CA2426906A1 - Statoreacteur rotatif - Google Patents

Statoreacteur rotatif Download PDF

Info

Publication number
CA2426906A1
CA2426906A1 CA002426906A CA2426906A CA2426906A1 CA 2426906 A1 CA2426906 A1 CA 2426906A1 CA 002426906 A CA002426906 A CA 002426906A CA 2426906 A CA2426906 A CA 2426906A CA 2426906 A1 CA2426906 A1 CA 2426906A1
Authority
CA
Canada
Prior art keywords
thruster
engine
recited
rotor
base
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.)
Granted
Application number
CA002426906A
Other languages
English (en)
Other versions
CA2426906C (fr
Inventor
Martin Brouillette
Jean-Sebastien Plante
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.)
SOCPRA Sciences et Genie SEC
Original Assignee
Universite de Sherbrooke
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
Priority claimed from CA002382382A external-priority patent/CA2382382A1/fr
Application filed by Universite de Sherbrooke filed Critical Universite de Sherbrooke
Priority to CA2426906A priority Critical patent/CA2426906C/fr
Publication of CA2426906A1 publication Critical patent/CA2426906A1/fr
Application granted granted Critical
Publication of CA2426906C publication Critical patent/CA2426906C/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA2426906A 2002-04-16 2003-04-16 Statoreacteur rotatif Expired - Lifetime CA2426906C (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA2426906A CA2426906C (fr) 2002-04-16 2003-04-16 Statoreacteur rotatif

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CA2,382,382 2002-04-16
CA002382382A CA2382382A1 (fr) 2002-04-16 2002-04-16 Moteur rotatif continu a combustion induite par onde de choc
CA2426906A CA2426906C (fr) 2002-04-16 2003-04-16 Statoreacteur rotatif

Publications (2)

Publication Number Publication Date
CA2426906A1 true CA2426906A1 (fr) 2003-10-16
CA2426906C CA2426906C (fr) 2011-06-14

Family

ID=29271306

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2426906A Expired - Lifetime CA2426906C (fr) 2002-04-16 2003-04-16 Statoreacteur rotatif

Country Status (1)

Country Link
CA (1) CA2426906C (fr)

Also Published As

Publication number Publication date
CA2426906C (fr) 2011-06-14

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Legal Events

Date Code Title Description
EEER Examination request
MKEX Expiry

Effective date: 20230417