FR2995038B1 - GAS TURBINE BLOWER HOUSING HAVING EQUIPMENT FASTENING BELT - Google Patents
GAS TURBINE BLOWER HOUSING HAVING EQUIPMENT FASTENING BELTInfo
- Publication number
- FR2995038B1 FR2995038B1 FR1258091A FR1258091A FR2995038B1 FR 2995038 B1 FR2995038 B1 FR 2995038B1 FR 1258091 A FR1258091 A FR 1258091A FR 1258091 A FR1258091 A FR 1258091A FR 2995038 B1 FR2995038 B1 FR 2995038B1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- blower housing
- fastening belt
- turbine blower
- equipment fastening
- 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
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
- F01D25/243—Flange connections; Bolting arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- F05D2240/00—Components
- F05D2240/90—Mounting on supporting structures or systems
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/292—Three-dimensional machined; miscellaneous tapered
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1258091A FR2995038B1 (en) | 2012-08-30 | 2012-08-30 | GAS TURBINE BLOWER HOUSING HAVING EQUIPMENT FASTENING BELT |
US14/012,299 US20140064957A1 (en) | 2012-08-30 | 2013-08-28 | Gas turbine fan casing having a belt for fastening equipment |
GB1315384.6A GB2507629A (en) | 2012-08-30 | 2013-08-29 | A gas turbine fan casing having a belt for fastening equipment. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1258091A FR2995038B1 (en) | 2012-08-30 | 2012-08-30 | GAS TURBINE BLOWER HOUSING HAVING EQUIPMENT FASTENING BELT |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2995038A1 FR2995038A1 (en) | 2014-03-07 |
FR2995038B1 true FR2995038B1 (en) | 2014-09-19 |
Family
ID=47003135
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1258091A Active FR2995038B1 (en) | 2012-08-30 | 2012-08-30 | GAS TURBINE BLOWER HOUSING HAVING EQUIPMENT FASTENING BELT |
Country Status (3)
Country | Link |
---|---|
US (1) | US20140064957A1 (en) |
FR (1) | FR2995038B1 (en) |
GB (1) | GB2507629A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2970715B1 (en) * | 2011-01-21 | 2014-10-17 | Snecma | MULTI-LAYER FABRIC FIBROUS STRUCTURE HAVING HOLLOW TUBULAR PART, MANUFACTURING METHOD AND COMPOSITE PIECE COMPRISING THE SAME |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE487116A (en) * | 1946-07-16 | |||
US2865167A (en) * | 1957-08-22 | 1958-12-23 | United Aircraft Corp | Inner cone attachment |
US4681353A (en) * | 1984-07-17 | 1987-07-21 | Pressure Science Incorporated | V-coupling for installation in narrow annular spaces |
US20010048048A1 (en) * | 1999-01-13 | 2001-12-06 | Brian L Riedel | Backside fitting attachment for nacelle acoustic panels |
US6607165B1 (en) * | 2002-06-28 | 2003-08-19 | General Electric Company | Aircraft engine mount with single thrust link |
US7611595B2 (en) * | 2006-02-01 | 2009-11-03 | Lockheed Martin Corporation | System, method, and apparatus for metallic-composite joint with compliant, non-corrosive interface |
FR2900979B1 (en) * | 2006-05-11 | 2008-06-27 | Airbus France Sas | AIRCRAFT ENGINE ASSEMBLY COMPRISING A GAS EJECTION CONE MOUNTED ON A CRANKCASE USING AN EXTERNAL JUNCTION FLANGE |
US8966754B2 (en) * | 2006-11-21 | 2015-03-03 | General Electric Company | Methods for reducing stress on composite structures |
US7871486B2 (en) * | 2006-11-21 | 2011-01-18 | General Electric Company | Methods for making structures having mounting flanges |
US7749927B2 (en) * | 2006-12-27 | 2010-07-06 | General Electric Company | Tethered corners and flanges and articles comprising the same |
FR2913053B1 (en) * | 2007-02-23 | 2009-05-22 | Snecma Sa | PROCESS FOR MANUFACTURING A GAS TURBINE CASE OF COMPOSITE MATERIAL AND CARTER THUS OBTAINED |
US8061977B2 (en) * | 2007-07-03 | 2011-11-22 | Siemens Energy, Inc. | Ceramic matrix composite attachment apparatus and method |
FR2920191B1 (en) * | 2007-08-23 | 2013-11-22 | Snecma | GAS TURBINE ENGINE WITH DRIVING MEANS FOR THE ACCESSORIES HOUSING AND METHOD OF MOUNTING THE SAME |
FR2923529B1 (en) * | 2007-11-09 | 2014-05-16 | Snecma | CONNECTION OF RADIAL ARMS TO A CIRCULAR VIROLE BY ILLUMINATION OF REPORTED PARTS |
FR2923542B1 (en) * | 2007-11-13 | 2014-02-07 | Snecma | CARTER FERRULE, CARTER PROVIDED WITH SUCH A BRACKET, DEVICE FOR FASTENING AN ACCESSORY HOUSING ON A SUCH CARTER AND TURBOMACHINE COMPRISING SUCH A CARTER |
FR2932233B1 (en) * | 2008-06-06 | 2012-09-28 | Aircelle Sa | CARTER FOR ROTOR OF TURBOMACHINE |
US8210908B2 (en) * | 2008-06-23 | 2012-07-03 | Flow International Corporation | Vented cutting head body for abrasive jet system |
GB0907582D0 (en) * | 2009-05-05 | 2009-06-10 | Rolls Royce Plc | A duct wall for a fan of a gas turbine engine |
US8721278B2 (en) * | 2010-08-02 | 2014-05-13 | Siemens Energy, Inc. | Exhaust manifold flange connection |
FR2970513B1 (en) * | 2011-01-14 | 2015-07-31 | Aircelle Sa | DEVICE FOR CONNECTING A FRAME FRONT TO A BLOWER HOUSING |
GB201103245D0 (en) * | 2011-02-25 | 2011-04-13 | Rolls Royce Plc | A joint assembly |
FR2979665B1 (en) * | 2011-09-02 | 2016-02-05 | Snecma | TIGHTENING DEVICE FOR TURBOMACHINE PARTS, INCLUDING AN ANNULAR CLOSURE WRENCH OPEN RADIALLY TO THE OUTSIDE |
US9840936B2 (en) * | 2012-02-16 | 2017-12-12 | United Technologies Corporation | Case with ballistic liner |
JP6018877B2 (en) * | 2012-10-25 | 2016-11-02 | 株式会社Ihi | Cylindrical case and manufacturing method of cylindrical case |
JP5945209B2 (en) * | 2012-10-25 | 2016-07-05 | 株式会社Ihi | Cylindrical case and manufacturing method of cylindrical case |
-
2012
- 2012-08-30 FR FR1258091A patent/FR2995038B1/en active Active
-
2013
- 2013-08-28 US US14/012,299 patent/US20140064957A1/en not_active Abandoned
- 2013-08-29 GB GB1315384.6A patent/GB2507629A/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB201315384D0 (en) | 2013-10-16 |
US20140064957A1 (en) | 2014-03-06 |
GB2507629A (en) | 2014-05-07 |
FR2995038A1 (en) | 2014-03-07 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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CD | Change of name or company name |
Owner name: SNECMA, FR Effective date: 20170713 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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PLFP | Fee payment |
Year of fee payment: 13 |