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Effects of Inlet Swirl Distortion on a Multi-Stage Compressor with Inlet Guide Vanes and Stall Margin Enhancement Method

open access: yesAerospace, 2023
Inlet swirl distortion is generally considered as a type of velocity distortion, and inlet guide vanes (IGVs) are widely used in the multi-stage compressor of aero-engines to eliminate the tangential velocity of the swirl flow.
Yibo Fang   +3 more
doaj   +4 more sources

A review on aero-engine inlet-compressor integration and inlet flow distortion in axial compressors

open access: yesFundamental Research
The air intake-compression systems of modern aircraft usually use the aero-engine intake and fan/compressor as the main components. Inlet-engine compatibility has always been the key to the stable and safe operation of the propulsion system, including ...
Zhenyu Li   +3 more
doaj   +5 more sources

Numerical simulation of S-shaped inlet under the intake total pressure distortion [PDF]

open access: yesMATEC Web of Conferences, 2022
During the development of the stealth fighter, the S-shaped inlet enters the designer’s vision because it has better stealth than bump inlet and straight inlet. During the use of the S-shaped inlet, due to its structural reasons, secondary flow is likely
Liu Ying   +5 more
doaj   +2 more sources

An Efficient Approach for Identification of the Inlet Distortion of Engine Based on Acoustic Emission Technique

open access: yesApplied Sciences, 2020
Effective and accurate diagnosis of engine health is key to ensuring the safe operation of engines. Inlet distortion is due to the flow or the pressure variations.
Jiaoyan Huang   +4 more
doaj   +2 more sources

Development of Block type Inlet Distortion Simulating Device for Gas Turbine Engine Inlet Distortion Test

open access: yesInternational Journal of Aeronautical and Space Sciences, 2007
In late 1960's, engineers of the engine manufacturer experienced that the distortion of inlet flow of turbofan and turbojet engine could cause the surge in compressor and affect overall engine operational performance, which result in the deterioration of stability of the engine.
Kyung-Jae Lee   +6 more
exaly   +3 more sources

Using Tip Injection to Stability Enhancement of a Transonic Centrifugal Impeller with Inlet Distortion [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2022
This paper aims to understand the effects of circumferential inlet distortion and tip injection on a transonic impeller performance and flow field. For distorted inflow, the impeller is subjected to a stationary 120-degrees circumferential total pressure
Z. Jahani, H. Khaleghi, S. Tabejamaat
doaj   +1 more source

Effect of insert plate on the inlet pressure distortion of the aero-engine

open access: yesAdvances in Mechanical Engineering, 2023
The shape of the inlet duct and other factors cause distortion of the total pressure, leading to a decrease in engine stability. This article inserts flat plate into the inlet port of a certain type of aviation turbojet engine to conduct an inlet ...
Chenxin He   +4 more
doaj   +1 more source

Improved Thrust Performance Optimization Method for UAVs Based on the Adaptive Margin Control Approach

open access: yesMathematics, 2023
This study proposes a strategy for improving the thrust performance of fixed-wing UAV turbine engines from the perspective of aircraft/engine integration.
Yeguang Wang, Honglin Liu, Kai Liu
doaj   +1 more source

A Modified Circumferentially Averaged Method for Compressor Performance under Inlet Distortion

open access: yesAerospace, 2023
Inlet distortion detrimentally affects the aerodynamic performance and lessens the stability of compressors, and has received considerable attention. The need to accurately estimate its effect on the performance and stability of compressor as early as ...
Yang Zhao, Donghai Jin, Xingmin Gui
doaj   +1 more source

Numerical Simulation on the Influence of Inlet Flow Characteristics on the Performance of a Centrifugal Compressor

open access: yesEnergies, 2023
Although inlet bent pipes are usually adopted due to limited installation space, the influences of different bend pipes on the inlet flow characteristics and performance of centrifugal compressors are still unclear.
Xing Li   +6 more
doaj   +1 more source

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