IT201700067602A1 - Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione. - Google Patents

Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione.

Info

Publication number
IT201700067602A1
IT201700067602A1 IT102017000067602A IT201700067602A IT201700067602A1 IT 201700067602 A1 IT201700067602 A1 IT 201700067602A1 IT 102017000067602 A IT102017000067602 A IT 102017000067602A IT 201700067602 A IT201700067602 A IT 201700067602A IT 201700067602 A1 IT201700067602 A1 IT 201700067602A1
Authority
IT
Italy
Prior art keywords
aircraft
realization
procedure
air intake
engine gondola
Prior art date
Application number
IT102017000067602A
Other languages
English (en)
Inventor
Luca Bottero
Massimo Gregori
Alberto Midali
Original Assignee
Leonardo Spa
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 Leonardo Spa filed Critical Leonardo Spa
Priority to IT102017000067602A priority Critical patent/IT201700067602A1/it
Priority to EP18178051.1A priority patent/EP3418199B1/en
Priority to ES18178051T priority patent/ES2927469T3/es
Priority to US16/011,305 priority patent/US11427342B2/en
Publication of IT201700067602A1 publication Critical patent/IT201700067602A1/it

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D15/00De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/045Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0233Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
IT102017000067602A 2017-06-19 2017-06-19 Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione. IT201700067602A1 (it)

Priority Applications (4)

Application Number Priority Date Filing Date Title
IT102017000067602A IT201700067602A1 (it) 2017-06-19 2017-06-19 Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione.
EP18178051.1A EP3418199B1 (en) 2017-06-19 2018-06-15 Air inlet for an aircraft engine nacelle and method of manufacturing such air inlet
ES18178051T ES2927469T3 (es) 2017-06-19 2018-06-15 Entrada de aire para una góndola de motor de aeronave y método de fabricación de tal entrada de aire
US16/011,305 US11427342B2 (en) 2017-06-19 2018-06-18 Air inlet for a nacelle for an aircraft and its process for manufacturing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT102017000067602A IT201700067602A1 (it) 2017-06-19 2017-06-19 Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione.

Publications (1)

Publication Number Publication Date
IT201700067602A1 true IT201700067602A1 (it) 2018-12-19

Family

ID=60182924

Family Applications (1)

Application Number Title Priority Date Filing Date
IT102017000067602A IT201700067602A1 (it) 2017-06-19 2017-06-19 Presa d'aria per gondola motore per un velivolo e relativo procedimento per la realizzazione.

Country Status (4)

Country Link
US (1) US11427342B2 (it)
EP (1) EP3418199B1 (it)
ES (1) ES2927469T3 (it)
IT (1) IT201700067602A1 (it)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10589869B2 (en) * 2018-07-25 2020-03-17 General Electric Company Nacelle inlet lip fuse structure
USD985426S1 (en) * 2020-09-04 2023-05-09 The Boeing Company Aerial vehicle

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080179448A1 (en) * 2006-02-24 2008-07-31 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
US20100199629A1 (en) * 2005-06-22 2010-08-12 Airbus France Systeme d'anti givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
US20150377128A1 (en) * 2012-12-27 2015-12-31 Alenia Aermacchi S.P.A. Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5702231A (en) * 1996-08-09 1997-12-30 The Boeing Company Apparatus and method for reducing noise emissions from a gas turbine engine inlet
US7588212B2 (en) * 2003-07-08 2009-09-15 Rohr Inc. Method and apparatus for noise abatement and ice protection of an aircraft engine nacelle inlet lip
FR2898868B1 (fr) * 2006-03-24 2008-12-12 Aircelle Sa Structure pour levre d'entree d'air de nacelle a degivrage electrique
FR2908738B1 (fr) * 2006-11-16 2009-12-04 Airbus France Bord d'attaque d'aeronef.
ITMI20071448A1 (it) * 2007-07-18 2009-01-19 Alenia Aermacchi Spa Procedimento di realizzazione di un pannello fonoassorbente per veicoli
EP2318683A2 (fr) * 2008-07-30 2011-05-11 Aircelle Panneau d'atténuation acoustique pour nacelle de moteur d'aéronef
US9010084B2 (en) * 2009-02-02 2015-04-21 Airbus Operations Sas Aircraft nacelle including an optimised acoustic processing system
US8197191B2 (en) * 2009-04-14 2012-06-12 Rohr, Inc. Inlet section of an aircraft engine nacelle
FR2976556B1 (fr) * 2011-06-17 2013-12-27 Airbus Operations Sas Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule
US8863893B2 (en) * 2011-11-17 2014-10-21 Spirit Aerosystems, Inc. Engine inlet varying impedance acoustic liner section
FR3013329B1 (fr) * 2013-11-15 2017-08-11 Aircelle Sa Dispositif de degivrage d’entree d’air de nacelle d’un moteur d’aeronef, procede de fabrication d’un tel dispositif de degivrage et nacelle de moteur d’aeronef equipe d’un tel dispositif de degivrage
US9604438B2 (en) * 2014-04-30 2017-03-28 The Boeing Company Methods and apparatus for noise attenuation in an engine nacelle
US9938852B2 (en) * 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9708072B2 (en) * 2014-04-30 2017-07-18 The Boeing Company Aircraft engine nacelle bulkheads and methods of assembling the same

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100199629A1 (en) * 2005-06-22 2010-08-12 Airbus France Systeme d'anti givrage et de degivrage de nacelle de moteur d'aeronef a tapis resistif
US20080179448A1 (en) * 2006-02-24 2008-07-31 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
US20150377128A1 (en) * 2012-12-27 2015-12-31 Alenia Aermacchi S.P.A. Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption

Also Published As

Publication number Publication date
US11427342B2 (en) 2022-08-30
EP3418199B1 (en) 2022-08-24
ES2927469T3 (es) 2022-11-07
US20180362178A1 (en) 2018-12-20
EP3418199A1 (en) 2018-12-26

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