CN106460916B - 用于涡轮发动机的球形接头设备 - Google Patents

用于涡轮发动机的球形接头设备 Download PDF

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Publication number
CN106460916B
CN106460916B CN201580031494.2A CN201580031494A CN106460916B CN 106460916 B CN106460916 B CN 106460916B CN 201580031494 A CN201580031494 A CN 201580031494A CN 106460916 B CN106460916 B CN 106460916B
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CN
China
Prior art keywords
lug
axis
equipment
shaft
axially
Prior art date
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Active
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CN201580031494.2A
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English (en)
Chinese (zh)
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CN106460916A (zh
Inventor
尼古拉·马克·弗洛朗
马克·帕特里克·特斯尼尔
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Safran Aircraft Engines SAS
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SNECMA SAS
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Publication of CN106460916A publication Critical patent/CN106460916A/zh
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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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • F16C11/0614—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints the female part of the joint being open on two sides
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • 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
    • F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
    • F16C23/02—Sliding-contact bearings
    • F16C23/04—Sliding-contact bearings self-adjusting
    • F16C23/043—Sliding-contact bearings self-adjusting with spherical surfaces, e.g. spherical plain 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
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/02—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
    • F16C2229/00—Setting preload
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Vibration Prevention Devices (AREA)
CN201580031494.2A 2014-05-21 2015-05-07 用于涡轮发动机的球形接头设备 Active CN106460916B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1454559A FR3021373B1 (fr) 2014-05-21 2014-05-21 Dispositif d'articulation a rotule pour une turbomachine.
FRFR1454559 2014-05-21
PCT/FR2015/051222 WO2015177431A1 (fr) 2014-05-21 2015-05-07 Dispositif d'articulation à rotule pour une turbomachine

Publications (2)

Publication Number Publication Date
CN106460916A CN106460916A (zh) 2017-02-22
CN106460916B true CN106460916B (zh) 2019-08-13

Family

ID=51298811

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201580031494.2A Active CN106460916B (zh) 2014-05-21 2015-05-07 用于涡轮发动机的球形接头设备

Country Status (8)

Country Link
US (1) US10626913B2 (https=)
EP (1) EP3146218B1 (https=)
CN (1) CN106460916B (https=)
BR (1) BR112016027060B8 (https=)
CA (1) CA2949603C (https=)
FR (1) FR3021373B1 (https=)
RU (1) RU2669502C2 (https=)
WO (1) WO2015177431A1 (https=)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10598211B2 (en) * 2016-05-23 2020-03-24 United Technologies Corporation Spherical bearing sleeve configured with one or more discrete collars
US10570950B2 (en) * 2016-05-23 2020-02-25 United Technologies Corporation Spherical joint assembly with a spherical bearing between integral collars
FR3059645B1 (fr) 2016-12-02 2018-12-07 Safran Aircraft Engines Dispositif de suspension pour turbomachine
US10634092B2 (en) 2017-09-08 2020-04-28 United Technologies Corporation Linkage assembly preventing axial rotation of the link rod
FR3086925B1 (fr) * 2018-10-08 2020-09-11 Safran Aircraft Engines Ensemble de suspension pour une turbomachine
FR3091520A1 (fr) * 2019-01-09 2020-07-10 Airbus Operations (S.A.S.) Attache-moteur d’aéronef comprenant au moins un système d’immobilisation en translation d’un pion de cisaillement comportant une plaque d’obturation, procédé de montage de ladite attache-moteur et aéronef comprenant ladite attache-moteur
FR3108096B1 (fr) * 2020-03-10 2023-02-10 Airbus Operations Sas Attache moteur pour un moteur d’un aeronef comportant une chape, une bielle et une piece d’usure entre la chape et la bielle
DE102022210332A1 (de) * 2022-09-29 2024-04-04 Robert Bosch Gesellschaft mit beschränkter Haftung Hebelvorrichtung mit geklemmter Hebelachse

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000283116A (ja) * 1999-03-27 2000-10-13 Yoshiyuki Tezuka 軸心合わせ金具
US20020012567A1 (en) * 2000-05-05 2002-01-31 Schmidt George R. Compliant pivot socket for automotive steering
US20070138337A1 (en) * 2005-12-15 2007-06-21 Airbus France Rear suspension for an aircraft engine with shackle in waiting and spring for such a hinge pin in waiting
CN102312916A (zh) * 2011-09-01 2012-01-11 万泰工业（大连）有限公司 一种球接头装置
CN103148091A (zh) * 2011-12-07 2013-06-12 扬州柳工建设机械有限公司 泵车单球面拖挂扣

