FR2961484B1 - Manche d?entree d?air pour nacelle de turboreacteur - Google Patents
Manche d?entree d?air pour nacelle de turboreacteurInfo
- Publication number
- FR2961484B1 FR2961484B1 FR1054873A FR1054873A FR2961484B1 FR 2961484 B1 FR2961484 B1 FR 2961484B1 FR 1054873 A FR1054873 A FR 1054873A FR 1054873 A FR1054873 A FR 1054873A FR 2961484 B1 FR2961484 B1 FR 2961484B1
- Authority
- FR
- France
- Prior art keywords
- air inlet
- inlet handle
- turboreactor
- nacelle
- turboreactor nacelle
- 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
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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- 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
- 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
-
- 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
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054873A FR2961484B1 (fr) | 2010-06-18 | 2010-06-18 | Manche d?entree d?air pour nacelle de turboreacteur |
US13/704,824 US20130087635A1 (en) | 2010-06-18 | 2011-06-15 | Air inlet duct for a turbojet nacelle |
CN2011800299855A CN102947182A (zh) | 2010-06-18 | 2011-06-15 | 涡轮喷气发动机短舱的进气道 |
PCT/FR2011/051362 WO2011157953A1 (fr) | 2010-06-18 | 2011-06-15 | Manche d'entree d'air pour nacelle de turboreacteur |
GB1300867.7A GB2494843A (en) | 2010-06-18 | 2011-06-15 | Air inlet duct for a turbojet nacelle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1054873A FR2961484B1 (fr) | 2010-06-18 | 2010-06-18 | Manche d?entree d?air pour nacelle de turboreacteur |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2961484A1 FR2961484A1 (fr) | 2011-12-23 |
FR2961484B1 true FR2961484B1 (fr) | 2013-01-04 |
Family
ID=43563523
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1054873A Active FR2961484B1 (fr) | 2010-06-18 | 2010-06-18 | Manche d?entree d?air pour nacelle de turboreacteur |
Country Status (5)
Country | Link |
---|---|
US (1) | US20130087635A1 (fr) |
CN (1) | CN102947182A (fr) |
FR (1) | FR2961484B1 (fr) |
GB (1) | GB2494843A (fr) |
WO (1) | WO2011157953A1 (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2907551A1 (fr) * | 2012-07-31 | 2014-02-06 | General Electric Company | Capot central en cmc et procede de fabrication |
US20160356180A1 (en) * | 2015-06-03 | 2016-12-08 | The Boeing Company | Nacelle inlet having an angle or curved aft bulkhead |
US10196937B2 (en) * | 2015-12-30 | 2019-02-05 | General Electric Company | Method and system for improving structural characteristics of composite component corners |
FR3057618A1 (fr) * | 2016-10-17 | 2018-04-20 | Airbus | Nacelle d'un turboreacteur comportant un volet inverseur |
FR3060650B1 (fr) * | 2016-12-20 | 2019-05-31 | Airbus Operations | Structure d'entree d'air pour une nacelle d'aeronef |
FR3095416B1 (fr) * | 2019-04-26 | 2021-04-23 | Safran Nacelles | Entrée d’air de nacelle de turboréacteur |
CN111024402B (zh) * | 2019-12-13 | 2021-05-07 | 湖南汉能科技有限公司 | 一种航空发动机试验台安装系统 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2149344A (en) | 1935-03-22 | 1939-03-07 | Du Pont | Apparatus and process for the study of plating solutions |
JPS62124279A (ja) * | 1985-11-22 | 1987-06-05 | Mitsubishi Rayon Co Ltd | 繊維強化複合材料の表面処理法 |
US5252160A (en) * | 1990-11-15 | 1993-10-12 | Auto Air Composites, Inc. | Method of manufacturing a metal/composite spinner cone |
US5881972A (en) * | 1997-03-05 | 1999-03-16 | United Technologies Corporation | Electroformed sheath and airfoiled component construction |
NL1025744C2 (nl) * | 2004-03-16 | 2005-01-18 | Stork Fokker Aesp Bv | Laminaat met verwarmingselement. |
US7923668B2 (en) * | 2006-02-24 | 2011-04-12 | Rohr, Inc. | Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
FR2913062A1 (fr) * | 2007-02-22 | 2008-08-29 | Aircelle Sa | Nacelle de turboreacteur a ecoulement ameliore |
FR2926537B1 (fr) * | 2008-01-18 | 2010-02-12 | Aircelle Sa | Systeme de verrouillage pour structure d'entree d'air d'une nacelle de turboreacteur |
FR2934247A1 (fr) | 2008-07-25 | 2010-01-29 | Snecma | Nacelle de turboreacteur. |
US8092169B2 (en) * | 2008-09-16 | 2012-01-10 | United Technologies Corporation | Integrated inlet fan case |
US8197191B2 (en) * | 2009-04-14 | 2012-06-12 | Rohr, Inc. | Inlet section of an aircraft engine nacelle |
-
2010
- 2010-06-18 FR FR1054873A patent/FR2961484B1/fr active Active
-
2011
- 2011-06-15 GB GB1300867.7A patent/GB2494843A/en not_active Withdrawn
- 2011-06-15 US US13/704,824 patent/US20130087635A1/en not_active Abandoned
- 2011-06-15 CN CN2011800299855A patent/CN102947182A/zh active Pending
- 2011-06-15 WO PCT/FR2011/051362 patent/WO2011157953A1/fr active Application Filing
Also Published As
Publication number | Publication date |
---|---|
GB2494843A (en) | 2013-03-20 |
GB201300867D0 (en) | 2013-03-06 |
FR2961484A1 (fr) | 2011-12-23 |
US20130087635A1 (en) | 2013-04-11 |
CN102947182A (zh) | 2013-02-27 |
WO2011157953A1 (fr) | 2011-12-22 |
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Legal Events
Date | Code | Title | Description |
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Year of fee payment: 6 |
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Year of fee payment: 8 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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Year of fee payment: 9 |
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