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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- 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
- F02C7/00—Features, 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- 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
- F02C7/00—Features, 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- 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
- F05D2260/00—Function
- F05D2260/96—Preventing, 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)
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)
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)
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)
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 |
-
2017
- 2017-06-19 IT IT102017000067602A patent/IT201700067602A1/it unknown
-
2018
- 2018-06-15 ES ES18178051T patent/ES2927469T3/es active Active
- 2018-06-15 EP EP18178051.1A patent/EP3418199B1/en active Active
- 2018-06-18 US US16/011,305 patent/US11427342B2/en active Active
Patent Citations (3)
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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