FR3075880B1 - Dispositif d'accouplement de deux arbres de turbomachine d'aeronef - Google Patents
Dispositif d'accouplement de deux arbres de turbomachine d'aeronef Download PDFInfo
- Publication number
- FR3075880B1 FR3075880B1 FR1763048A FR1763048A FR3075880B1 FR 3075880 B1 FR3075880 B1 FR 3075880B1 FR 1763048 A FR1763048 A FR 1763048A FR 1763048 A FR1763048 A FR 1763048A FR 3075880 B1 FR3075880 B1 FR 3075880B1
- Authority
- FR
- France
- Prior art keywords
- annular
- flanges
- shafts
- radial wall
- aircraft turbomachine
- 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
- 230000008878 coupling Effects 0.000 title abstract 2
- 238000010168 coupling process Methods 0.000 title abstract 2
- 238000005859 coupling reaction Methods 0.000 title abstract 2
Classifications
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- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/026—Shaft to shaft connections
-
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
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- 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
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
-
- 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
- F05D2260/40—Transmission of power
- F05D2260/403—Transmission of power through the shape of the drive components
- F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
- F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
-
- 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
- F05D2260/60—Fluid transfer
- F05D2260/609—Deoiling or demisting
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- General Details Of Gearings (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Abstract
Dispositif (20) d'accouplement de deux arbres (8a, 8b) de turbomachine d'aéronef, comportant des premier et second arbres s'étendant autour d'un même axe, le premier arbre comprenant une portion annulaire d'extrémité (8ab) qui a en section une forme sensiblement en L et qui comporte une première paroi radiale (22) comportant à sa périphérie externe une première bride annulaire (24) de raccordement, le second arbre comprenant une portion annulaire d'extrémité (8ba) qui a en section une forme sensiblement en L et qui comporte une seconde paroi radiale (26) sensiblement parallèle à ladite première paroi radiale et comportant à sa périphérie externe une seconde bride annulaire (28) de raccordement à ladite première bride annulaire, lesdites première et seconde brides étant traversées par des vis (32) axiales de serrage axial et de fixation des brides, caractérisé en ce que lesdites vis (32) sont logées dans un capotage annulaire (38) recouvrant au moins en partie lesdites brides (24, 28).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1763048A FR3075880B1 (fr) | 2017-12-22 | 2017-12-22 | Dispositif d'accouplement de deux arbres de turbomachine d'aeronef |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1763048A FR3075880B1 (fr) | 2017-12-22 | 2017-12-22 | Dispositif d'accouplement de deux arbres de turbomachine d'aeronef |
FR1763048 | 2017-12-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3075880A1 FR3075880A1 (fr) | 2019-06-28 |
FR3075880B1 true FR3075880B1 (fr) | 2020-09-04 |
Family
ID=62092005
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1763048A Active FR3075880B1 (fr) | 2017-12-22 | 2017-12-22 | Dispositif d'accouplement de deux arbres de turbomachine d'aeronef |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3075880B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3128483A1 (fr) * | 2021-10-27 | 2023-04-28 | Safran Aircraft Engines | Rotor de turbomachine comprenant un cache couvrant des boulons de fixation |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5211541A (en) * | 1991-12-23 | 1993-05-18 | General Electric Company | Turbine support assembly including turbine heat shield and bolt retainer assembly |
GB9828812D0 (en) * | 1998-12-29 | 1999-02-17 | Rolls Royce Plc | Gas turbine nose cone assembly |
GB2489727B (en) * | 2011-04-07 | 2013-07-10 | Rolls Royce Plc | Windage shield |
US10030519B2 (en) * | 2015-10-26 | 2018-07-24 | Rolls-Royce Corporation | System and method to retain a turbine cover plate between nested turbines with a tie bolt and spanner nut |
-
2017
- 2017-12-22 FR FR1763048A patent/FR3075880B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3075880A1 (fr) | 2019-06-28 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20190628 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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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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PLFP | Fee payment |
Year of fee payment: 7 |