FR2929655B1 - Nacelle de turboreacteur a double flux - Google Patents

Nacelle de turboreacteur a double flux

Info

Publication number
FR2929655B1
FR2929655B1 FR0801828A FR0801828A FR2929655B1 FR 2929655 B1 FR2929655 B1 FR 2929655B1 FR 0801828 A FR0801828 A FR 0801828A FR 0801828 A FR0801828 A FR 0801828A FR 2929655 B1 FR2929655 B1 FR 2929655B1
Authority
FR
France
Prior art keywords
double flow
nacelle
flow turboreactor
turboreactor nacelle
double
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.)
Active
Application number
FR0801828A
Other languages
English (en)
Other versions
FR2929655A1 (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 FR0801828A priority Critical patent/FR2929655B1/fr
Priority to PCT/FR2009/050544 priority patent/WO2009125157A2/fr
Publication of FR2929655A1 publication Critical patent/FR2929655A1/fr
Application granted granted Critical
Publication of FR2929655B1 publication Critical patent/FR2929655B1/fr
Active 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
    • F02K1/64—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
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud
    • 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)
  • Exhaust Gas After Treatment (AREA)
FR0801828A 2008-04-02 2008-04-02 Nacelle de turboreacteur a double flux Active FR2929655B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0801828A FR2929655B1 (fr) 2008-04-02 2008-04-02 Nacelle de turboreacteur a double flux
PCT/FR2009/050544 WO2009125157A2 (fr) 2008-04-02 2009-03-31 Nacelle de turboréacteur à double flux

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0801828A FR2929655B1 (fr) 2008-04-02 2008-04-02 Nacelle de turboreacteur a double flux

Publications (2)

Publication Number Publication Date
FR2929655A1 FR2929655A1 (fr) 2009-10-09
FR2929655B1 true FR2929655B1 (fr) 2010-04-16

Family

ID=39968115

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0801828A Active FR2929655B1 (fr) 2008-04-02 2008-04-02 Nacelle de turboreacteur a double flux

Country Status (2)

Country Link
FR (1) FR2929655B1 (fr)
WO (1) WO2009125157A2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103201489A (zh) * 2010-10-21 2013-07-10 萨热姆防务安全公司 用于飞机推进单元的致动系统

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3087498B1 (fr) * 2018-10-22 2021-03-05 Airbus Operations Sas Turboreacteur comportant une nacelle equipee d’un systeme d’inversion de poussee mobile en translation et d’un carter de soufflante equipe de supports

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996012881A1 (fr) * 1994-10-20 1996-05-02 United Technologies Corporation Buse d'evacuation d'air de ventilation, a section de superficie variable
JPH09195853A (ja) * 1995-12-14 1997-07-29 United Technol Corp <Utc> 可変面積ファンエキゾーストノズル
US5806302A (en) * 1996-09-24 1998-09-15 Rohr, Inc. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
US7174704B2 (en) * 2004-07-23 2007-02-13 General Electric Company Split shroud exhaust nozzle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103201489A (zh) * 2010-10-21 2013-07-10 萨热姆防务安全公司 用于飞机推进单元的致动系统

Also Published As

Publication number Publication date
FR2929655A1 (fr) 2009-10-09
WO2009125157A3 (fr) 2009-12-03
WO2009125157A2 (fr) 2009-10-15

Similar Documents

Publication Publication Date Title
FR2929998B1 (fr) Nacelle de turboreacteur a double flux
FR2908461B1 (fr) Generateur de secours a turboreacteur a double flux
IT1393131B1 (it) Controvento a ingobbamento limitato
BRPI0918482A2 (pt) turbina eólica
BRPI0915747A2 (pt) conversor de fluxo
BRPI0915538A2 (pt) turbina eólica
AT507394A3 (de) Windkraftanlage
BRPI0917179A2 (pt) turbina
DK2429882T3 (da) Forbindelsesanordning
DK2333163T3 (da) Offshore-bygningskonstruktion
BRPI0915880A2 (pt) turbina hidráulica
BRPI0922070A2 (pt) turbina.
GB2461286B (en) Fluid turbine
FR2925545B1 (fr) Nacelle de securite
FI20080510A0 (fi) Tuulivoimala
FR2913664B1 (fr) Nacelle pour turboreacteur double flux
FR2953810B1 (fr) Nacelle de turboreacteur
IT1396671B1 (it) Scambiatore a microcanali
FR2935762B1 (fr) Eolienne
FR2929654B1 (fr) Nacelle de turboreacteur a double flux
BRPI0920293A2 (pt) nacela
FR2929655B1 (fr) Nacelle de turboreacteur a double flux
DK2325483T3 (da) Indretning med en modulær nacelle med en udstråler
FR2933753B1 (fr) Eolienne
ITMI20080225U1 (it) Altalena a dondolo

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

CD Change of name or company name

Owner name: SAFRAN NACELLES, FR

Effective date: 20180125

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17