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CA2736720A1 - Systeme de detournement de gaz d'echappement afin d'actionner d'autres elements d'un aeronef - Google Patents

Systeme de detournement de gaz d'echappement afin d'actionner d'autres elements d'un aeronef Download PDF

Info

Publication number
CA2736720A1
CA2736720A1 CA 2736720 CA2736720A CA2736720A1 CA 2736720 A1 CA2736720 A1 CA 2736720A1 CA 2736720 CA2736720 CA 2736720 CA 2736720 A CA2736720 A CA 2736720A CA 2736720 A1 CA2736720 A1 CA 2736720A1
Authority
CA
Canada
Prior art keywords
duct
combustion engine
internal
inlet
auxiliary feature
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
CA 2736720
Other languages
English (en)
Inventor
Salvador Vidal
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CA 2736720 priority Critical patent/CA2736720A1/fr
Publication of CA2736720A1 publication Critical patent/CA2736720A1/fr
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • F02C1/002—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid using an auxiliary fluid
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)
CA 2736720 2011-04-08 2011-04-08 Systeme de detournement de gaz d'echappement afin d'actionner d'autres elements d'un aeronef Abandoned CA2736720A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA 2736720 CA2736720A1 (fr) 2011-04-08 2011-04-08 Systeme de detournement de gaz d'echappement afin d'actionner d'autres elements d'un aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA 2736720 CA2736720A1 (fr) 2011-04-08 2011-04-08 Systeme de detournement de gaz d'echappement afin d'actionner d'autres elements d'un aeronef

Publications (1)

Publication Number Publication Date
CA2736720A1 true CA2736720A1 (fr) 2012-10-08

Family

ID=47008171

Family Applications (1)

Application Number Title Priority Date Filing Date
CA 2736720 Abandoned CA2736720A1 (fr) 2011-04-08 2011-04-08 Systeme de detournement de gaz d'echappement afin d'actionner d'autres elements d'un aeronef

Country Status (1)

Country Link
CA (1) CA2736720A1 (fr)

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Legal Events

Date Code Title Description
FZDE Dead

Effective date: 20170410