CN110909433A - Gas turbine compressor rotor fir-shaped tenon-mortise connection structure optimization method - Google Patents
Gas turbine compressor rotor fir-shaped tenon-mortise connection structure optimization method Download PDFInfo
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- CN110909433A CN110909433A CN201911269375.7A CN201911269375A CN110909433A CN 110909433 A CN110909433 A CN 110909433A CN 201911269375 A CN201911269375 A CN 201911269375A CN 110909433 A CN110909433 A CN 110909433A
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- 238000000034 method Methods 0.000 title claims abstract description 36
- 238000005457 optimization Methods 0.000 title claims abstract description 25
- 238000009826 distribution Methods 0.000 claims abstract description 10
- 238000009434 installation Methods 0.000 claims abstract description 7
- 238000013461 design Methods 0.000 claims description 22
- 239000011159 matrix material Substances 0.000 claims description 9
- 238000004364 calculation method Methods 0.000 claims description 7
- 238000004458 analytical method Methods 0.000 claims description 4
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Classifications
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- 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
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- 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
- F04D29/601—Mounting; Assembling; Disassembling specially adapted for elastic fluid pumps
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
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- Structures Of Non-Positive Displacement Pumps (AREA)
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CN201911269375.7A CN110909433B (en) | 2019-12-11 | 2019-12-11 | Optimization method for fir-type tenon-mortise connection structure of gas turbine compressor rotor |
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CN201911269375.7A CN110909433B (en) | 2019-12-11 | 2019-12-11 | Optimization method for fir-type tenon-mortise connection structure of gas turbine compressor rotor |
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CN110909433A true CN110909433A (en) | 2020-03-24 |
CN110909433B CN110909433B (en) | 2023-06-20 |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111579396A (en) * | 2020-04-29 | 2020-08-25 | 南京航空航天大学 | Optimization method of turbine joggling fretting fatigue test piece |
CN112287580A (en) * | 2020-10-27 | 2021-01-29 | 中国船舶重工集团公司第七0三研究所 | Axial flow compressor surge boundary calculation method based on full three-dimensional numerical simulation |
CN112324520A (en) * | 2020-10-27 | 2021-02-05 | 中国船舶重工集团公司第七0三研究所 | Stationary blade ring structure of gas turbine |
CN112685852A (en) * | 2020-12-22 | 2021-04-20 | 中国船舶重工集团公司第七0三研究所 | Axial flow compressor load customized pneumatic optimization method capable of keeping continuity of through-flow structure |
CN115060439A (en) * | 2022-05-30 | 2022-09-16 | 大连理工大学 | Contact stiffness and damping identification device and identification method of tenon joint structure |
CN115628115A (en) * | 2022-10-25 | 2023-01-20 | 中国科学院工程热物理研究所 | Method and device for repairing tenon and groove of annular blade of compressor case |
Citations (5)
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CN203308525U (en) * | 2013-05-07 | 2013-11-27 | 中国航空动力机械研究所 | Fir tree-shaped tenon structure |
CN204312392U (en) * | 2014-11-15 | 2015-05-06 | 哈尔滨广瀚燃气轮机有限公司 | For installing novel tenon and the tongue-and-groove linkage structure of compressor blade and drum-type wheel disc |
