KR20020036663A - 조립된 토크 샤프트 - Google Patents
조립된 토크 샤프트 Download PDFInfo
- Publication number
- KR20020036663A KR20020036663A KR1020010040418A KR20010040418A KR20020036663A KR 20020036663 A KR20020036663 A KR 20020036663A KR 1020010040418 A KR1020010040418 A KR 1020010040418A KR 20010040418 A KR20010040418 A KR 20010040418A KR 20020036663 A KR20020036663 A KR 20020036663A
- Authority
- KR
- South Korea
- Prior art keywords
- torque shaft
- arm
- main body
- assembled
- stage
- Prior art date
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
- 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
-
- 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
- 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
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/04—Crankshafts, eccentric-shafts; Cranks, eccentrics
- F16C3/06—Crankshafts
- F16C3/10—Crankshafts assembled of several parts, e.g. by welding by crimping
- F16C3/12—Crankshafts assembled of several parts, e.g. by welding by crimping releasably connected
-
- 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
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/04—Crankshafts, eccentric-shafts; Cranks, eccentrics
- F16C3/22—Cranks; Eccentrics
-
- 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
- F05D2240/60—Shafts
-
- 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
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/72—Adjusting of angle of incidence or attack of rotating blades by turning around an axis parallel to the rotor centre line
-
- 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)
- Ocean & Marine Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
Description
Claims (11)
- 조립된 토크 샤프트(10, 12, 210)에 있어서,전방 단부 및 후방 단부를 갖는 토크 샤프트 메인 몸체(26)와,상기 전방 단부에 인접하여 형성되는 제 1 베어링(42) 및 상기 메인 몸체의 후방 단부에 형성되는 제 2 베어링(44)과,상기 토크 샤프트를 압축기(14)의 다수의 베인 스테이지에 작동가능하게 연결하기 위해 상기 토크 샤프트 메인 몸체를 따라 이격된 위치에 제공된 다수의 암 구조체(32, 232; 46, 246; 52, 252; 56; 62; 68, 268; 74, 274)를 포함하며;상기 암 구조체(32, 232; 46, 246; 52, 252; 56; 62; 68, 268; 74, 274)중 적어도 하나는 상기 토크 샤프트 메인 몸체(26)에 분리가능하게 고정되어, 상기 적어도 하나의 암 구조체가 제거되고 다른 암 구조체로 교체될 수 있는조립된 토크 샤프트.
- 제 1 항에 있어서,상기 다수의 암 구조체(32, 232; 46, 246; 52, 252; 56; 62; 68, 268; 74, 274)는 상기 토크 샤프트 메인 몸체(26)에 분리가능하게 고정되는조립된 토크 샤프트.
- 제 2 항에 있어서,상기 토크 샤프트 메인 몸체는 상기 각 분리가능한 암 구조체(46, 246; 52, 252; 56; 62; 68, 268; 74, 274)를 수납하기 위한 리세스형 저장소(84, 86, 88, 90, 92, 94)를 포함하는조립된 토크 샤프트.
- 제 3 항에 있어서,상기 리세스형 저장소(84, 86, 88, 90, 92, 94)는 상기 토크 샤프트 메인 몸체(26)내에 기계가공되는조립된 토크 샤프트.
- 제 4 항에 있어서,상기 리세스형 저장소(84, 86, 88, 90, 92, 94)는 상기 각 분리가능한 암 구조체를 위해 각기 상이한 깊이로 기계가공되는조립된 토크 샤프트.
- 제 3 항에 있어서,상기 리세스형 저장소(84, 86, 88, 90, 92)중 적어도 일부에 배치되어, 상기 각 분리가능한 암 구조체(46, 246; 56; 62; 68, 268; 74, 274)를 그 내에 위치설정하기 위한 핀 요소(110)를 더 포함하는조립된 토크 샤프트.
- 제 6 항에 있어서,상기 각 핀 요소(110)는 상기 리세스형 저장소(84, 86, 88, 90, 92)내에 단독으로 위치되고, 상기 각 암 구조체(46, 246; 56; 62; 68, 268; 74, 274)는 대응하는 단일 위치에 형성된 핀 구멍(112)을 포함하며, 그에 따라 상기 각 암 구조체가 상기 각 저장소 및 핀 요소에 의해 수납 및 단독 결합될 수 있는조립된 토크 샤프트.