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US2838331A (en) * 1954-07-21 1958-06-10 Archie V Coleman Steering idler arm repair kit
US4597499A (en) * 1984-06-20 1986-07-01 Hanula Richard M Biased pin retainer block for a rotary coupling system
DE3608782A1 (de) * 1986-03-15 1987-09-24 Thyssen Industrie Drehgelenk mit durchstroemkanaelen
GB8722021D0 (en) * 1987-09-18 1987-10-28 British Aerospace Lock nut assemblies
JP2751385B2 (ja) 1988-05-19 1998-05-18 大正製薬株式会社 エリスロマイシンａオキシム及びその塩の製造方法
FR2635751B1 (fr) * 1988-09-01 1991-01-04 Snecma Dispositif de fixation d'une biellette de suspension d'un turboreacteur
JPH0634235Y2 (ja) * 1988-09-29 1994-09-07 光洋精工株式会社 浮体物係留装置
US5044812A (en) * 1990-01-23 1991-09-03 Dresser Industries, Inc. Sealed and lubricated pivot pin assembly and method
RU2005667C1 (ru) * 1992-06-05 1994-01-15 Самарское государственное научно-производственное предприятие "Труд" Задний пояс системы подвески газотурбинного двигателя
US5961141A (en) * 1997-11-26 1999-10-05 Caterpillar Inc. Pin assembly
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FR2879695B1 (fr) 2004-12-16 2007-04-06 Snecma Moteurs Sa Dispositif de liaison, de longueur ajustable, entre deux pieces
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
FR2887853B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage
DE102006036245A1 (de) * 2006-08-03 2008-02-07 Schaeffler Kg Gelenkkupplung für Schienenfahrzeuge
FR2907177B1 (fr) * 2006-10-13 2009-12-04 Snecma Assemblage d'un dispositif rotulant sur une chape de renvoi d'angle, systeme de commande d'un redresseur a calage variable le comportant, et moteur d'aeronef en etant muni
FR2923460B1 (fr) * 2007-11-12 2010-05-14 Snecma Montage d'un organe de suspension d'un turbomoteur
NO337432B1 (no) * 2007-11-12 2016-04-11 Bolt Norge As Anordning ved spennbolt
RU2377162C1 (ru) * 2008-04-28 2009-12-27 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Устройство для крепления газотурбинного двигателя к летательному аппарату
US8192104B2 (en) * 2009-02-25 2012-06-05 Caterpillar Inc. Machine suspension link pin retention system
FR2975132B1 (fr) * 2011-05-09 2015-06-26 Snecma Bielles de suspension du canal de flux froid d'un turboreacteur a rotules excentriques
GB201110483D0 (en) * 2011-06-21 2011-08-03 Airbus Operations Ltd Pivot joint assembly
US8851417B2 (en) * 2012-08-07 2014-10-07 United Technologies Corporation Self-retaining shear pin for blind mount location
FR3014973B1 (fr) * 2013-12-12 2016-01-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation
FR3014972B1 (fr) * 2013-12-12 2016-04-22 Airbus Operations Sas Assemblage comprenant un axe d'articulation supporte par une chape et immobilise en translation par un dispositif de blocage integrant un double systeme d'anti-rotation

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2000283116A (ja) * 1999-03-27 2000-10-13 Yoshiyuki Tezuka 軸心合わせ金具
US20020012567A1 (en) * 2000-05-05 2002-01-31 Schmidt George R. Compliant pivot socket for automotive steering
US20070138337A1 (en) * 2005-12-15 2007-06-21 Airbus France Rear suspension for an aircraft engine with shackle in waiting and spring for such a hinge pin in waiting
CN102312916A (zh) * 2011-09-01 2012-01-11 万泰工业（大连）有限公司 一种球接头装置
CN103148091A (zh) * 2011-12-07 2013-06-12 扬州柳工建设机械有限公司 泵车单球面拖挂扣

Also Published As

Publication number Publication date
EP3146218A1 (fr) 2017-03-29
US10626913B2 (en) 2020-04-21
EP3146218B1 (fr) 2018-10-10
BR112016027060B8 (pt) 2022-02-22
CN106460916A (zh) 2017-02-22
US20170102026A1 (en) 2017-04-13
RU2016148630A3 (https=) 2018-09-03
CA2949603A1 (fr) 2015-11-26
BR112016027060A2 (https=) 2017-08-15
CA2949603C (fr) 2022-04-19
BR112016027060B1 (pt) 2021-09-28
FR3021373A1 (fr) 2015-11-27
WO2015177431A1 (fr) 2015-11-26
FR3021373B1 (fr) 2016-12-09
RU2669502C2 (ru) 2018-10-11
RU2016148630A (ru) 2018-06-22

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