzellenmaschine

Country Status (7)

Country Link
US (1) US6321713B1 (de)
EP (1) EP1315904B1 (de)
AT (1) ATE411464T1 (de)
AU (1) AU2001280985A1 (de)
CA (1) CA2416272C (de)
DE (1) DE60136196D1 (de)
WO (1) WO2002010588A1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2006318473B2 (en) * 2005-11-23 2012-06-07 Vengeance Power Inc. Internal combustion engine
FR2944832A1 (fr) * 2009-04-28 2010-10-29 Vache Conseils Et Participatio Moteur rotatif a air equipe de pales coulissantes
US10544732B2 (en) 2011-07-28 2020-01-28 Pratt & Whitney Canada Corp. Rotary internal combustion engine with removable subchamber insert
US10557407B2 (en) 2011-07-28 2020-02-11 Pratt & Whitney Canada Corp. Rotary internal combustion engine with pilot subchamber
US9528434B1 (en) 2011-07-28 2016-12-27 Pratt & Whitney Canada Corp. Rotary internal combustion engine with pilot subchamber
US9038594B2 (en) 2011-07-28 2015-05-26 Pratt & Whitney Canada Corp. Rotary internal combustion engine with pilot subchamber
US10280830B2 (en) 2013-03-08 2019-05-07 Pratt & Whitney Canada Corp. System for pilot subchamber temperature control
US9334794B2 (en) 2013-06-05 2016-05-10 Pratt & Whitney Canada Corp. Rotary internal combustion engine with pilot subchamber and ignition element
US10876470B2 (en) * 2014-08-10 2020-12-29 Merton W. Pekrul Dynamic rotary engine vane force actuation apparatus including vane with stressed sheet
US10041402B2 (en) 2016-05-12 2018-08-07 Pratt & Whitney Canada Corp. Internal combustion engine with split pilot injection
US10082029B2 (en) 2016-07-08 2018-09-25 Pratt & Whitney Canada Corp. Internal combustion engine with rotor having offset peripheral surface
CN107401454B (zh) * 2017-06-16 2019-08-02 江苏大学 一种可实现转子发动机转子壁面加热的执行机构
US10145291B1 (en) 2017-10-10 2018-12-04 Pratt & Whitney Canada Corp. Rotary engine and method of combusting fuel
US10801394B2 (en) 2017-11-29 2020-10-13 Pratt & Whitney Canada Corp. Rotary engine with pilot subchambers
US12163461B2 (en) * 2019-08-09 2024-12-10 Astron Aerospace Llc Rotary engine, parts thereof, and methods
US11788462B2 (en) 2020-07-29 2023-10-17 Astron Aerospace Llc Rotary engine, parts thereof, and methods

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB394048A (en) * 1931-01-26 1933-06-22 Bendix Aviat Corp Improvements in internal combustion engines of the liquid fuel injection type
GB519659A (en) * 1938-09-27 1940-04-02 Arthur John Rowledge Improvements in or relating to sleeve-valve internal combustion engines
GB1017381A (en) * 1962-01-07 1966-01-19 Eickmann Karl Improvements in and relating to rotary machines of the radially sliding vane type
US3961483A (en) * 1975-07-03 1976-06-08 The Boeing Company Composite cycle engine
DE3642359A1 (de) * 1986-12-11 1988-06-16 Rainer Ruether Verbrennungsmotor
US4870827A (en) * 1987-08-12 1989-10-03 United Technologies Hybrid composite compressor
DE3909831A1 (de) * 1989-03-25 1990-09-27 Becker Kg Gebr Trockenlaufende drehschiebervakuumpumpe sowie verfahren zu deren herstellung
KR940006042B1 (ko) * 1990-06-04 1994-07-02 가부시끼가이샤 니뽄 크린 엔진 겐뀨쇼 열면충돌착화식 내연기관 및 그 열면충돌착화방법
US5836282A (en) * 1996-12-27 1998-11-17 Samsung Electronics Co., Ltd. Method of reducing pollution emissions in a two-stroke sliding vane internal combustion engine
US6125813A (en) * 1997-06-09 2000-10-03 Patrick Power Products, Inc. Prechamber combustion for a rotary diesel engine
US6078028A (en) * 1999-02-19 2000-06-20 Saint-Gobain Industrial Ceramics, Inc. Solderless ceramic igniter having a leadframe attachment

Also Published As

Publication number Publication date
CA2416272C (en) 2009-12-22
EP1315904B1 (de) 2008-10-15
AU2001280985A1 (en) 2002-02-13
EP1315904A1 (de) 2003-06-04
EP1315904A4 (de) 2004-06-23
CA2416272A1 (en) 2002-02-07
US6321713B1 (en) 2001-11-27
DE60136196D1 (de) 2008-11-27
WO2002010588A1 (en) 2002-02-07

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Legal Events

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