supported by the National Key Research and Development Program of China(No.2019YFB1704500);the National Natural Science Foundation of China(No.51875428);the Key Research and Development Program of Hubei Province,China(No.2020BAB144);the Excellent Youth Foundation of Hubei Province,China(No.2019CFA041);the Innovative Research Team Development Program of Ministry of Education of China(No.IRT_17R83);the 111 Project of China(No.B17034)。
The aeroengine casing ring forgings have complex cross-section shapes,when the conventional ultrasonic or phased array is applied to detect such curved surfaces,the inspection images always have low resolution and eve...
To investigate the containment characteristics and mechanisms of axial compressor blade and casing in turboshaft engine,experimental and simulation research is conducted on Titanium alloy axial compressor blades and s...
co-supported by the Young Scientists Fund of the National Natural Science Foundation of China(No.51905025);the Joint Funds of the National Natural Science Foundation of China(No.U1708257);the Fundamental Research Funds for the Central Universities(No.JD1911)。
Bearings in a gas turbine engine are the key connecting components transmitting force and motion between rotors and thin-walled flexible casing.The bearing stiffness and damping of squeeze film damper(SFD)nearby beari...
supported by the National Natural Science Foundation of China(No.51676005)。
Squealer tip is widely used in turbines to reduce tip leakage loss.In typical turbine environment,the squealer tip leakage flow is affected by multiple factors such as the relative casing motion and the wide range of ...
supported by the Chinese Aviation Propulsion Technology Development Program (No. APTD-1103-07)
Aramid fabrics have been commonly used in the civil turbofan engine fan blade containment system for its excellent performance. To investigate the behavior and capability of soft wall containment casing, a series of f...
supported by the National Natural Science Foundation of China (Nos. 51790514, 11661141020 and 51576008)
Casing treatment is a mature stabilization technique which has been widely applied on aero-engines for modern aircrafts and turbo-chargers for automobiles. After the investigations of half century since the 1960 s, th...
supported by the National Natural Science Foundation of China (No.51236006);Advanced Aeroengine Collaborative Innovation Center
This paper presents the aspirated modification of a dual-stage counter-rotating compressor which contains inlet guide vanes(IGVs), two counter-rotating rotors(R1, R2), and outlet guide vanes(OGVs).Uniform circul...
In order to reduce the losses caused by tip-leakage flow, axisymmetric contouring is applied to the casing of a two-stage unshrouded high pressure turbine(HPT) of aero-engine in this paper. This investigation focuse...
Enhancing containment capability and reducing weight are always great concerns in the design of casings. Ballistic tests can help to mitigate a catastrophic event after a blade out, yet taking time and costing money. ...
Ballistic impact test of different-scale casings is an efficient way to demonstrate the casing containment capability at the preliminary design stage of the engine. For the sake of studying the titanium alloy TC4 casi...