Triple inlet passage adjustable outlet area volute design

By designing a three-intake-channel adjustable outlet intake volute, the problem of the inflexible intake degree of the volute was solved, achieving efficient intake management and turbine efficiency improvement under different conditions, and reducing replacement costs.

CN120739592BActive Publication Date: 2025-11-04AEROSPACE POWER RES INST (SUZHOU) CO LTD
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Patent Information

Application Number
CN202511174023.9
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-08-21
Publication Date
2025-11-04
Estimated Expiration
2045-08-21

AI Technical Summary

Technical Problem

The design of the volute air intake in existing gas turbine power generation systems cannot be flexibly adjusted, resulting in low efficiency under different operating conditions. Furthermore, the volute needs to be replaced under different conditions to adapt to the difference in air intake, which increases cost and complexity.

Method used

A three-intake-channel adjustable outlet intake volute was designed, comprising a three-intake compressor equalization mechanism, an intake adjustment flame-retardant mechanism, an isolation support mechanism, an equalization and anti-interference flow guiding mechanism, and a heat dissipation and fire extinguishing mechanism. It can flexibly adjust the number of intake channels and intake volume under different conditions to ensure turbine efficiency.

Benefits of technology

This achieves stability and efficiency of the volute inlet state under conditions with significant differences in intake volume, reducing the cost and time of volute replacement and improving turbine blowing efficiency and safety.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application relates to gas turbine technology field, and discloses three inlet channel adjustable outlet inlet degree volute design, comprising: three inlet air pressure equalizing mechanism, one end of the three inlet air pressure equalizing mechanism is provided with inlet degree adjustment fire prevention mechanism.The three inlet channel adjustable outlet inlet degree volute design can change the originally fixed full circle inlet into the range adjustment of sixteenth inlet degree to full circle inlet, change the originally single channel inlet and double channel inlet design into three channel inlet, when coping with different state tests, the number of inlet channels can be freely selected, the test state of volute inlet can be ensured in small state and large state, and then the turbine rotation efficiency is ensured, in addition, the present application can cope with the test state of large difference between inlet size, without machining and replacing different inlet degree volutes in different test states like traditional volutes, so that the manpower, material resources and time cost in test are greatly reduced.
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Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of gas turbine, in particular to a three-inlet-channel adjustable-outlet-inlet-degree volute design. BACKGROUND

[0002] The gas turbine power generation system is a kind of efficient and flexible power generation technology, which drives the turbine to rotate by burning fuel, and then drives the generator to generate electricity, the gas turbine power generation system is that gas enters the turbine through the volute, and the turbine drives the generator to generate electricity, therefore the efficiency of the gas blowing the turbine affects the overall efficiency of the gas turbine power generation system, since the gas turbine system has multiple working states, and the inlet flow of different working states is significantly different, the ordinary inlet volute outlet adopts fixed inlet degree.

[0003] Under the condition of "local inlet", small flow, fixed large inlet degree will cause energy dispersion, under the condition of "full circle inlet", large flow, fixed small inlet degree will cause airflow congestion, and even trigger flow channel surge, and the inlet degree of the existing volute is a fixed value, for different working conditions, a special volute needs to be customized, the inlet degree cannot be changed according to the working conditions of "full circle inlet" and "local inlet", at the same time, the mainstream volute adopts single inlet channel or double inlet channel, which can only match fixed inlet range, and the inlet degree is usually the maximum state, corresponding to all turbine blades, when the turbine needs to switch from "full circle inlet" to "local inlet", corresponding to a small amount of turbine blades, the traditional structure needs to process and replace the volute with different inlet degrees, and cannot be adjusted flexibly. SUMMARY

[0004] In view of the deficiencies of the prior art, the present application provides a three-inlet-channel adjustable-outlet-inlet-degree volute design, which solves the problems mentioned in the above background.

[0005] The application provides the following technical scheme: a three-inlet channel adjustable outlet air inlet degree volute design, comprising: a three-inlet air pressure equalizing mechanism, one end of the three-inlet air pressure equalizing mechanism is provided with an air inlet degree adjusting flame-retardant mechanism, the inside of the three-inlet air pressure equalizing mechanism is provided with an isolation support mechanism, an air equalizing anti-disturbance flow guiding mechanism is arranged between the three-inlet air pressure equalizing mechanism and the isolation support mechanism, the surface of the three-inlet air pressure equalizing mechanism is provided with a heat dissipation fire extinguishing mechanism, the three-inlet air pressure equalizing mechanism comprises a flow guiding main shell, a rotating seat and a damping block, the rotating seat is integrally arranged on the surface of the bottom of the flow guiding main shell, the damping block is fixedly connected to the inside of the rotating seat, the air inlet degree adjusting flame-retardant mechanism comprises a flow guiding auxiliary shell, a rotating connecting head, a mounting frame, a second air inlet hole, a mounting groove, a wind deflector and a fixing frame, the flow guiding auxiliary shell is arranged at one end of the flow guiding main shell, the rotating connecting head is integrally arranged on the surface of the bottom of the flow guiding auxiliary shell, the mounting frame is fixedly connected to the inside of the end of the flow guiding main shell close to the flow guiding auxiliary shell, the fixing frame is fixedly connected to the inside of the end of the flow guiding auxiliary shell close to the flow guiding main shell, the number of the second air inlet holes is six, the six second air inlet holes are all through holes arranged on the two sides of the flow guiding auxiliary shell, the mounting groove is inlaidly arranged in the inside of the end of the second air inlet hole close to the fixing frame, the wind deflector is movably mounted in the inside of the mounting groove, and the number of the wind deflectors is adjusted between zero and six.

