AU2020101455A4 - Online monitoring method for stability of aero compressor system under distorted inflow - Google Patents
Online monitoring method for stability of aero compressor system under distorted inflow Download PDFInfo
- Publication number
- AU2020101455A4 AU2020101455A4 AU2020101455A AU2020101455A AU2020101455A4 AU 2020101455 A4 AU2020101455 A4 AU 2020101455A4 AU 2020101455 A AU2020101455 A AU 2020101455A AU 2020101455 A AU2020101455 A AU 2020101455A AU 2020101455 A4 AU2020101455 A4 AU 2020101455A4
- Authority
- AU
- Australia
- Prior art keywords
- compressor
- dynamic pressure
- similarity coefficient
- rotor
- sct
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
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
- F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
- F04D27/001—Testing thereof; Determination or simulation of flow characteristics; Stall or surge detection, e.g. condition monitoring
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010003731.7 | 2020-01-03 | ||
CN202010003731.7A CN111140532B (zh) | 2020-01-03 | 2020-01-03 | 一种畸变来流条件下航空压气机系统稳定性在线监测方法 |
Publications (1)
Publication Number | Publication Date |
---|---|
AU2020101455A4 true AU2020101455A4 (en) | 2020-08-27 |
Family
ID=70523349
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2020101455A Active AU2020101455A4 (en) | 2020-01-03 | 2020-07-23 | Online monitoring method for stability of aero compressor system under distorted inflow |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN111140532B (zh) |
AU (1) | AU2020101455A4 (zh) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116659769A (zh) * | 2023-05-30 | 2023-08-29 | 中国民用航空飞行学院 | 一种用于轴流压气机封严腔泄漏流识别与检测的方法 |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116658451B (zh) * | 2023-08-02 | 2023-10-03 | 中国航发四川燃气涡轮研究院 | 基于尾迹损失的核心机环境下压气机出口总压修正方法 |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101887479B (zh) * | 2010-07-23 | 2012-05-09 | 华南理工大学 | 基于确定学习理论的轴流压气机旋转失速的快速诊断方法 |
CN102022351B (zh) * | 2010-12-08 | 2012-06-27 | 北京航空航天大学 | 一种拓宽高负荷轴流压气机稳定工作范围的方法 |
KR101466267B1 (ko) * | 2013-02-27 | 2014-11-28 | 삼성중공업 주식회사 | 축류팬의 스톨 감지 장치 |
CN103216461B (zh) * | 2013-04-17 | 2016-01-13 | 南京航空航天大学 | 轴流式压气机的失速先兆识别方法 |
CN105298889B (zh) * | 2015-09-24 | 2017-02-01 | 西北工业大学 | 一种压气机喘振的检测方法 |
CN107165850B (zh) * | 2017-06-27 | 2018-11-23 | 西北工业大学 | 一种基于频域驼峰识别的轴流压气机旋转失速预警方法 |
CN109815624B (zh) * | 2019-02-21 | 2022-01-04 | 南京航空航天大学 | 一种考虑进气总压畸变影响的压气机稳定边界判断方法 |
CN110195716A (zh) * | 2019-07-19 | 2019-09-03 | 中国航发沈阳发动机研究所 | 一种压气机进气畸变试验系统及方法 |
CN110454441A (zh) * | 2019-08-30 | 2019-11-15 | 康跃科技股份有限公司 | 一种进气畸变约束装置及具有该装置的离心压缩机 |
CN110608187A (zh) * | 2019-10-30 | 2019-12-24 | 江西理工大学 | 基于频率特征变化的轴流压气机失速喘振预测装置 |
-
2020
- 2020-01-03 CN CN202010003731.7A patent/CN111140532B/zh active Active
- 2020-07-23 AU AU2020101455A patent/AU2020101455A4/en active Active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116659769A (zh) * | 2023-05-30 | 2023-08-29 | 中国民用航空飞行学院 | 一种用于轴流压气机封严腔泄漏流识别与检测的方法 |
CN116659769B (zh) * | 2023-05-30 | 2024-01-23 | 中国民用航空飞行学院 | 一种用于轴流压气机封严腔泄漏流识别与检测的方法 |
Also Published As
Publication number | Publication date |
---|---|
CN111140532A (zh) | 2020-05-12 |
CN111140532B (zh) | 2020-11-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
AU2020101455A4 (en) | Online monitoring method for stability of aero compressor system under distorted inflow | |
Camp et al. | 1997 Best Paper Award—Turbomachinery Committee: a study of spike and modal stall phenomena in a low-speed axial compressor | |
Schulz et al. | Experimental investigation of the three-dimensional flow in an annular compressor cascade | |
Wang et al. | Evolution of the flow instabilities in an axial compressor rotor with large tip clearance: An experimental and URANS study | |
Hodson et al. | An investigation of boundary layer development in a multistage LP turbine | |
CN106640722B (zh) | 一种压气机气动稳定性诊断和控制的装置及方法 | |
CN107165850B (zh) | 一种基于频域驼峰识别的轴流压气机旋转失速预警方法 | |
CN104296714B (zh) | 一种涡轮凹腔叶片叶尖间隙测量方法 | |
EP2026160A1 (en) | Event monitoring via combination of signals | |
Orth | Unsteady boundary-layer transition in flow periodically disturbed by wakes | |
CN110608187A (zh) | 基于频率特征变化的轴流压气机失速喘振预测装置 | |
CN110080833B (zh) | 一种改善机组调峰的汽轮机高调门调频能力的评估方法 | |
CN112580267A (zh) | 基于多分支特征融合网络的航空发动机喘振预测方法 | |
CN111828103A (zh) | 一种汽轮机深度调峰运行叶片颤振区在线判别方法 | |
Weichert et al. | Detailed measurements of spike formation in an axial compressor | |
Walker et al. | Periodic transition on an axial compressor stator: Incidence and clocking effects: Part I—Experimental data | |
Wang et al. | The effects on stability, performance, and tip leakage flow of recirculating casing treatment in a subsonic axial flow compressor | |
Jackson | Stall cell development in an axial compressor | |
CN102900564B (zh) | 用于轴流压缩系统叶顶喷气稳定性控制的控制器 | |
RU2382909C2 (ru) | Способ диагностики помпажа компрессора | |
RU2354851C1 (ru) | Способ контроля режимов работы компрессора и устройство для его осуществления | |
US6755617B2 (en) | Method for the early detection of aerodynamic instabilities in a turbomachine compressor | |
US7269954B2 (en) | Method for operating a gas turbine installation, and gas turbine installation | |
CN114542402A (zh) | 一种基于多参量分析的风电叶片故障类型在线诊断方法及系统 | |
Walker et al. | Periodic Transition on an Axial Compressor Stator—Incidence and Clocking Effects: Part I—Experimental Data |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FGI | Letters patent sealed or granted (innovation patent) |