CN113266473A - Method for measuring starting resistance moment of aero-engine under non-loading condition - Google Patents
Method for measuring starting resistance moment of aero-engine under non-loading condition Download PDFInfo
- Publication number
- CN113266473A CN113266473A CN202110609249.2A CN202110609249A CN113266473A CN 113266473 A CN113266473 A CN 113266473A CN 202110609249 A CN202110609249 A CN 202110609249A CN 113266473 A CN113266473 A CN 113266473A
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- Prior art keywords
- engine
- starting
- air
- torque
- measuring
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- 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
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
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- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
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- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
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- 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
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Engines (AREA)
Abstract
Description
Claims (7)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202110609249.2A CN113266473B (en) | 2021-06-01 | 2021-06-01 | Method for measuring starting resistance moment of aero-engine under non-loading condition |
Applications Claiming Priority (1)
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CN202110609249.2A CN113266473B (en) | 2021-06-01 | 2021-06-01 | Method for measuring starting resistance moment of aero-engine under non-loading condition |
Publications (2)
Publication Number | Publication Date |
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CN113266473A true CN113266473A (en) | 2021-08-17 |
CN113266473B CN113266473B (en) | 2022-10-28 |
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Family Applications (1)
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CN202110609249.2A Active CN113266473B (en) | 2021-06-01 | 2021-06-01 | Method for measuring starting resistance moment of aero-engine under non-loading condition |
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CN (1) | CN113266473B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114136644A (en) * | 2021-10-20 | 2022-03-04 | 中国航发四川燃气涡轮研究院 | Device and method for measuring resistance of air inlet channel in aircraft engine ground platform test |
CN114935419A (en) * | 2022-05-19 | 2022-08-23 | 中国航发沈阳发动机研究所 | Method for evaluating power characteristics of aircraft engine starter under installation condition |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106342205B (en) * | 2010-08-31 | 2013-12-11 | 中国兵器工业集团第七○研究所 | Engine start moment of resistance method of testing |
CN107916997A (en) * | 2016-10-11 | 2018-04-17 | 和谐工业有限责任公司 | Integrated actuating device for aircraft |
US20180266328A1 (en) * | 2017-03-17 | 2018-09-20 | Hamilton Sundstrand Corporation | Air turbine starter with automated variable inlet vanes |
US20200003072A1 (en) * | 2018-06-28 | 2020-01-02 | Hamilton Sundstrand Corporation | Air turbine starter with turbine air exhaust outlet valve |
CN112729856A (en) * | 2020-12-23 | 2021-04-30 | 南京航腾机电科技有限公司 | Measurement and control system of air turbine starter comprehensive test bed |
-
2021
- 2021-06-01 CN CN202110609249.2A patent/CN113266473B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106342205B (en) * | 2010-08-31 | 2013-12-11 | 中国兵器工业集团第七○研究所 | Engine start moment of resistance method of testing |
CN107916997A (en) * | 2016-10-11 | 2018-04-17 | 和谐工业有限责任公司 | Integrated actuating device for aircraft |
US20180266328A1 (en) * | 2017-03-17 | 2018-09-20 | Hamilton Sundstrand Corporation | Air turbine starter with automated variable inlet vanes |
US20200003072A1 (en) * | 2018-06-28 | 2020-01-02 | Hamilton Sundstrand Corporation | Air turbine starter with turbine air exhaust outlet valve |
CN112729856A (en) * | 2020-12-23 | 2021-04-30 | 南京航腾机电科技有限公司 | Measurement and control system of air turbine starter comprehensive test bed |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114136644A (en) * | 2021-10-20 | 2022-03-04 | 中国航发四川燃气涡轮研究院 | Device and method for measuring resistance of air inlet channel in aircraft engine ground platform test |
CN114136644B (en) * | 2021-10-20 | 2023-09-19 | 中国航发四川燃气涡轮研究院 | Aeroengine ground table test air inlet channel resistance measuring device and method |
CN114935419A (en) * | 2022-05-19 | 2022-08-23 | 中国航发沈阳发动机研究所 | Method for evaluating power characteristics of aircraft engine starter under installation condition |
CN114935419B (en) * | 2022-05-19 | 2023-09-22 | 中国航发沈阳发动机研究所 | Method for evaluating power characteristics of starter of aero-engine under installed condition |
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CN113266473B (en) | 2022-10-28 |
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TA01 | Transfer of patent application right |
Effective date of registration: 20220406 Address after: 1901 MoMA building, 199 Chaoyang North Road, Chaoyang District, Beijing 100020 Applicant after: BEIJING QINGRUAN CHUANGXIANG INFORMATION TECHNOLOGY Co.,Ltd. Applicant after: AVIC SHENYANG AIRCRAFT DESIGN & Research Institute Address before: Thavorn street in Huanggu District of Shenyang city of Liaoning Province, No. 40 110035 Applicant before: AVIC SHENYANG AIRCRAFT DESIGN & Research Institute |
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TA01 | Transfer of patent application right | ||
TA01 | Transfer of patent application right |
Effective date of registration: 20220914 Address after: Thavorn street in Huanggu District of Shenyang city of Liaoning Province, No. 40 110035 Applicant after: AVIC SHENYANG AIRCRAFT DESIGN & Research Institute Address before: 1901 MoMA building, 199 Chaoyang North Road, Chaoyang District, Beijing 100020 Applicant before: BEIJING QINGRUAN CHUANGXIANG INFORMATION TECHNOLOGY Co.,Ltd. Applicant before: AVIC SHENYANG AIRCRAFT DESIGN & Research Institute |
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