FR3006715B1 - Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles - Google Patents

Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles

Info

Publication number
FR3006715B1
FR3006715B1 FR1355279A FR1355279A FR3006715B1 FR 3006715 B1 FR3006715 B1 FR 3006715B1 FR 1355279 A FR1355279 A FR 1355279A FR 1355279 A FR1355279 A FR 1355279A FR 3006715 B1 FR3006715 B1 FR 3006715B1
Authority
FR
France
Prior art keywords
thrust inverter
turbojet nacelle
grids fixed
mobile hoods
hoods
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
FR1355279A
Other languages
English (en)
Other versions
FR3006715A1 (fr
Inventor
Guy Bernard Vauchel
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.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
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 Aircelle SA filed Critical Aircelle SA
Priority to FR1355279A priority Critical patent/FR3006715B1/fr
Priority to CA2908678A priority patent/CA2908678A1/fr
Priority to PCT/FR2014/051349 priority patent/WO2014195646A1/fr
Priority to EP14733272.0A priority patent/EP3004614A1/fr
Publication of FR3006715A1 publication Critical patent/FR3006715A1/fr
Application granted granted Critical
Publication of FR3006715B1 publication Critical patent/FR3006715B1/fr
Priority to US14/950,479 priority patent/US20160076484A1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • F02K1/625—Reversing jet main flow by blocking the rearward discharge by means of flaps the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/34—Arrangement of components translated

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)
FR1355279A 2013-06-07 2013-06-07 Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles Expired - Fee Related FR3006715B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1355279A FR3006715B1 (fr) 2013-06-07 2013-06-07 Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles
CA2908678A CA2908678A1 (fr) 2013-06-07 2014-06-05 Inverseur de poussee d'une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles
PCT/FR2014/051349 WO2014195646A1 (fr) 2013-06-07 2014-06-05 Inverseur de poussée d'une nacelle de turboréacteur, comprenant des grilles fixées aux capots mobiles
EP14733272.0A EP3004614A1 (fr) 2013-06-07 2014-06-05 Inverseur de poussée d'une nacelle de turboréacteur, comprenant des grilles fixées aux capots mobiles
US14/950,479 US20160076484A1 (en) 2013-06-07 2015-11-24 Turbojet engine nacelle thrust reverser comprising cascades secured to the mobile cowls

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1355279A FR3006715B1 (fr) 2013-06-07 2013-06-07 Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles

Publications (2)

Publication Number Publication Date
FR3006715A1 FR3006715A1 (fr) 2014-12-12
FR3006715B1 true FR3006715B1 (fr) 2015-06-05

Family

ID=49003888

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1355279A Expired - Fee Related FR3006715B1 (fr) 2013-06-07 2013-06-07 Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles fixees aux capots mobiles

Country Status (4)

Country Link
EP (1) EP3004614A1 (fr)
CA (1) CA2908678A1 (fr)
FR (1) FR3006715B1 (fr)
WO (1) WO2014195646A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10344709B2 (en) * 2015-09-10 2019-07-09 Honeywell International Inc. System and method for reducing idle thrust in a translating cowl thrust reverser

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3347467A (en) * 1963-08-07 1967-10-17 Gen Electric Combination jet exhaust nozzle and thrust reverser
US3500645A (en) * 1968-04-10 1970-03-17 Rohr Corp Thrust reverser
GB2156004A (en) * 1984-03-15 1985-10-02 Gen Electric Thrust modulation device for a gas turbine engine
US4807434A (en) 1987-12-21 1989-02-28 The Boeing Company Thrust reverser for high bypass jet engines
US5228641A (en) 1991-08-15 1993-07-20 Rohr, Inc. Cascade type aircraft engine thrust reverser with hidden link actuator
US8201390B2 (en) * 2007-12-12 2012-06-19 Spirit Aerosystems, Inc. Partial cascade thrust reverser

Also Published As

Publication number Publication date
EP3004614A1 (fr) 2016-04-13
CA2908678A1 (fr) 2014-12-11
FR3006715A1 (fr) 2014-12-12
WO2014195646A1 (fr) 2014-12-11

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Legal Events

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Year of fee payment: 3

ST Notification of lapse

Effective date: 20170228