BRPI1007499A2 - reator, especialmente um reator de aeronave - Google Patents

reator, especialmente um reator de aeronave

Info

Publication number
BRPI1007499A2
BRPI1007499A2 BRPI1007499A BRPI1007499A BRPI1007499A2 BR PI1007499 A2 BRPI1007499 A2 BR PI1007499A2 BR PI1007499 A BRPI1007499 A BR PI1007499A BR PI1007499 A BRPI1007499 A BR PI1007499A BR PI1007499 A2 BRPI1007499 A2 BR PI1007499A2
Authority
BR
Brazil
Prior art keywords
reactor
aircraft
reactor especially
aircraft reactor
Prior art date
Application number
BRPI1007499A
Other languages
English (en)
Inventor
Michel Aguilar
Original Assignee
Michel Aguilar
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 FR0900330A external-priority patent/FR2941496A1/fr
Application filed by Michel Aguilar filed Critical Michel Aguilar
Publication of BRPI1007499A2 publication Critical patent/BRPI1007499A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • 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
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants
    • 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
    • F02K7/02—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 the jet being intermittent, i.e. pulse-jet
    • F02K7/06—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 the jet being intermittent, i.e. pulse-jet with combustion chambers having valves
    • F02K7/067—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 the jet being intermittent, i.e. pulse-jet with combustion chambers having valves having aerodynamic valves
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/40—Cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Exhaust Silencers (AREA)
BRPI1007499A 2009-01-27 2010-01-15 reator, especialmente um reator de aeronave BRPI1007499A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0900330A FR2941496A1 (fr) 2009-01-27 2009-01-27 Turbomachine a combustion isochore, detente totale et effet statoreacteur pulse
FR0903942A FR2945316B1 (fr) 2009-01-27 2009-08-12 Reacteur, notamment reacteur pour aeronef
PCT/EP2010/000195 WO2010086091A1 (fr) 2009-01-27 2010-01-15 Reacteur notamment un reacteur pour aeronef

Publications (1)

Publication Number Publication Date
BRPI1007499A2 true BRPI1007499A2 (pt) 2016-02-16

Family

ID=42061050

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1007499A BRPI1007499A2 (pt) 2009-01-27 2010-01-15 reator, especialmente um reator de aeronave

Country Status (6)

Country Link
US (1) US8925296B2 (pt)
EP (1) EP2391802A1 (pt)
BR (1) BRPI1007499A2 (pt)
CA (1) CA2748891A1 (pt)
FR (1) FR2945316B1 (pt)
WO (1) WO2010086091A1 (pt)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2971814A1 (fr) * 2011-02-21 2012-08-24 Michel Aguilar Reacteur, notamment reacteur d'aeronef.
FR2983906B1 (fr) * 2011-12-09 2014-06-27 Michel Aguilar Procede d'allumage thermique de moteur a combustion pulsee, ainsi que thermoreacteur a allumage thermique
FR2991721B1 (fr) * 2012-06-07 2016-07-08 Michel Aguilar Procede et thermoreacteur de propulsion mono-valve a injection et combustion multiples par cycle de rotation
FR2994250B1 (fr) * 2012-08-03 2014-09-05 Snecma Chambre de combustion cvc pour turbomachine d'aeronef comprenant une valve d'admission / d'echappement a tournant spherique
CN104234869A (zh) * 2014-06-27 2014-12-24 吴润秀 气流隔热保温航天冲压发动机
FR3032025B1 (fr) 2015-01-26 2018-06-15 Safran Module de combustion a volume constant pour une turbomachine
FR3037384B1 (fr) 2015-06-11 2017-06-23 Turbomeca Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion
CN105066175B (zh) * 2015-08-31 2017-03-29 华能国际电力股份有限公司 一种旋转等容增压燃烧室
FR3092615B1 (fr) 2019-02-13 2021-01-22 Safran Aircraft Engines module de combustion CVC pour turbomachine d’aéronef comprenant des sous-ensembles de chambres indépendants
FR3098859B1 (fr) * 2019-07-15 2023-04-28 Safran Aircraft Engines Chambre de combustion de turbomachine a volume constant
US11662097B2 (en) 2020-10-13 2023-05-30 Venture Aerospace, Llc Jet engine with toroidal air stream combustion

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE548631C (de) * 1930-07-31 1932-04-15 E H Hans Holzwarth Dr Ing Betriebsverfahren fuer Verpuffungskammern, insbesondere fuer Brennkraftturbinen
US2623355A (en) * 1946-04-30 1952-12-30 Boulet Georges Hot pressurized gas producing means
DE947655C (de) * 1952-06-15 1956-08-23 Schmidt Paul Ventil fuer einen Brennraum mit periodisch wiederholten angenaeherten Gleichraumverbrennungen, insbesondere fuer Strahltriebwerke
FR2562199B3 (fr) * 1984-03-28 1986-08-08 Messerschmitt Boelkow Blohm Dispositif a valve pour la commande de l'ecoulement des fluides, en particulier pour le dosage des quantites de gaz riches en combustibles penetrant dans la chambre de combustion de statoreacteurs-fusees
US5110047A (en) * 1989-08-21 1992-05-05 Moog Inc. Vane-type nozzle(s) for varying the magnitude and direction of a thrust vector, and methods of operating same
GB2377257B (en) 2001-07-06 2004-09-01 Hubert Michael Benians Compound gas turbine engines and methods of operation thereof
FR2829528B1 (fr) * 2001-09-07 2004-02-27 Bernard Gilbert Macarez Pulsomoteur-turbomoteur a impulsion-turbine a gaz a chambre de combustion impulsionnelle et a detente de bouffees
GB0613781D0 (en) * 2006-07-12 2006-08-23 Rolls Royce Plc Flow modulation method and apparatus
US7891164B2 (en) * 2006-10-31 2011-02-22 General Electric Company Inlet airflow management system for a pulse detonation engine for supersonic applications
FR2941496A1 (fr) 2009-01-27 2010-07-30 Michel Aguilar Turbomachine a combustion isochore, detente totale et effet statoreacteur pulse

Also Published As

Publication number Publication date
US20120017563A1 (en) 2012-01-26
FR2945316A1 (fr) 2010-11-12
US8925296B2 (en) 2015-01-06
CA2748891A1 (fr) 2010-08-05
WO2010086091A1 (fr) 2010-08-05
EP2391802A1 (fr) 2011-12-07
FR2945316B1 (fr) 2013-01-04

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Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law

Free format text: REFERENTE A 6A ANUIDADE.

B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2384 DE 13-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.