MX2013011269A - Aparato y procedimiento para probar un motor de turbina de gas industrial y componentes del mismo. - Google Patents
Aparato y procedimiento para probar un motor de turbina de gas industrial y componentes del mismo.Info
- Publication number
- MX2013011269A MX2013011269A MX2013011269A MX2013011269A MX2013011269A MX 2013011269 A MX2013011269 A MX 2013011269A MX 2013011269 A MX2013011269 A MX 2013011269A MX 2013011269 A MX2013011269 A MX 2013011269A MX 2013011269 A MX2013011269 A MX 2013011269A
- Authority
- MX
- Mexico
- Prior art keywords
- gas turbine
- turbine engine
- testing
- compressed air
- components
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/14—Testing gas-turbine engines or jet-propulsion engines
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Testing Of Engines (AREA)
Abstract
Se describen un sistema y un procedimiento para probar un motor de turbina de gas o componente del mismo, especialmente para un motor de turbina de gas tipo aviación grande; y un procedimiento para probar un motor de turbina de gas industrial grande que requiere de grandes relaciones de capacidad de flujo y de presión. El sistema y el procedimiento pueden incluir el uso de un depósito grande de aire comprimido para proporcionar aire comprimido al sistema de prueba. Además, el sistema y el procedimiento también pueden incluir el uso de un sistema de precalentamiento, el cual puede incluir un calentador y un dispositivo intercambiador térmico, para calentar el aire comprimido del depósito de almacenamiento de aire comprimido a una temperatura adecuada para simular condiciones normales de operación del motor de turbina de gas o componente del mismo.
Applications Claiming Priority (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161468771P | 2011-03-29 | 2011-03-29 | |
US201113108029A | 2011-05-16 | 2011-05-16 | |
US201161561956P | 2011-11-21 | 2011-11-21 | |
US201161569378P | 2011-12-12 | 2011-12-12 | |
US201261587022P | 2012-01-16 | 2012-01-16 | |
US201213410051A | 2012-03-01 | 2012-03-01 | |
PCT/US2012/029231 WO2012134824A1 (en) | 2011-03-29 | 2012-03-15 | Apparatus and process for testing an industrial gas turbine engine and components thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2013011269A true MX2013011269A (es) | 2014-03-27 |
MX339093B MX339093B (es) | 2016-05-10 |
Family
ID=46931843
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2013011269A MX339093B (es) | 2011-03-29 | 2012-03-15 | Aparato y procedimiento para probar un motor de turbina de gas industrial y componentes del mismo. |
Country Status (12)
Country | Link |
---|---|
US (1) | US9200983B2 (es) |
EP (1) | EP2691757B1 (es) |
CN (1) | CN103597333B (es) |
AU (1) | AU2012237974B2 (es) |
BR (1) | BR112013025204A2 (es) |
CA (1) | CA2831668C (es) |
DK (1) | DK2691757T3 (es) |
MX (1) | MX339093B (es) |
PL (1) | PL2691757T3 (es) |
PT (1) | PT2691757T (es) |
RU (1) | RU2013148004A (es) |
WO (1) | WO2012134824A1 (es) |
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US9410869B2 (en) * | 2011-03-29 | 2016-08-09 | S & J Design Llc | Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir |
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US10823054B2 (en) * | 2012-11-06 | 2020-11-03 | Fuad AL MAHMOOD | Reducing the load consumed by gas turbine compressor and maximizing turbine mass flow |
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US9255493B2 (en) * | 2014-05-23 | 2016-02-09 | Yee-Chang Feng | Clean energy generation system |
CN104456947B (zh) * | 2014-10-17 | 2018-02-13 | 北京航天益森风洞工程技术有限公司 | 蓄热式纯净空气加热系统 |
CN104777002B (zh) * | 2015-03-19 | 2017-08-25 | 西北工业大学 | 一种甲烷燃烧加热的超燃冲压发动机燃烧室实验系统 |
CN104764610A (zh) * | 2015-03-30 | 2015-07-08 | 西北工业大学 | 一种试验气体污染对超音速燃烧室性能影响的试验系统 |
CN104931248B (zh) * | 2015-06-23 | 2018-06-01 | 江苏大学 | 一种高压余能回收液力透平试验台及其控制方法 |
