MX2019013305A - Perno para reducir el movimiento rotatorio relativo de un disco y un espaciador de un motor de turbina. - Google Patents
Perno para reducir el movimiento rotatorio relativo de un disco y un espaciador de un motor de turbina.Info
- Publication number
- MX2019013305A MX2019013305A MX2019013305A MX2019013305A MX2019013305A MX 2019013305 A MX2019013305 A MX 2019013305A MX 2019013305 A MX2019013305 A MX 2019013305A MX 2019013305 A MX2019013305 A MX 2019013305A MX 2019013305 A MX2019013305 A MX 2019013305A
- Authority
- MX
- Mexico
- Prior art keywords
- spacer
- disk
- pin
- turbine engine
- rotational movement
- Prior art date
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
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/64—Mounting; Assembling; Disassembling of axial pumps
- F04D29/644—Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps
-
- 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
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
- F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage 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
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
-
- 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
- F05D2250/10—Two-dimensional
- F05D2250/13—Two-dimensional trapezoidal
- F05D2250/132—Two-dimensional trapezoidal hexagonal
-
- 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
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Un compresor axial (12) de un motor de turbina (10) incluye una pluralidad de pares de disco y espaciador (14) orientada a lo largo de un eje de rotación común. Cada uno de un disco (16) y un espaciador (18) de los pares de disco y espaciador (14) tiene una cara de contacto (20, 22) que define una sujeción entre el disco (16) y el espaciador (18). La cara de contacto (20, 22) de cada uno del disco (16) y el espaciador (18) incluye un área empotrada (24, 26). Un perno (28) tiene un vástago (30) recibido dentro del área empotrada (24) del disco (16) y una cabeza (32) recibida dentro del área empotrada (26) del espaciador (18). La cabeza (32) del perno (28) incluye al menos dos planos (40) que corresponden a superficies complementarias del área empotrada (26) del espaciador (18).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/588,871 US10385874B2 (en) | 2017-05-08 | 2017-05-08 | Pin to reduce relative rotational movement of disk and spacer of turbine engine |
PCT/US2018/030938 WO2018208577A1 (en) | 2017-05-08 | 2018-05-03 | Pin to reduce relative rotational movement of disk and spacer of turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2019013305A true MX2019013305A (es) | 2020-02-07 |
Family
ID=64015221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2019013305A MX2019013305A (es) | 2017-05-08 | 2018-05-03 | Perno para reducir el movimiento rotatorio relativo de un disco y un espaciador de un motor de turbina. |
Country Status (5)
Country | Link |
---|---|
US (1) | US10385874B2 (es) |
CN (1) | CN110603372B (es) |
AU (1) | AU2018264866B2 (es) |
MX (1) | MX2019013305A (es) |
WO (1) | WO2018208577A1 (es) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114909381B (zh) * | 2021-02-07 | 2023-11-03 | 中国航发商用航空发动机有限责任公司 | 一种螺栓防转装配结构及采用该装配结构的航空发动机 |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB749279A (en) * | 1953-12-05 | 1956-05-23 | Power Jets Res & Dev Ltd | Bladed rotors for multistage axial flow compressors, turbines and like fluid flow machines |
GB897415A (en) * | 1959-10-20 | 1962-05-30 | Rolls Royce | Improvements in or relating to bladed rotors |
