FR2687433B1 - INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING. - Google Patents

INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING.

Info

Publication number
FR2687433B1
FR2687433B1 FR9201693A FR9201693A FR2687433B1 FR 2687433 B1 FR2687433 B1 FR 2687433B1 FR 9201693 A FR9201693 A FR 9201693A FR 9201693 A FR9201693 A FR 9201693A FR 2687433 B1 FR2687433 B1 FR 2687433B1
Authority
FR
France
Prior art keywords
inverter component
propeller
modulated
feeding
modulated feeding
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.)
Expired - Fee Related
Application number
FR9201693A
Other languages
French (fr)
Other versions
FR2687433A1 (en
Inventor
Yves Ribaud
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.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
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 Office National dEtudes et de Recherches Aerospatiales ONERA filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Priority to FR9201693A priority Critical patent/FR2687433B1/en
Publication of FR2687433A1 publication Critical patent/FR2687433A1/en
Application granted granted Critical
Publication of FR2687433B1 publication Critical patent/FR2687433B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • 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
FR9201693A 1992-02-14 1992-02-14 INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING. Expired - Fee Related FR2687433B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9201693A FR2687433B1 (en) 1992-02-14 1992-02-14 INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9201693A FR2687433B1 (en) 1992-02-14 1992-02-14 INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING.

Publications (2)

Publication Number Publication Date
FR2687433A1 FR2687433A1 (en) 1993-08-20
FR2687433B1 true FR2687433B1 (en) 1994-05-06

Family

ID=9426655

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9201693A Expired - Fee Related FR2687433B1 (en) 1992-02-14 1992-02-14 INVERTER COMPONENT PROPELLER, WITH MODULATED FEEDING.

Country Status (1)

Country Link
FR (1) FR2687433B1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2561764C1 (en) * 2014-01-10 2015-09-10 Николай Борисович Болотин Hydrogen gas turbine engine
RU2554392C1 (en) * 2014-01-10 2015-06-27 Николай Борисович Болотин Hydrogen gas turbine engine
RU2552012C1 (en) * 2014-01-10 2015-06-10 Николай Борисович Болотин Hydrogen gas-turbine engine
RU2561773C1 (en) * 2014-01-29 2015-09-10 Николай Борисович Болотин Double-fuel air-jet engine
RU2553052C1 (en) * 2014-01-29 2015-06-10 Николай Борисович Болотин Hydrogen air-jet engine
RU2573438C1 (en) * 2014-08-07 2016-01-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Method of aircraft engine augmentation
RU2594091C1 (en) * 2015-01-12 2016-08-10 Николай Борисович Болотин Engine of hypersonic aircraft
RU2593573C1 (en) * 2015-01-12 2016-08-10 Николай Борисович Болотин Engine of hypersonic aircraft
RU2591361C1 (en) * 2015-01-13 2016-07-20 Николай Борисович Болотин Engine of hypersonic aircraft
RU2594828C1 (en) * 2015-01-19 2016-08-20 Николай Борисович Болотин Propulsion engine of supersonic aircraft
US11041463B1 (en) * 2015-02-11 2021-06-22 Raytheon Technologies Corporation Turbine engine structure with oxidizer enhanced mode
US10487780B2 (en) * 2016-11-14 2019-11-26 The Boeing Company System and method for increasing the efficiency of heating a cryogenic fluid flowing through a conduit
GB2584094B (en) * 2019-05-20 2022-01-26 Rolls Royce Plc Engine
EP3978736A1 (en) 2020-09-30 2022-04-06 Rolls-Royce plc Fuel delivery

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1288767A (en) * 1961-02-06 1962-03-30 Snecma Turbomachinery reactor
FR1496091A (en) * 1966-04-20 1967-09-29 Snecma Ejection nozzle for thrusters with several motor flows, in particular with two motor flows
US3938328A (en) * 1971-11-08 1976-02-17 The Boeing Company Multicycle engine
GB2126658B (en) * 1982-09-07 1986-07-02 Secr Defence Generation of power from liquid hydrogen
DE3617915C1 (en) * 1986-05-28 1987-09-17 Messerschmitt Boelkow Blohm Combination drive
FR2615903B1 (en) * 1987-05-26 1992-11-20 Onera (Off Nat Aerospatiale) AEROBIC HEAT ENGINE, PARTICULARLY FOR THE PROPULSION OF HYPERSONIC AIRCRAFT
DE3738703A1 (en) * 1987-05-27 1988-12-08 Mtu Muenchen Gmbh COMBINED, SWITCHABLE JET ENGINE FOR DRIVING PLANES AND SPACES
DE3909050C1 (en) * 1989-03-18 1990-08-16 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
FR2648517B1 (en) * 1989-06-14 1994-04-01 Snecma COMBINED TURBOFUSE STATOREACTOR WITH HEATER AND OPERATING METHOD THEREOF

Also Published As

Publication number Publication date
FR2687433A1 (en) 1993-08-20

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20071030