WO2017058709A1 (en) * | 2015-09-30 | 2017-04-06 | Florida Turbine Technologies, Inc. | Caes combustor test facility |
BE1023509B1 (fr) * | 2015-10-09 | 2017-04-11 | Safran Aero Boosters S.A. | Banc de test de turbomachine sur bateau |
CA2914247C (en) * | 2015-11-06 | 2023-03-28 | Florida Turbine Technologies, Inc. | Process for testing a compressor or a combustor of a gas turbine engine using a large compressed air storage reservoir |
CN105738120B (zh) * | 2016-03-17 | 2018-04-20 | 上海发电设备成套设计研究院 | 重型燃机透平叶片全温全压冷效试验装置 |
CN105756727B (zh) * | 2016-04-26 | 2017-09-15 | 中科合肥微小型燃气轮机研究院有限责任公司 | 一种用于燃气轮机试验台的综合气源系统 |
CN106017935B (zh) * | 2016-05-17 | 2018-09-04 | 大连理工大学 | 一种紧固试验用航空发动机低压涡轮轴分体化试件及其设计方法 |
RU2623619C1 (ru) * | 2016-08-30 | 2017-06-28 | Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") | Способ испытания авиационного газотурбинного двигателя |
US10288520B1 (en) * | 2017-02-24 | 2019-05-14 | Florida Turbine Technologies, Inc | Apparatus and process for testing an aero vehicle at high Mach number |
WO2018164713A1 (en) | 2017-03-08 | 2018-09-13 | Florida Turbine Technologies, Inc. | Apparatus and process for testing a large combustor using a caes facility |
CN107764553A (zh) * | 2017-10-23 | 2018-03-06 | 北京理工大学 | 一种可调节的进气预热装置试验系统 |
CN109883714A (zh) * | 2019-02-13 | 2019-06-14 | 中国船舶重工集团公司第七O三研究所无锡分部 | 一种燃气轮机试验台进气盐雾装置 |
US11486795B2 (en) | 2019-05-16 | 2022-11-01 | Textron Innovations, Inc. | Engine testing system and process |
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CN110208025B (zh) * | 2019-06-24 | 2024-05-07 | 中国矿业大学 | 一种多类型矿井乏风换热器热湿交换性能测试装置 |
RU2725114C1 (ru) * | 2019-10-24 | 2020-06-29 | Акционерное общество "Корпорация "Тактическое ракетное вооружение" | Способ проверки работоспособности газовых редукторов летательных аппаратов и пневматический испытательный стенд для его осуществления |
CN110887683A (zh) * | 2019-12-09 | 2020-03-17 | 中国人民解放军国防科技大学 | 一种电加热式的超声速引射器实验系统 |
US20210207611A1 (en) * | 2020-01-02 | 2021-07-08 | Viettel Group | Airflow amplifier device for testing purpose |
CN112601308B (zh) * | 2020-12-16 | 2023-05-12 | 北京航天益森风洞工程技术有限公司 | 一种加热大流量空气的组合感应加热系统 |
CN113301678A (zh) * | 2021-05-25 | 2021-08-24 | 北京化工大学 | 一种感应加热装置和微流亚跨超音速高温风洞设备 |
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-
2012
- 2012-03-15 EP EP12712183.8A patent/EP2691757B1/en active Active
- 2012-03-15 AU AU2012237974A patent/AU2012237974B2/en active Active
- 2012-03-15 WO PCT/US2012/029231 patent/WO2012134824A1/en active Application Filing
- 2012-03-15 PT PT127121838T patent/PT2691757T/pt unknown
- 2012-03-15 PL PL12712183T patent/PL2691757T3/pl unknown
- 2012-03-15 MX MX2013011269A patent/MX339093B/es active IP Right Grant
- 2012-03-15 DK DK12712183.8T patent/DK2691757T3/en active
- 2012-03-15 RU RU2013148004/06A patent/RU2013148004A/ru not_active Application Discontinuation
- 2012-03-15 US US14/008,308 patent/US9200983B2/en active Active
- 2012-03-15 BR BR112013025204-9A patent/BR112013025204A2/pt not_active Application Discontinuation
- 2012-03-15 CA CA2831668A patent/CA2831668C/en active Active
- 2012-03-15 CN CN201280026244.6A patent/CN103597333B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
CA2831668A1 (en) | 2012-10-04 |
BR112013025204A2 (pt) | 2020-10-20 |
PT2691757T (pt) | 2017-06-06 |
EP2691757A1 (en) | 2014-02-05 |
RU2013148004A (ru) | 2015-05-10 |
DK2691757T3 (en) | 2017-05-22 |
AU2012237974B2 (en) | 2015-08-13 |
EP2691757B1 (en) | 2017-05-03 |
CA2831668C (en) | 2016-06-21 |
CN103597333B (zh) | 2017-03-29 |
PL2691757T3 (pl) | 2017-09-29 |
AU2012237974A1 (en) | 2013-10-24 |
WO2012134824A1 (en) | 2012-10-04 |
US20140053641A1 (en) | 2014-02-27 |
CN103597333A (zh) | 2014-02-19 |
US9200983B2 (en) | 2015-12-01 |
MX339093B (es) | 2016-05-10 |
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