BR112016016336B1 - Rotor de uma turbomáquina de aeronave e turbomáquina de aeronave - Google Patents

Rotor de uma turbomáquina de aeronave e turbomáquina de aeronave Download PDF

Info

Publication number
BR112016016336B1
BR112016016336B1 BR112016016336-2A BR112016016336A BR112016016336B1 BR 112016016336 B1 BR112016016336 B1 BR 112016016336B1 BR 112016016336 A BR112016016336 A BR 112016016336A BR 112016016336 B1 BR112016016336 B1 BR 112016016336B1
Authority
BR
Brazil
Prior art keywords
rotor
speed
critical speed
critical
component
Prior art date
Application number
BR112016016336-2A
Other languages
English (en)
Portuguese (pt)
Other versions
BR112016016336A2 (enExample
Inventor
Julien Michel Patrick Christian Austruy
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of BR112016016336A2 publication Critical patent/BR112016016336A2/pt
Publication of BR112016016336B1 publication Critical patent/BR112016016336B1/pt

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/10Anti- vibration means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/323Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/24Rotors for turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/50Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/96Preventing, counteracting or reducing vibration or noise
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • F05D2300/501Elasticity

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BR112016016336-2A 2014-01-20 2015-01-19 Rotor de uma turbomáquina de aeronave e turbomáquina de aeronave BR112016016336B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1450424A FR3016659B1 (fr) 2014-01-20 2014-01-20 Organe mobile de turbomachine qui comporte des moyens pour changer sa frequence de resonance
FR1450424 2014-01-20
PCT/FR2015/050118 WO2015107310A1 (fr) 2014-01-20 2015-01-19 Organe mobile de turbomachine qui comporte des moyens pour changer sa fréquence de résonance

Publications (2)

Publication Number Publication Date
BR112016016336A2 BR112016016336A2 (enExample) 2017-08-08
BR112016016336B1 true BR112016016336B1 (pt) 2022-08-09

Family

ID=50290156

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016016336-2A BR112016016336B1 (pt) 2014-01-20 2015-01-19 Rotor de uma turbomáquina de aeronave e turbomáquina de aeronave

Country Status (8)

Country Link
US (1) US9624777B2 (enExample)
EP (1) EP3097266B1 (enExample)
CN (1) CN105917079B (enExample)
BR (1) BR112016016336B1 (enExample)
CA (1) CA2936772C (enExample)
FR (1) FR3016659B1 (enExample)
RU (1) RU2683334C1 (enExample)
WO (1) WO2015107310A1 (enExample)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3064764B1 (fr) * 2017-03-28 2019-06-28 Hutchinson Generateur d'efforts dynamiques comprenant au moins deux balourds et actionneur comprenant de tels generateurs

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3032985A (en) * 1960-07-27 1962-05-08 Gen Motors Corp Dual rotor governor
FR2336550A1 (fr) * 1975-12-24 1977-07-22 Europ Propulsion Montage d'arbre long, notamment pour turbomachine
US4117742A (en) * 1977-07-29 1978-10-03 Stein Philip C Permanent automatic rotor balancer for shafts operating above critical speed
RU1828166C (ru) * 1989-11-09 1995-09-10 Научно-производственное предпри тие "Завод им.В.Я.Климова" Роторная машина (ее варианты)
FR2864995B1 (fr) * 2004-01-12 2008-01-04 Snecma Moteurs Support de palier a double raideur
EP1892379B1 (de) * 2006-08-16 2015-11-18 Siemens Aktiengesellschaft Rotor für eine Strömungsmaschine
FR2918107B1 (fr) * 2007-06-26 2013-04-12 Snecma Dispositif amortisseur adapte aux arbres de turbomachine.
US8013481B2 (en) * 2009-03-27 2011-09-06 General Electric Company Detuner for tuning torsional mode of a rotating body

Also Published As

Publication number Publication date
US9624777B2 (en) 2017-04-18
CN105917079B (zh) 2018-01-26
CA2936772A1 (fr) 2015-07-23
RU2016129585A (ru) 2018-01-24
CA2936772C (fr) 2023-03-14
EP3097266B1 (fr) 2017-11-15
US20160333696A1 (en) 2016-11-17
FR3016659B1 (fr) 2016-03-04
FR3016659A1 (fr) 2015-07-24
CN105917079A (zh) 2016-08-31
WO2015107310A1 (fr) 2015-07-23
EP3097266A1 (fr) 2016-11-30
RU2683334C1 (ru) 2019-03-28
BR112016016336A2 (enExample) 2017-08-08

Similar Documents

Publication Publication Date Title
JP5511436B2 (ja) ヘリコプタロータ
JP3393037B2 (ja) ロータに偶発的偏心が現われた後に航空機用ターボエンジンの運転を維持するための方法及びベアリングサポート
RU2517643C2 (ru) Винт вертолета и вертолет (варианты), содержащий этот винт
JPS6267238A (ja) 可動羽根用の作動器
JP4541170B2 (ja) 第1および第2の軸受により支持される駆動シャフトに固定されるファンを有するターボファンエンジン
EP3141700B1 (en) Seal crystalline orientation for increased compliance
CN102656338A (zh) 具有受控加载的涡轮机叶片阻尼装置
US20110142654A1 (en) Turbine Blade Damping Device With Controlled Loading
EP1832511A1 (en) Rotating duct type rotor with shroud
US2727716A (en) Bladed body
ES2648304T3 (es) Dispositivo de protección mecánica
CN105992890A (zh) 离心力摆和具有这种离心力摆的扭矩传递装置
CN103282604A (zh) 燃气涡轮叶片的减振方法和实施该方法所用的减振器
CN111630249A (zh) 阻尼装置
CN104843180B (zh) 飞行器及具有用于将主齿轮箱和发动机连接在一起的连接装置的飞行器动力设备
BR112016016336B1 (pt) Rotor de uma turbomáquina de aeronave e turbomáquina de aeronave
KR101675269B1 (ko) 가스터빈 디스크
JP4890826B2 (ja) ヘリコプター用の回転翼
US9316116B2 (en) Method and damping device for vibration damping of a blade of a turbomachine as well as turbomachine
JP2010156461A (ja) ロータ付き装置の取付用の取付手段
JP6424254B2 (ja) ロータ及びかかるロータが提供された航空機
US9506372B2 (en) Damping means for damping a blade movement of a turbomachine
BRPI0411088B1 (pt) Conjunto de suporte com parte inclinada
KR102785680B1 (ko) 프로펠러샤프트의 공진 회피기구
CN106812723A (zh) 叶片、涡轮及压气机

Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 19/01/2015, OBSERVADAS AS CONDICOES LEGAIS