Multi-shaft turbine compression expander
A technology of compression expander and turbo expander, which is applied in the direction of mechanical equipment, machine/engine, non-variable pump, etc., and can solve the problem of deviation from the optimal operating speed at the expansion end, complex equipment layout and piping system, and organization mode Unable to meet the requirements and other problems, to achieve the effect of compact and beautiful unit, reduced space layout, and improved efficiency
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Embodiment 1
[0026] Embodiment 1. In this embodiment, if Figure 1 to Figure 2 As shown, a multi-shaft turbocompression expander includes a one-stage centrifugal compressor 1, a two-stage centrifugal compressor 2, a three-stage centrifugal compressor 3 and a centripetal turboexpander 4, and the one-stage centrifugal compressor 1 The two-stage centrifugal compressor 2 is axially connected through a gearbox 5, and the three-stage centrifugal compressor 3 is also axially connected with the centripetal turbo expander 4 through a gearbox 5; the one-stage centrifugal compressor 1, two The first-stage centrifugal compressor 2 and the third-stage centrifugal compressor 3 are connected through pipeline components.
[0027] The present invention is further configured as follows: the first-stage centrifugal compressor 1 and the second-stage centrifugal compressor 2 are respectively axially connected to the two ends of the first high-speed shaft 6 in the gearbox 5; the third-stage centrifugal compress...
Embodiment 2
[0039] Embodiment 2. This embodiment provides a multi-shaft turbocompressor-expander, including a first-stage centrifugal compressor 1, a second-stage centrifugal compressor 2, a third-stage centrifugal compressor 3, and a centripetal turboexpander 4. The one-stage centrifugal compressor 1 and the two-stage centrifugal compressor 2 are axially connected through a gear box 5, and the three-stage centrifugal compressor 3 and the centripetal turboexpander 4 are also axially connected through a gear box 5; the gear The box 5 is driven by energy recovery components; the first-stage centrifugal compressor 1 , the second-stage centrifugal compressor 2 , the third-stage centrifugal compressor 3 and the centripetal turboexpander 4 are connected through pipeline components.
[0040] The present invention is further configured as follows: the first-stage centrifugal compressor 1 and the second-stage centrifugal compressor 2 are respectively axially connected to the two ends of the first h...
Embodiment 3
[0054] Embodiment three, the difference with embodiment one, embodiment two is: as image 3 Shown: no drive assembly or energy recovery assembly is provided, so that a multi-shaft turbocompressor-expander with balanced input and output power is provided; in Embodiment 2 and Embodiment 3, the centripetal turboexpander 4 and the three-stage centrifugal compressor Machine 3 is not communicated through pipelines.
[0055] In all embodiments, the working medium gas passing through the one-stage centrifugal compressor 1, the two-stage centrifugal compressor 2, the three-stage centrifugal compressor 3, the centripetal turbo expander 4 and the gear box 5 can be the same fluid , The same medium or different mediums, the working medium gas is one or more mixed gases of air, nitrogen, hydrocarbon gas, carbon dioxide, water vapor, and Freon.
[0056] The above three embodiments are an integrated unit integrating an H-type multistage centrifugal compressor and a single-stage or multi-stag...
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