- 제 1 항에 있어서,상기 토크 샤프트 메인 몸체의 회전 위치를 제어하도록 상기 토크 샤프트 메인 몸체에 배치되는 입력 암(52, 252)을 더 포함하는조립된 토크 샤프트.
- 제 8 항에 있어서,상기 입력 암(52, 252)은 상기 토크 샤프트 메인 몸체(26)에 분리가능하게 고정되는조립된 토크 샤프트.
- 제 9 항에 있어서,상기 입력 암(52, 252)용 저장소(94)를 더 포함하는조립된 토크 샤프트.
- 제 1 항에 있어서,상기 각 암 구조체가 기부(130)와, 제 1 및 제 2 측벽(132)을 포함하고, 상기 각 측벽은 상기 기부의 평면에 대체로 수직하고 상기 토크 샤프트 메인 몸체(26)의 종방향 축에 수직한 각 평면에 배치되는조립된 토크 샤프트.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/707,912 US6457937B1 (en) | 2000-11-08 | 2000-11-08 | Fabricated torque shaft |
US09/707,912 | 2000-11-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
KR20020036663A true KR20020036663A (ko) | 2002-05-16 |
KR100677644B1 KR100677644B1 (ko) | 2007-02-01 |
Family
ID=24843649
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020010040418A KR100677644B1 (ko) | 2000-11-08 | 2001-07-06 | 조립된 토크 샤프트 |
Country Status (5)
Country | Link |
---|---|
US (1) | US6457937B1 (ko) |
EP (1) | EP1207271B1 (ko) |
JP (1) | JP5148031B2 (ko) |
KR (1) | KR100677644B1 (ko) |
DE (1) | DE60135966D1 (ko) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6769868B2 (en) * | 2002-07-31 | 2004-08-03 | General Electric Company | Stator vane actuator in gas turbine engine |
US20050129340A1 (en) * | 2003-12-10 | 2005-06-16 | Arnold Robert A. | Hourglass bearing |
US8777537B2 (en) * | 2007-12-26 | 2014-07-15 | Rolls-Royce North American Technologies, Inc. | Fastener with shear bushing |
US8282349B2 (en) * | 2008-03-07 | 2012-10-09 | General Electric Company | Steam turbine rotor and method of assembling the same |
WO2010031768A2 (en) * | 2008-09-18 | 2010-03-25 | Siemens Aktiengesellschaft | Method, system, device for variable guide vanes |
IT1401664B1 (it) * | 2010-08-31 | 2013-08-02 | Nuova Pignone S R L | Dispositivo di centraggio e sistema per anello di guida. |
KR101188639B1 (ko) | 2010-12-21 | 2012-10-09 | 두산중공업 주식회사 | 가스터빈 압축기의 공기 유입 가이드 장치 |
JP5340333B2 (ja) * | 2011-03-07 | 2013-11-13 | 株式会社日立製作所 | 軸流圧縮機の改造方法 |
DE102012007129A1 (de) * | 2012-04-10 | 2013-10-10 | Rolls-Royce Deutschland Ltd & Co Kg | Leitschaufelverstellvorrichtung einer Gasturbine |
US20140064911A1 (en) * | 2012-08-29 | 2014-03-06 | General Electric Company | Systems and Methods to Control Variable Stator Vanes in Gas Turbine Engines |
EP2956631B1 (en) * | 2013-02-12 | 2020-04-15 | United Technologies Corporation | Variable vane adjustment system |
FR3008450B1 (fr) * | 2013-07-09 | 2015-08-07 | Snecma | Carter de turbomachine a bride decoupee |
GB201409449D0 (en) | 2014-05-28 | 2014-07-09 | Rolls Royce Deutschland | A variable stator vane arrangment |
US20170108032A1 (en) * | 2015-10-16 | 2017-04-20 | General Electric Company | Stepped shaft assembly |
US9982686B2 (en) | 2015-11-04 | 2018-05-29 | General Electric Company | Turnbuckle dampening links |
US11156120B2 (en) * | 2016-03-21 | 2021-10-26 | Raytheon Technologies Corporation | Link setting assembly and method |
US10519797B2 (en) * | 2016-06-27 | 2019-12-31 | General Electric Company | Turbine engine and stator vane pitch adjustment system therefor |
