PL415534A1 - Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych - Google Patents

Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych

Info

Publication number
PL415534A1
PL415534A1 PL415534A PL41553416A PL415534A1 PL 415534 A1 PL415534 A1 PL 415534A1 PL 415534 A PL415534 A PL 415534A PL 41553416 A PL41553416 A PL 41553416A PL 415534 A1 PL415534 A1 PL 415534A1
Authority
PL
Poland
Prior art keywords
cover
sheath
septum
attached
rear side
Prior art date
Application number
PL415534A
Other languages
English (en)
Inventor
Marcin Jacek Lobocki
Wiktor Wardecki
Joseph C. Kulesa
Maciej Staszewski
Original Assignee
General Electric Company
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 General Electric Company filed Critical General Electric Company
Priority to PL415534A priority Critical patent/PL415534A1/pl
Priority to JP2016211155A priority patent/JP2017122433A/ja
Priority to US15/336,831 priority patent/US10502233B2/en
Priority to EP16196832.6A priority patent/EP3187690A1/en
Priority to CA2947368A priority patent/CA2947368A1/en
Priority to CN201610960765.9A priority patent/CN107023333B/zh
Publication of PL415534A1 publication Critical patent/PL415534A1/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • 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
    • F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
    • 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
    • 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
    • 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
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc
    • 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/08—Sealings
    • F04D29/083—Sealings especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/126—Baffles or ribs
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/71—Shape curved
    • F05D2250/712—Shape curved concave
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/30—Retaining components in desired mutual position
    • F05D2260/31—Retaining bolts or nuts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych zawiera osłonę przedstawioną na rysunku. Osłona ma pierwszy koniec skonfigurowany do dołączenia do pierścieniowego członu nośnego silnika turbospalinowego i drugi koniec. Osłona ma również dalszy koniec zawierający odchodzący osiowo do tyłu występ, i zespół uszczelniający skonfigurowany do utworzenia uszczelnienia z pierścieniowym zestawem obrotowych zębów na wirniku silnika turbospalinowego. Osłona zawiera ponadto łukowy korpus osłony rozciągający się pomiędzy dalszym końcem a drugim końcem. Zespół osłony i przegrody zawiera również przegrodę dołączoną do tylnego boku osłony. Przegroda zawiera promieniowo zewnętrzny koniec dołączony do tylnego boku, promieniowo wewnętrzny koniec dołączony do odchodzącego osiowo do tyłu występu i rozciągający się pomiędzy nimi łukowy korpus przegrody. Zarówno osłona, jak i przegroda rozciągają się obwodowo wokół osi środkowej.
PL415534A 2016-01-04 2016-01-04 Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych PL415534A1 (pl)

Priority Applications (6)

Application Number Priority Date Filing Date Title
PL415534A PL415534A1 (pl) 2016-01-04 2016-01-04 Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych
JP2016211155A JP2017122433A (ja) 2016-01-04 2016-10-28 入口案内翼のシュラウド・バッフル組立体のためのシステム
US15/336,831 US10502233B2 (en) 2016-01-04 2016-10-28 System for an inlet guide vane shroud and baffle assembly
EP16196832.6A EP3187690A1 (en) 2016-01-04 2016-11-02 System for an inlet guide vane shroud and baffle assembly
CA2947368A CA2947368A1 (en) 2016-01-04 2016-11-03 System for an inlet guide vane shroud and baffle assembly
CN201610960765.9A CN107023333B (zh) 2016-01-04 2016-11-04 用于入口导叶护罩和挡板组件的系统

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL415534A PL415534A1 (pl) 2016-01-04 2016-01-04 Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych

Publications (1)

Publication Number Publication Date
PL415534A1 true PL415534A1 (pl) 2017-07-17

Family

ID=57218829

Family Applications (1)

Application Number Title Priority Date Filing Date
PL415534A PL415534A1 (pl) 2016-01-04 2016-01-04 Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych

Country Status (6)

