Harbin Engineering University

Harbin Medical University

Jie Yang

Xinyu Zhang

Jie Guo

Yipeng Cao

Xiaochen Zhao

Chen Liu

Yang Liu

Xilin Sun

Kai Wang

Lili Yang

Wenping Zhang

Lina Wu

Runze Zhang

Gongmin Liu

Zequn Ma

Shuang Liu

Changhong Sun

Shaoran Du

Yao Song

Jiaxuan Lin

Haoxiang Li

Yingbo Li

Xu Zhan

Zexi Wu

Xiaona Li

A method and apparatus for acquiring aerodynamic noise of a compressor, a medium, and a product are provided. The method includes: performing inverse Fourier transform on a known frequency-domain noise spectrum to obtain known time-domain noise data, then predicting unknown time-domain noise using a time series neural network, obtaining finer time-frequency noise data in combination with the known time-frequency noise data, and finally, performing Fourier transform on the finer time-frequency noise data to obtain new frequency-domain noise data. Limitations of a limited time step and a total simulation time on the acquisition of aerodynamic noise data in traditional numerical calculation of aerodynamic noise can be overcome. Finer aerodynamic noise data can be acquired rapidly and accurately. The frequency resolution of the noise spectrum can be increased, and reducing the consumption of computing resources and saving manpower and material resources can be achieved.

Method and apparatus for acquiring aerodynamic noise of compressor, medium, and product

A noise-reducing and nonuniform tip clearance structure of centrifugal compressor is provided, which includes a compressor impeller body and a compressor impeller shroud. The compressor impeller shroud is circumferentially wrapped outside the compressor impeller body, and multiple impeller blade bodies are uniformly arranged in a circumferential direction of the compressor impeller body. A clearance between an impeller tip meridian line of the impeller blade body and an impeller shroud meridian line on the compressor impeller shroud is an impeller tip clearance. The impeller tip clearance gradually decreases in a direction from a leading edge to a trailing edge of the impeller blade body, and a change rate of the impeller tip clearance in the direction from the leading edge to the trailing edge of the impeller blade body also gradually decreases.

Noise-reducing and nonuniform tip clearance structure of centrifugal compressor

Provided is an intake bypass recirculation structure capable of silencing, including: an intake bypass recirculation structure body and a structure-conducted silencing device. An intake bypass recirculation cavity is provided on the intake bypass recirculation structure body. An inlet of the intake bypass recirculation structure and an outlet of the intake bypass recirculation structure that are provided on the intake bypass recirculation structure body are each connected to the intake bypass recirculation cavity. The structure-conducted silencing device is disposed inside the intake bypass recirculation cavity. In this application, during working, noise generated by a compressor is transmitted into the intake bypass recirculation cavity via an inlet of the intake bypass recirculation structure, and transmitted outside via the outlet of the intake bypass recirculation structure.

Intake bypass recirculation structure capable of silencing

Some embodiments of the disclosure provide an air intake bypass recirculation structure with adjustable air entraining amount and controllable broadband noise which includes main body of the air intake bypass recirculation structure and an air entraining amount adjusting structure. In some examples, an air intake bypass recirculation cavity is formed in the main body of the air intake bypass recirculation structure. An air inlet of an air intake pipe and an air outlet of the air intake pipe are formed in two ends of the main body of the air intake bypass recirculation structure respectively. An airflow inlet of the air intake bypass recirculation structure and an airflow outlet of the air intake bypass recirculation structure are formed in the inner side of the main body of the air intake bypass recirculation structure. The air entraining amount adjusting structure is arranged in the air intake bypass recirculation cavity.

Air intake bypass recirculation structure with adjustable air entraining amount and controllable broadband noise

The present invention provides aF-MR/fluorescence multi-mode molecular imaging and drug loading diagnosis-treatment integrated nanoprobe, and a preparation method and an application. The nano-probe is a nanoparticle formed by coating a mixture of a surfactant containing a molecular targeting treatment drug and a fluorescent dye with a Perfluorocarbon (PFC) carrier; and by uniformly dispersing a mixed solution into water and glycerol, processing ultrasonically, removing a component which is not effectively coated, and purifying, the drug-loading nanoparticle capable of being used for 19 F-MR imaging may be prepared. The nano-probe may implement in-vivo 19F-MR molecular imaging; a carried molecular targeting treatment drug can implement targeted binding and targeted treatment; and by virtue of a characteristic that PFC in a nucleus may carry and release oxygen massively, an anaerobious microenvironment in the tumor is improved, a chemosensitization effect is achieved, and thus the diagnosis-treatment integration of the tumor is implemented finally.

Diagnosis-treatment integrated nano-probe forF-MR/fluorescence multi-mode molecular imaging and drug-loading and preparation method and application of nano-probe

Growing community of inventors

Harbin City, Heilongjiang, China

Jie Yang