DE102016225482A1 (de) | 2016-12-19 | 2018-06-21 | Rolls-Royce Deutschland Ltd & Co Kg | Verstelleinrichtung für die Verstellung mehrerer Leitschaufeln eines Triebwerks |
US11092167B2 (en) * | 2018-08-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Variable vane actuating system |
US11092032B2 (en) * | 2018-08-28 | 2021-08-17 | Pratt & Whitney Canada Corp. | Variable vane actuating system |
US10704412B2 (en) | 2018-10-05 | 2020-07-07 | Raytheon Technologies Corporation | Bell crank and bar assembly |
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US2404428A (en) * | 1944-01-31 | 1946-07-23 | Westinghouse Electric Corp | Turbine apparatus |
US2819732A (en) * | 1954-07-14 | 1958-01-14 | Thompson Prod Inc | Variable area turbine entrance nozzle |
US3219134A (en) * | 1962-06-15 | 1965-11-23 | Douglas Aircraft Co Inc | Ground effect machine |
US3487992A (en) * | 1967-11-01 | 1970-01-06 | Gen Electric | Stator adjusting mechanism for axial flow compressors |
JPS51334B2 (ko) * | 1971-10-12 | 1976-01-07 | ||
US3779665A (en) * | 1972-09-22 | 1973-12-18 | Gen Electric | Combined variable angle stator and windmill control system |
US3873230A (en) * | 1974-04-10 | 1975-03-25 | United Aircraft Corp | Stator vane actuating mechanism |
GB1511723A (en) * | 1975-05-01 | 1978-05-24 | Rolls Royce | Variable stator vane actuating mechanism |
US4096614A (en) * | 1975-09-02 | 1978-06-27 | General Electric Company | Method and apparatus for removing stator vanes |
GB2078865B (en) * | 1980-06-28 | 1983-06-08 | Rolls Royce | A variable stator vane operating mechanism for a gas turbine engine |
US4400135A (en) * | 1981-04-06 | 1983-08-23 | General Motors Corporation | Vane actuation system |
JPS597708A (ja) * | 1982-07-07 | 1984-01-14 | Hitachi Ltd | 軸流機械における静翼取付角可変装置 |
US4856962A (en) * | 1988-02-24 | 1989-08-15 | United Technologies Corporation | Variable inlet guide vane |
US4890977A (en) * | 1988-12-23 | 1990-01-02 | Pratt & Whitney Canada, Inc. | Variable inlet guide vane mechanism |
US5549448A (en) | 1995-02-08 | 1996-08-27 | United Technolgies Corporation | Variable stator vane linkage system and method |
US6174130B1 (en) * | 1999-06-30 | 2001-01-16 | General Electric Company | Movable shaft assembly |
US6551057B1 (en) * | 1999-11-22 | 2003-04-22 | General Electric Company | Damped torque shaft assembly |
-
2000
- 2000-11-08 US US09/707,912 patent/US6457937B1/en not_active Expired - Lifetime
-
2001
- 2001-07-05 DE DE60135966T patent/DE60135966D1/de not_active Expired - Lifetime
- 2001-07-05 EP EP01305823A patent/EP1207271B1/en not_active Expired - Lifetime
- 2001-07-06 KR KR1020010040418A patent/KR100677644B1/ko active IP Right Grant
- 2001-07-06 JP JP2001205488A patent/JP5148031B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6457937B1 (en) | 2002-10-01 |
JP2002147387A (ja) | 2002-05-22 |
DE60135966D1 (de) | 2008-11-13 |
JP5148031B2 (ja) | 2013-02-20 |
EP1207271A2 (en) | 2002-05-22 |
EP1207271A3 (en) | 2003-08-06 |
EP1207271B1 (en) | 2008-10-01 |
KR100677644B1 (ko) | 2007-02-01 |
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