Country Link
US (1) US10502233B2 (pl)
EP (1) EP3187690A1 (pl)
JP (1) JP2017122433A (pl)
CN (1) CN107023333B (pl)
CA (1) CA2947368A1 (pl)
PL (1) PL415534A1 (pl)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3646114B1 (en) * 2017-06-29 2023-06-28 Materion Precision Optics (Shanghai) Limited Phosphor wheel

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3781802A2 (en) 2018-04-17 2021-02-24 Kayara, Sammy Wind-funneling for gas turbines
US11131204B2 (en) * 2018-08-21 2021-09-28 General Electric Company Additively manufactured nested segment assemblies for turbine engines
FR3099792B1 (fr) * 2019-08-06 2021-07-30 Safran Aircraft Engines Compresseur de turbomoteur d’aéronef comprenant un dispositif de blocage d’un anneau de retenue
FR3099794B1 (fr) * 2019-08-06 2021-07-16 Safran Aircraft Engines Compresseur de turbomoteur d’aéronef comprenant un organe de liaison d’un anneau de retenue au carter intermédiaire
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines
KR102343928B1 (ko) * 2020-09-14 2021-12-24 두산중공업 주식회사 압축기 베인 슈라우드 조립체 및 이를 포함하는 가스 터빈
CN115387906B (zh) * 2022-05-12 2024-04-16 中国航发四川燃气涡轮研究院 低进口轮毂比发动机的进气承力框架连接结构及装配方法
US12454913B2 (en) * 2022-10-28 2025-10-28 Pratt & Whitney Canada Corp. Gas turbine engine component with integral heat exchanger
US12392295B2 (en) * 2023-01-11 2025-08-19 General Electric Company Aircraft propulsion system
US12584443B2 (en) * 2024-08-23 2026-03-24 Pratt & Whitney Canada Corp. Accelerating turbine engine rotating structure with compressed air

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL103792C (pl) 1954-12-16
US3703081A (en) 1970-11-20 1972-11-21 Gen Electric Gas turbine engine
US4087199A (en) 1976-11-22 1978-05-02 General Electric Company Ceramic turbine shroud assembly
FR2455674A1 (fr) 1979-05-02 1980-11-28 Snecma Dispositif d'etancheite entre deux elements de turbomachine
GB2239678B (en) 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
FR2685033B1 (fr) * 1991-12-11 1994-02-11 Snecma Stator dirigeant l'entree de l'air a l'interieur d'une turbomachine et procede de montage d'une aube de ce stator.
US5327716A (en) 1992-06-10 1994-07-12 General Electric Company System and method for tailoring rotor tip bleed air
US5361580A (en) * 1993-06-18 1994-11-08 General Electric Company Gas turbine engine rotor support system
US5443590A (en) * 1993-06-18 1995-08-22 General Electric Company Rotatable turbine frame
US20040126258A1 (en) 2002-12-30 2004-07-01 Industrial Technology Research Institute Baffle plate assembly for a compressor
US7658063B1 (en) 2005-07-15 2010-02-09 Florida Turbine Technologies, Inc. Gas turbine having a single shaft bypass configuration
US8047773B2 (en) 2007-08-23 2011-11-01 General Electric Company Gas turbine shroud support apparatus
DE102008049358A1 (de) 2008-09-29 2010-04-01 Mtu Aero Engines Gmbh Axiale Strömungsmaschine mit asymmetrischem Verdichtereintrittsleitgitter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3646114B1 (en) * 2017-06-29 2023-06-28 Materion Precision Optics (Shanghai) Limited Phosphor wheel

Also Published As

Publication number Publication date
JP2017122433A (ja) 2017-07-13
CN107023333B (zh) 2019-03-19
US20170191500A1 (en) 2017-07-06
US10502233B2 (en) 2019-12-10
EP3187690A1 (en) 2017-07-05
CN107023333A (zh) 2017-08-08
CA2947368A1 (en) 2017-07-04

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