US3263962A (en) * | 1965-04-22 | 1966-08-02 | Gen Motors Corp | Rotor blade lock |
US3597110A (en) * | 1969-10-23 | 1971-08-03 | Gen Electric | Joint construction |
FR2607866B1 (fr) * | 1986-12-03 | 1991-04-12 | Snecma | Axes de fixation de rotors de turbomachine, procede de montage et rotors ainsi montes |
US5320488A (en) | 1993-01-21 | 1994-06-14 | General Electric Company | Turbine disk interstage seal anti-rotation system |
US5388963A (en) * | 1993-07-02 | 1995-02-14 | United Technologies Corporation | Flange for high speed rotors |
JPH11132166A (ja) * | 1997-10-28 | 1999-05-18 | Mitsubishi Heavy Ind Ltd | スクロール型流体機械 |
US6158102A (en) | 1999-03-24 | 2000-12-12 | General Electric Co. | Apparatus and methods for aligning holes through wheels and spacers and stacking the wheels and spacers to form a turbine rotor |
GB9925261D0 (en) | 1999-10-27 | 1999-12-29 | Rolls Royce Plc | Locking devices |
US6524069B2 (en) * | 2000-07-07 | 2003-02-25 | Turning Point Propellers, Inc. | Propeller assembly incorporating improved locking structure |
FR2869374B1 (fr) * | 2004-04-23 | 2009-01-30 | Snecma Moteurs Sa | Systeme de fixation de pieces par des goujons a collerettes |
JP4918263B2 (ja) | 2006-01-27 | 2012-04-18 | 三菱重工業株式会社 | 軸流圧縮機の静翼環 |
US7581931B2 (en) | 2006-10-13 | 2009-09-01 | Siemens Energy, Inc. | Gas turbine belly band seal anti-rotation structure |
EP2299060A1 (de) * | 2009-09-17 | 2011-03-23 | Siemens Aktiengesellschaft | Schaufelbefestigung mit Sicherheitseinrichtung für Turbinenschaufeln |
US8840375B2 (en) | 2011-03-21 | 2014-09-23 | United Technologies Corporation | Component lock for a gas turbine engine |
CN103477051B (zh) * | 2011-04-11 | 2016-05-11 | 博格华纳公司 | 排气涡轮增压器的轴承壳体 |
US20130017092A1 (en) * | 2011-07-11 | 2013-01-17 | General Electric Company | Rotor assembly for gas turbines |
US8932022B2 (en) * | 2012-02-03 | 2015-01-13 | Pratt & Whitney Canada Corp. | Fastening system for fan and shaft interconnection |
JP6045244B2 (ja) * | 2012-08-06 | 2016-12-14 | 三菱重工業株式会社 | 回転機械のロータ軸心合せ接続用治具、及びロータ接続方法 |
FR3002970A1 (fr) * | 2013-03-07 | 2014-09-12 | Alstom Technology Ltd | Rotor de turbine pour une centrale thermoelectrique |
US9316106B2 (en) * | 2013-07-19 | 2016-04-19 | Siemens Energy, Inc. | Expanding lock pin for turbine side entry blade |
EP3056683B1 (de) * | 2015-02-16 | 2018-05-23 | MTU Aero Engines GmbH | Axial geteilter Innenring für eine Strömungsmaschine und Leitschaufelkranz |
ES2733952T3 (es) * | 2015-12-15 | 2019-12-03 | MTU Aero Engines AG | Estructura de fijación |
US10864585B2 (en) * | 2017-03-13 | 2020-12-15 | General Electric Company | Machining system for turbomachine dovetail |
KR101919228B1 (ko) * | 2017-03-16 | 2018-11-15 | 두산중공업 주식회사 | 버킷의 축 방향 고정 장치와 버킷 조립체 및 이를 포함하는 가스터빈 |
US10865646B2 (en) * | 2017-05-04 | 2020-12-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
-
2017
- 2017-05-08 US US15/588,871 patent/US10385874B2/en active Active
-
2018
- 2018-05-03 CN CN201880030216.9A patent/CN110603372B/zh active Active
- 2018-05-03 AU AU2018264866A patent/AU2018264866B2/en active Active
- 2018-05-03 MX MX2019013305A patent/MX2019013305A/es unknown
- 2018-05-03 WO PCT/US2018/030938 patent/WO2018208577A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2018208577A1 (en) | 2018-11-15 |
US10385874B2 (en) | 2019-08-20 |
AU2018264866A1 (en) | 2019-12-05 |
AU2018264866B2 (en) | 2023-11-30 |
CN110603372B (zh) | 2022-04-29 |
CN110603372A (zh) | 2019-12-20 |
US20180320708A1 (en) | 2018-11-08 |
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