Issues with the inlet booster of the Fuxin compressor
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I heard that there is a turbocharger at the inlet of the Fu Xin compressor. What is its design? It is said to be able to convert kinetic energy into pressure, thereby reducing the power required by the rich gas compressor. Does anyone know anything about this? ? ?
I’ve been looking at what you said for a long time but still can’t understand it; moreover, I’ve never heard of any turbocharger at the inlet of the fuel-rich compressor.
I’ve never heard of that. The design pressure at the inlet of a gas-rich compressor is determined based on the system pressure; how can it be increased arbitrarily? Besides, doesn’t a turbocharger consume energy? Could an expert please explain what it looks like and its benefits?
I’ve heard of it for the first time too; does anyone know? Explain in detail.
I work in the compressor industry. Could you provide more details? 13911379725 I’m happy to help you
This is the first time I’ve heard that there’s some kind of turbocharger at the inlet of a rich gas compressor. Where did you hear that? Could you talk about it?
Compressor inlet pipe Application number/Patent number: 200810091182 This invention relates to a compressor inlet pipe. The present invention provides an inlet for a compressor, which has an inlet defining a roughly C-shaped shape and a housing configured to accommodate rotor cavities for a first and a second rotor. The inlet includes an inlet pipe with a defined inlet and an outlet in a roughly C-shaped configuration. The inlet duct has an inner wall that defines a cavity, which enables the transfer of air flow between the inlet and a roughly C-shaped outlet. The roughly C-shaped outlet of the inlet pipe has a shape that is essentially similar to the roughly C-shaped inlet of the shell. The inner wall includes the bottom and the top. The shape and contour of at least a portion of this bottom are designed such that, during the rotation of the first and second rotors, they exert on the airflow velocity components that complement the tangential velocity of each of the first and second rotors. This post was last edited by chengkang on 2009-3-7 08:57]
1. This rich gas compressor is a centrifugal compressor； 2. The diffuser (turbocharger) is part of the compressor stator and is used in conjunction with the compressor stator flow channels ； 3. The diffuser (supercharger) within a centrifugal compressor serves primarily to increase pressure and stabilize flow, thereby improving the efficiency of the compressor ； 4. The diffuser (supercharger) can prevent the compressor from operating in a blocked condition characterized by a low pressure ratio and high flow rate.