BR112016028858A2 - ?conjuntos de suspensor e tubo base? - Google Patents

?conjuntos de suspensor e tubo base?

Info

Publication number
BR112016028858A2
BR112016028858A2 BR112016028858A BR112016028858A BR112016028858A2 BR 112016028858 A2 BR112016028858 A2 BR 112016028858A2 BR 112016028858 A BR112016028858 A BR 112016028858A BR 112016028858 A BR112016028858 A BR 112016028858A BR 112016028858 A2 BR112016028858 A2 BR 112016028858A2
Authority
BR
Brazil
Prior art keywords
base tube
hanger
base
suspension
tube assemblies
Prior art date
Application number
BR112016028858A
Other languages
English (en)
Inventor
John Breslin Andrew
Loring Heitman Bryce
Christopher Schilling Jan
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112016028858A2 publication Critical patent/BR112016028858A2/pt

Links

Classifications

    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Supports For Pipes And Cables (AREA)

Abstract

trata-se de um conjunto de suspensor de tubo base (30) que é fornecido para suspensores (34) e tubos base (50) que definem componentes dimensionalmente incompatíveis como aqueles que são encaixados por pressão ou atrito para engatar um ao outro. o conjunto de suspensor de tubo base (30) inclui um suspensor com múltiplas peças (34) e um tubo base (50) que é preso com pinos ao conjunto de suspensor (30) por pelo menos um pino que se estende de modo axial (70) e que localiza o tubo base em relação ao suspensor para controlar o movimento em uma ou ambas as direções circunferencial (tangencial) e radial em relação ao motor.
BR112016028858A 2014-06-12 2015-05-06 ?conjuntos de suspensor e tubo base? BR112016028858A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201462011237P 2014-06-12 2014-06-12
PCT/US2015/029342 WO2015191186A1 (en) 2014-06-12 2015-05-06 Shroud hanger assembly

Publications (1)

Publication Number Publication Date
BR112016028858A2 true BR112016028858A2 (pt) 2017-08-22

Family

ID=53177383

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016028858A BR112016028858A2 (pt) 2014-06-12 2015-05-06 ?conjuntos de suspensor e tubo base?

Country Status (7)

Country Link
US (3) US11215081B2 (pt)
EP (2) EP3670844B1 (pt)
JP (1) JP6804305B2 (pt)
CN (1) CN106661952B (pt)
BR (1) BR112016028858A2 (pt)
CA (1) CA2955121C (pt)
WO (1) WO2015191186A1 (pt)

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JP6804305B2 (ja) 2014-06-12 2020-12-23 ゼネラル・エレクトリック・カンパニイ シュラウドハンガ組立体
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FR3045715B1 (fr) 2015-12-18 2018-01-26 Safran Aircraft Engines Ensemble d'anneau de turbine avec maintien a froid et a chaud
FR3049003B1 (fr) 2016-03-21 2018-04-06 Safran Aircraft Engines Ensemble d'anneau de turbine sans jeu de montage a froid
FR3056632B1 (fr) * 2016-09-27 2020-06-05 Safran Aircraft Engines Ensemble d'anneau turbine comprenant un element de repartition de l'air de refroidissement
GB201621455D0 (en) * 2016-12-16 2017-02-01 Rolls Royce Plc Mount Structure
US10619514B2 (en) 2017-10-18 2020-04-14 Rolls-Royce Corporation Ceramic matrix composite assembly with compliant pin attachment features
US10801350B2 (en) 2018-02-23 2020-10-13 Rolls-Royce Corporation Actively cooled engine assembly with ceramic matrix composite components
JP7018131B2 (ja) * 2018-05-11 2022-02-09 川崎重工業株式会社 ガスタービンのシュラウド組立体
US10753221B2 (en) * 2018-12-12 2020-08-25 Raytheon Technologies Corporation Seal assembly with ductile wear liner
US11021990B2 (en) * 2018-12-19 2021-06-01 General Electric Company Shroud sealing for a gas turbine engine
US10830050B2 (en) 2019-01-31 2020-11-10 General Electric Company Unitary body turbine shrouds including structural breakdown and collapsible features
US11098608B2 (en) * 2019-03-13 2021-08-24 Raytheon Technologies Corporation CMC BOAS with internal support structure
US20200300107A1 (en) * 2019-03-18 2020-09-24 United Technologies Corporation Cmc blade outer air seal
US11047250B2 (en) * 2019-04-05 2021-06-29 Raytheon Technologies Corporation CMC BOAS transverse hook arrangement
FR3095668B1 (fr) * 2019-05-03 2021-04-09 Safran Aircraft Engines Ensemble d’anneau de turbine monté sur entretoise
US11255209B2 (en) * 2019-08-29 2022-02-22 Raytheon Technologies Corporation CMC BOAS arrangement
US11174747B2 (en) * 2020-02-13 2021-11-16 Raytheon Technologies Corporation Seal assembly with distributed cooling arrangement
US11215064B2 (en) 2020-03-13 2022-01-04 Raytheon Technologies Corporation Compact pin attachment for CMC components
FR3122210A1 (fr) * 2021-04-21 2022-10-28 Safran Aircraft Engines Ensemble d’anneau de turbine monté sur entretoise
FR3123943B1 (fr) * 2021-06-14 2024-01-26 Safran Aircraft Engines Ensemble d’anneau de turbine monté sur entretoise
US20220412222A1 (en) * 2021-06-25 2022-12-29 General Electric Company Attachment structures for airfoil bands
US11781448B1 (en) * 2022-04-05 2023-10-10 General Electric Company Shroud pin for gas turbine engine shroud
FR3139292A1 (fr) * 2022-09-01 2024-03-08 Safran Aircraft Engines Ensemble d’anneau de turbine à rattrapage de jeux intégré
US11773751B1 (en) 2022-11-29 2023-10-03 Rolls-Royce Corporation Ceramic matrix composite blade track segment with pin-locating threaded insert
US11840936B1 (en) 2022-11-30 2023-12-12 Rolls-Royce Corporation Ceramic matrix composite blade track segment with pin-locating shim kit
US11713694B1 (en) 2022-11-30 2023-08-01 Rolls-Royce Corporation Ceramic matrix composite blade track segment with two-piece carrier
US11732604B1 (en) 2022-12-01 2023-08-22 Rolls-Royce Corporation Ceramic matrix composite blade track segment with integrated cooling passages
US11885225B1 (en) 2023-01-25 2024-01-30 Rolls-Royce Corporation Turbine blade track with ceramic matrix composite segments having attachment flange draft angles

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Also Published As

Publication number Publication date
WO2015191186A1 (en) 2015-12-17
EP3670844B1 (en) 2022-01-05
WO2015191186A8 (en) 2017-01-12
EP3155229A1 (en) 2017-04-19
US20190284958A1 (en) 2019-09-19
CA2955121A1 (en) 2015-12-17
JP6804305B2 (ja) 2020-12-23
JP2017524089A (ja) 2017-08-24
US20240141804A1 (en) 2024-05-02
EP3155229B1 (en) 2020-03-18
CA2955121C (en) 2019-10-01
CN106661952A (zh) 2017-05-10
EP3670844A1 (en) 2020-06-24
US11879349B2 (en) 2024-01-23
CN106661952B (zh) 2019-09-03
US20220120198A1 (en) 2022-04-21
US11215081B2 (en) 2022-01-04

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements