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Gas vane type gas-liquid rotary turbine separation device

A separation device and blade-type technology, which is applied in the field of gas blade-type gas-liquid rotary turbine separation device, can solve the problems of inability to ensure efficient utilization of fluid pressure energy, useful energy consumption of multiphase fluids, and reduction of secondary mixing, etc., to achieve Small footprint, minimizes gas entrainment and liquid carryover, reduces remixing effects

Inactive Publication Date: 2011-12-14
CHINA UNIV OF PETROLEUM (EAST CHINA)
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the petroleum industry, the traditional gas-liquid two-phase separation technology has been well developed, but there are three main problems: one is that the traditional separation equipment is bulky and heavy; the other is that the useful energy in the multiphase fluid is partially or completely consumed; the third is that when foam and emulsification are produced, the separation is not complete
[0004] The pressure energy conversion device in the hybrid two-phase turbine in the Hays patent - the gas-liquid two-phase nozzle, is realized by an irregular flow channel with an adjustable throat cross-sectional area. Although it can achieve a certain degree of flow regulation, it cannot guarantee the fluid Efficient use of pressure energy; the separated liquid film is always in contact with the gas, which is not conducive to reducing the secondary mixing; the gas blades of the separator adopt axial blades, the overall length is large, and the floor area is large

Method used

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  • Gas vane type gas-liquid rotary turbine separation device
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  • Gas vane type gas-liquid rotary turbine separation device

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Embodiment

[0026] as attached figure 1 , 5 As shown, the present invention mainly includes a casing 1 as a gas-liquid discharge device, a gas-liquid two-phase nozzle 2, a separation rotor 3, a sealing and lubricating device 4, a separator shaft 5, and a separator support 6. The cavity in the housing 1 is an axially horizontal rotationally symmetrical structure, and the cavity of the housing 1 is provided with a separator shaft 5 fixed in the cavity through a sealing and lubricating device 4 from right to left. 5. One end protrudes from the shell 1, and the other end is fixed with the separation rotor 3 and is located in the middle of the cavity. On the left side of the separation rotor 3, a gas-liquid two-phase nozzle 2 is fixed on the left end of the shell 1. Invented the overall axial "building block" installation, which is beneficial to the maintenance of the separator and the replacement of parts.

[0027] as attached Figure 2-4 As shown, the separation rotor 3 of the present inv...

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Abstract

The invention discloses a gas-vane type gas-liquid rotating turbine separating device. The separating device comprises a hollow shell mounted on a bracket, and a rotating shaft fixed in the shell through a sealing and lubricating device, wherein one end of the rotating shaft extends out of the shell, and a separating rotor positioned in the middle of an inner cavity of the shell is fixed at the other end of the rotating shaft; one end of the shell adjacent to the separating rotor is provided with a gas-liquid two-phase nozzle; the separating rotor comprises a separating disc fixed on the rotating shaft, wherein an annular liquid collecting tank and an annular gas collecting cavity are axially arranged on the separating disc in order; the liquid collecting tank is connected with a separating cone and communicated with a liquid retroaction nozzle; a circle of gas vanes communicated with the gas collecting cavity surround the periphery at the bottom of the gas collecting cavity, and an annular separating board is arranged between the liquid collecting tank and the gas collecting cavity; and a liquid volute and a gas volute which are separated by a separating board are axially arranged at the middle part of the inner cavity of the shell in parallel. The gas-vane type gas-liquid rotating turbine separating device is reasonable in structure, novel in design, high in separation efficiency, and convenient in demounting and maintenance due to axial cordwood system arrangement; and since the axial geometric size is reduced, the floor space of the separating device is reduced.

Description

technical field [0001] The invention relates to a gas-liquid separation device, in particular to a gas-blade type gas-liquid rotary turbine separation device, which belongs to the technical field of oil-gas separation and natural gas dehydration in oil-gas gathering and transportation systems. Background technique [0002] In the petroleum industry, the traditional gas-liquid two-phase separation technology has been well developed, but there are three main problems: one is that the traditional separation equipment is bulky and heavy; the other is that the useful energy in the multiphase fluid is partially or completely consumed; the third is that when foam and emulsification are produced, the separation is not complete. With the continuous development of my country's oil and gas industry, especially the development of offshore oil and gas fields for the development of oil and gas industry requirements, oil and gas separators have developed from the traditional gravity type t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B01D45/14B01D19/00
Inventor 何利民王天祥吕宇玲罗小明王鑫刘超
Owner CHINA UNIV OF PETROLEUM (EAST CHINA)
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