CN105756719A (en) * | 2016-01-08 | 2016-07-13 | 北京航空航天大学 | Gas compressor stator blade root slotting method based on optimization algorithm |
CN107301268A (en) * | 2017-05-18 | 2017-10-27 | 哈尔滨工程大学 | A kind of ship gas turbine variable stator vane angle compressor deflection angle optimization method |
CN110489925A (en) * | 2019-09-02 | 2019-11-22 | 杭州汽轮动力集团有限公司 | A kind of Gas Turbine fir-tree root leaf slot modular design method |
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2019
- 2019-12-11 CN CN201911269375.7A patent/CN110909433B/en active Active
Patent Citations (5)
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CN203308525U (en) * | 2013-05-07 | 2013-11-27 | 中国航空动力机械研究所 | Fir tree-shaped tenon structure |
CN204312392U (en) * | 2014-11-15 | 2015-05-06 | 哈尔滨广瀚燃气轮机有限公司 | For installing novel tenon and the tongue-and-groove linkage structure of compressor blade and drum-type wheel disc |
CN105756719A (en) * | 2016-01-08 | 2016-07-13 | 北京航空航天大学 | Gas compressor stator blade root slotting method based on optimization algorithm |
CN107301268A (en) * | 2017-05-18 | 2017-10-27 | 哈尔滨工程大学 | A kind of ship gas turbine variable stator vane angle compressor deflection angle optimization method |
CN110489925A (en) * | 2019-09-02 | 2019-11-22 | 杭州汽轮动力集团有限公司 | A kind of Gas Turbine fir-tree root leaf slot modular design method |
Non-Patent Citations (11)
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LING J 等: ""Optimal Turbulent Schmidt Number for RANS Modeling of Trailing Edge Slot Film Cooling"", 《JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER》 * |
倪长辉 等: ""基于接触应力的高参数汽轮机叶片枞树形叶根型线优化"", 《计算机辅助工程》 * |
唐钊: ""发动机冷却风扇叶片参数的研究和优化"", 《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》 * |
宗洪明 等: "某型燃气轮机枞树形榫接结构多齿形参数优化分析" * |
张明辉 等: ""基于三维热弹性接触的汽轮机调节级叶片枞树型叶根轮缘结构的优化"", 《动力工程学报》 * |
张晓磊: ""重型燃气轮机压气机叶片机械加工技术研究"", 《中国优秀硕士学位论文全文数据库工程科技Ⅰ辑》 * |
李骏;宋友辉;刘汉斌;徐凌志;郭昊雁;: "涡轮叶片-榫头-轮盘的蠕变与低循环疲劳寿命预测" * |
杨敏超 等: "涡轮榫头/榫槽的结构优化设计" * |
王斌: ""涡轮盘枞树型叶根榫槽切削刀具结构优化及强度预测"", 《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》 * |
王琦 等: ""定制叶型在多级压气机中的应用研究"", 《热能动力工程》 * |
高翔 等: ""航空发动机榫槽拉刀快速设计系统研究与开发"", 《机械制造与自动化》 * |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111579396A (en) * | 2020-04-29 | 2020-08-25 | 南京航空航天大学 | Optimization method of turbine joggling fretting fatigue test piece |
CN111579396B (en) * | 2020-04-29 | 2021-08-06 | 南京航空航天大学 | An optimization method for turbine tenon joint fretting fatigue test piece |
CN112287580A (en) * | 2020-10-27 | 2021-01-29 | 中国船舶重工集团公司第七0三研究所 | Axial flow compressor surge boundary calculation method based on full three-dimensional numerical simulation |
CN112324520A (en) * | 2020-10-27 | 2021-02-05 | 中国船舶重工集团公司第七0三研究所 | Stationary blade ring structure of gas turbine |
CN112324520B (en) * | 2020-10-27 | 2022-08-30 | 中国船舶重工集团公司第七0三研究所 | Stationary blade ring structure of gas turbine |
CN112685852A (en) * | 2020-12-22 | 2021-04-20 | 中国船舶重工集团公司第七0三研究所 | Axial flow compressor load customized pneumatic optimization method capable of keeping continuity of through-flow structure |
CN115060439A (en) * | 2022-05-30 | 2022-09-16 | 大连理工大学 | Contact stiffness and damping identification device and identification method of tenon joint structure |
CN115628115A (en) * | 2022-10-25 | 2023-01-20 | 中国科学院工程热物理研究所 | Method and device for repairing tenon and groove of annular blade of compressor case |
CN115628115B (en) * | 2022-10-25 | 2025-04-15 | 中国科学院工程热物理研究所 | A method and device for repairing the tenon groove of annular blades of a compressor casing |
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CN110909433B (en) | 2023-06-20 |
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