FR3125319B1 - MECHANICAL ASSEMBLY AND MECHANICAL REDUCER OF AIRCRAFT TURBOMACHINE COMPRISING SUCH AN ASSEMBLY - Google Patents
MECHANICAL ASSEMBLY AND MECHANICAL REDUCER OF AIRCRAFT TURBOMACHINE COMPRISING SUCH AN ASSEMBLY Download PDFInfo
- Publication number
- FR3125319B1 FR3125319B1 FR2107720A FR2107720A FR3125319B1 FR 3125319 B1 FR3125319 B1 FR 3125319B1 FR 2107720 A FR2107720 A FR 2107720A FR 2107720 A FR2107720 A FR 2107720A FR 3125319 B1 FR3125319 B1 FR 3125319B1
- Authority
- FR
- France
- Prior art keywords
- assembly
- mechanical
- ring
- nut
- shoulder
- 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
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- 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
- F02C7/06—Arrangements of bearings; Lubricating
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/58—Raceways; Race rings
- F16C33/583—Details of specific parts of races
- F16C33/586—Details of specific parts of races outside the space between the races, e.g. end faces or bore of inner ring
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
- F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
- F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
- F16C35/063—Fixing them on the shaft
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- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
- F16C2226/10—Force connections, e.g. clamping
- F16C2226/12—Force connections, e.g. clamping by press-fit, e.g. plug-in
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
- F16C2226/10—Force connections, e.g. clamping
- F16C2226/16—Force connections, e.g. clamping by wedge action, e.g. by tapered or conical parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
- F16C2226/50—Positive connections
- F16C2226/60—Positive connections with threaded parts, e.g. bolt and nut connections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2226/00—Joining parts; Fastening; Assembling or mounting parts
- F16C2226/50—Positive connections
- F16C2226/70—Positive connections with complementary interlocking parts
- F16C2226/72—Positive connections with complementary interlocking parts with bayonet joints, i.e. parts are rotated to create positive interlock
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/08—General details of gearing of gearings with members having orbital motion
- F16H2057/085—Bearings for orbital gears
Abstract
Ensemble mécanique (150) pour une turbomachine d’aéronef, cet ensemble comportant : - une pièce (156) comportant un filetage externe (170) et une surface cylindrique externe (166) s’étendant autour d’un même axe (Y), - un palier à roulements (94) monté sur ladite surface (166), ce palier (94) comportant une bague interne (158) qui est configurée pour être frettée sur ladite surface (166) et qui est en appui sur un épaulement cylindrique (168) de ladite pièce (156), et - un écrou (152) comportant un filetage interne (185) et configuré pour être vissé sur ledit filetage (170) afin de bloquer axialement ladite bague interne (158) contre ledit épaulement (168), ledit écrou (152) comportant un diamètre interne inférieur au diamètre externe (Dex) de ladite bague (158), ledit écrou (152) et ledit épaulement (168) étant situés d’un même côté de la bague (158). Figure pour l'abrégé : Figure 6Mechanical assembly (150) for an aircraft turbomachine, this assembly comprising: - a part (156) comprising an external thread (170) and an external cylindrical surface (166) extending around the same axis (Y), - a rolling bearing (94) mounted on said surface (166), this bearing (94) comprising an inner ring (158) which is configured to be shrunk on said surface (166) and which bears on a cylindrical shoulder ( 168) of said part (156), and - a nut (152) comprising an internal thread (185) and configured to be screwed onto said thread (170) in order to axially lock said internal ring (158) against said shoulder (168) , said nut (152) having an internal diameter smaller than the external diameter (Dex) of said ring (158), said nut (152) and said shoulder (168) being located on the same side of the ring (158). Figure for abstract: Figure 6
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2107720A FR3125319B1 (en) | 2021-07-16 | 2021-07-16 | MECHANICAL ASSEMBLY AND MECHANICAL REDUCER OF AIRCRAFT TURBOMACHINE COMPRISING SUCH AN ASSEMBLY |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2107720 | 2021-07-16 | ||
FR2107720A FR3125319B1 (en) | 2021-07-16 | 2021-07-16 | MECHANICAL ASSEMBLY AND MECHANICAL REDUCER OF AIRCRAFT TURBOMACHINE COMPRISING SUCH AN ASSEMBLY |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3125319A1 FR3125319A1 (en) | 2023-01-20 |
FR3125319B1 true FR3125319B1 (en) | 2023-06-09 |
Family
ID=77180290
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2107720A Active FR3125319B1 (en) | 2021-07-16 | 2021-07-16 | MECHANICAL ASSEMBLY AND MECHANICAL REDUCER OF AIRCRAFT TURBOMACHINE COMPRISING SUCH AN ASSEMBLY |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3125319B1 (en) |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2942284B1 (en) | 2009-02-16 | 2011-03-04 | Snecma | LUBRICATION AND COOLING OF AN EPICYCLOIDAL GEAR TRAIN REDUCER |
FR2987416B1 (en) | 2012-02-23 | 2015-09-04 | Snecma | DEVICE FOR LUBRICATING AN EPICYCLOIDAL REDUCER. |
FR3008463B1 (en) | 2013-07-10 | 2015-08-07 | Hispano Suiza Sa | COMPACT DRIVE HOUSING STRUCTURE FOR AIRCRAFT TURBOMACHINE |
FR3008462B1 (en) | 2013-07-10 | 2016-12-23 | Hispano Suiza Sa | INTEGRATION OF A GEAR TRAIN IN A DRIVE GEAR FOR DRIVE HOUSING FOR TURBOMACHINE |
PL406855A1 (en) * | 2014-01-15 | 2015-07-20 | General Electric Company | An unit immobilizing a bearing and method for assembling it |
FR3041054B1 (en) | 2015-09-15 | 2017-09-15 | Hispano-Suiza | OIL SUPPLY DEVICE FOR AN EPICYCLOIDAL TRAIN REDUCER. |
US20170089218A1 (en) * | 2015-09-25 | 2017-03-30 | General Electric Company | Double row cylindrical roller bearing with high length to diameter ratio rollers |
US10234018B2 (en) * | 2015-10-19 | 2019-03-19 | General Electric Company | Planet gearbox with cylindrical roller bearing with under race lube scheme |
-
2021
- 2021-07-16 FR FR2107720A patent/FR3125319B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3125319A1 (en) | 2023-01-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20230120 |
|
PLFP | Fee payment |
Year of fee payment: 3 |