FR3099463B1 - DEVICE FOR MOUNTING AN AXLE ON A SCREED FOR AN AIRCRAFT TURBOMACHINE - Google Patents

DEVICE FOR MOUNTING AN AXLE ON A SCREED FOR AN AIRCRAFT TURBOMACHINE Download PDF

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Publication number
FR3099463B1
FR3099463B1 FR1908857A FR1908857A FR3099463B1 FR 3099463 B1 FR3099463 B1 FR 3099463B1 FR 1908857 A FR1908857 A FR 1908857A FR 1908857 A FR1908857 A FR 1908857A FR 3099463 B1 FR3099463 B1 FR 3099463B1
Authority
FR
France
Prior art keywords
axle
bores
aircraft turbomachine
mounting
screed
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
Application number
FR1908857A
Other languages
French (fr)
Other versions
FR3099463A1 (en
Inventor
Ludovic Michaël Laurent Toupet
Giovanni Ingrassia
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1908857A priority Critical patent/FR3099463B1/en
Publication of FR3099463A1 publication Critical patent/FR3099463A1/en
Application granted granted Critical
Publication of FR3099463B1 publication Critical patent/FR3099463B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/045—Pivotal connections with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin
    • 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
    • F16C43/00—Assembling bearings
    • F16C43/02—Assembling sliding-contact bearings
    • 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
    • F16C2226/14—Force connections, e.g. clamping by shrink fit, i.e. heating and shrinking part to allow assembly
    • 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
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • 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
    • F16C2360/00—Engines or pumps
    • F16C2360/23—Gas turbine engines
    • 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
    • F16C33/02—Parts of sliding-contact bearings
    • F16C33/04—Brasses; Bushes; Linings
    • F16C33/06—Sliding surface mainly made of metal
    • F16C33/08—Attachment of brasses, bushes or linings to the bearing housing

Abstract

L’invention concerne un dispositif (100) de montage d’un axe (1) sur une chape (2) pour une turbomachine d’aéronef, comportant une chape (2) comportant deux oreilles (3, 4) comprenant des alésages de passage (5, 6) de l’axe (1), une première douille (7) engagée de manière ajustée et coulissante dans un premier des alésages (5, 6), une seconde douille (8) engagée de manière ajustée et coulissante dans un second des alésages (5, 6), l’axe (1) comportant une tête (10) serrée axialement contre la première douille (7) et un écrou serré (11) axialement contre la seconde douille (8). Selon l’invention, les alésages (5, 6) ont des diamètres internes (Di1, Di2) différents et le premier alésage (5) comprend un épaulement annulaire (15) ayant un diamètre interne (Di15) inférieur au diamètre interne (Di1) de cet alésage (5). L’invention concerne aussi une turbomachine d’aéronef, comportant au moins un tel dispositif (100). Figure pour l’abrégé : Figure 1The invention relates to a device (100) for mounting an axle (1) on a yoke (2) for an aircraft turbomachine, comprising a yoke (2) comprising two lugs (3, 4) comprising passage bores. (5, 6) of the axle (1), a first bush (7) fitted and slidably engaged in a first of the bores (5, 6), a second bush (8) fitted and slidably engaged in a second of the bores (5, 6), the axis (1) comprising a head (10) clamped axially against the first sleeve (7) and a nut tightened (11) axially against the second sleeve (8). According to the invention, the bores (5, 6) have different internal diameters (Di1, Di2) and the first bore (5) comprises an annular shoulder (15) having an internal diameter (Di15) less than the internal diameter (Di1) of this bore (5). The invention also relates to an aircraft turbomachine, comprising at least one such device (100). Figure for the abstract: Figure 1

FR1908857A 2019-08-01 2019-08-01 DEVICE FOR MOUNTING AN AXLE ON A SCREED FOR AN AIRCRAFT TURBOMACHINE Active FR3099463B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1908857A FR3099463B1 (en) 2019-08-01 2019-08-01 DEVICE FOR MOUNTING AN AXLE ON A SCREED FOR AN AIRCRAFT TURBOMACHINE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1908857 2019-08-01
FR1908857A FR3099463B1 (en) 2019-08-01 2019-08-01 DEVICE FOR MOUNTING AN AXLE ON A SCREED FOR AN AIRCRAFT TURBOMACHINE

Publications (2)

Publication Number Publication Date
FR3099463A1 FR3099463A1 (en) 2021-02-05
FR3099463B1 true FR3099463B1 (en) 2021-07-16

Family

ID=67999960

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1908857A Active FR3099463B1 (en) 2019-08-01 2019-08-01 DEVICE FOR MOUNTING AN AXLE ON A SCREED FOR AN AIRCRAFT TURBOMACHINE

Country Status (1)

Country Link
FR (1) FR3099463B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2602822A (en) * 2021-01-15 2022-07-20 Airbus Operations Ltd A pin joint assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6076423A (en) * 1998-02-27 2000-06-20 United Technologies Corporation Bellcrank mechanism
KR100894532B1 (en) * 2005-01-25 2009-04-24 가부시키가이샤 고마쓰 세이사쿠쇼 Bearing device
GB0609712D0 (en) * 2006-05-16 2006-06-28 Airbus Uk Ltd Bearing failure indicator
FR2907177B1 (en) * 2006-10-13 2009-12-04 Snecma ASSEMBLING A ROTULATING DEVICE ON AN ANGLE RETRACTING CAP, A CONTROL SYSTEM FOR A VARIABLE TIMING RECTIFIER COMPRISING IT, AND AN AIRCRAFT ENGINE BEING MUNIED
FR2923460B1 (en) 2007-11-12 2010-05-14 Snecma ASSEMBLING A SUSPENSION MEMBER OF A TURBOMOTEUR
GB0913506D0 (en) * 2009-08-04 2009-09-16 Airbus Operations Ltd Retaining nut

Also Published As

Publication number Publication date
FR3099463A1 (en) 2021-02-05

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