[0006] Preferably, the three-inlet air pressure equalizing mechanism further comprises a heat dissipation fin and an air pressure outer ring, the number of the heat dissipation fins is multiple, the multiple heat dissipation fins are integrally arranged on the surface of the flow guiding main shell, the air pressure outer ring is fixedly connected to the inner wall of the end of the flow guiding main shell away from the flow guiding auxiliary shell, and the surface of the air pressure outer ring is provided with a first flow guiding curved surface.

[0007] Preferably, the three-inlet air pressure equalizing mechanism further comprises a flow guiding end shell and an air inlet channel, the flow guiding end shell is arranged at the end of the flow guiding main shell away from the flow guiding auxiliary shell, the end of the flow guiding main shell close to the flow guiding end shell and the end of the flow guiding end shell close to the flow guiding main shell are both integrally provided with a second flange ring, the flow guiding main shell is fixedly connected with the flow guiding end shell through the second flange ring and bolts, the number of the air inlet channels is three, the three air inlet channels are all integrally arranged on the surface of the flow guiding main shell, and the included angle between adjacent two air inlet channels is 120 degrees.

[0008] Preferably, the air inlet degree adjusting flame-retardant mechanism further comprises a flame-retardant frame, six first air inlet holes and a flame-retardant net, the flame-retardant frame is fixedly connected to the inside of the flow guide auxiliary shell away from the end of the flow guide auxiliary shell, the six first air inlet holes are all through the two sides of the flame-retardant frame, and the six first air inlet holes correspond to the six second air inlet holes respectively, the flame-retardant net is fixedly connected to the inside of the first air inlet hole, the flow guide auxiliary shell is rotatably connected to the flow guide main shell through a rotating connector and a rotating seat, the surface of the damping block is slidably connected to the surface of the rotating connector, and the end of the flow guide main shell and the end of the flow guide auxiliary shell are both integrally provided with a first flange ring, and the flow guide main shell is fixedly connected to the flow guide auxiliary shell through the first flange ring and bolts.

[0009] Preferably, the air inlet degree adjusting flame-retardant mechanism further comprises a sealing ring, six third air inlet holes, a positioning strip and a positioning groove, the sealing ring is fixedly connected to the inner wall of the mounting groove, and the sealing ring is located between the mounting groove and the wind shield piece, the six third air inlet holes are all through the two sides of the fixing frame, and the six third air inlet holes correspond to the six second air inlet holes respectively, the positioning strip is integrally arranged on the side of the fixing frame close to the mounting frame, and the positioning groove is arranged on the side of the mounting frame close to the fixing frame, and the shape and size of the positioning strip and the shape and size of the positioning groove are matched with each other.

[0010] Preferably, the isolation supporting mechanism comprises a supporting cylinder, an air inlet curved surface, an end supporting ring, a gas pressing inner ring and a supporting inner ring, the supporting cylinder is fixedly connected to the inside of the flow guide end shell, and the surface of one end of the supporting cylinder is fixedly connected to the inner wall of the mounting frame, the air inlet curved surface is integrally arranged on the surface of one end of the supporting cylinder close to the flow guide end shell, the end supporting ring is fixedly connected to the inside of the flame-retardant frame and the fixing frame, and the end supporting ring is located at the end of the supporting cylinder away from the air inlet curved surface, the gas pressing inner ring is fixedly sleeved on the surface of the supporting cylinder, and the surface of the gas pressing inner ring is provided with a second flow guide curved surface and a third flow guide curved surface respectively, the second flow guide curved surface is located on the side of the gas pressing outer ring close to the flow guide auxiliary shell, the third flow guide curved surface is located on the side of the gas pressing outer ring away from the flow guide auxiliary shell, and the supporting inner ring is integrally arranged on the end of the supporting cylinder close to the end supporting ring and the end of the end supporting ring close to the supporting cylinder.

[0011] Preferably, the air inlet degree adjusting flame-retardant mechanism further comprises a sealing ring, six third air inlet holes, a positioning strip and a positioning groove, the sealing ring is fixedly connected to the inner wall of the mounting groove, and the sealing ring is located between the mounting groove and the wind shield piece, the six third air inlet holes are all through the two sides of the fixing frame, and the six third air inlet holes correspond to the six second air inlet holes respectively, the positioning strip is integrally arranged on the side of the fixing frame close to the mounting frame, and the positioning groove is arranged on the side of the mounting frame close to the fixing frame, and the shape and size of the positioning strip and the shape and size of the positioning groove are matched with each other.

[0012] Preferably, the heat dissipation fire extinguishing mechanism comprises a first conversion seat, a first flow guide hole, a liquid pump, a first one-way valve and a water inlet elbow, the first conversion seat is fixedly connected to the surface of the flow guide main shell and is located below the flow guide main shell, the first flow guide hole is provided through the inside of the first conversion seat, the liquid pump is fixedly installed on the outside of the first conversion seat, and the output end of the first conversion seat is in communication with the first flow guide hole, the first one-way valve is fixedly connected to the output end of the first conversion seat and unidirectionally guides to the first flow guide hole, the number of the water inlet elbows is two, and the two water inlet elbows are fixedly connected to the two ends of the first flow guide hole, and one of the water inlet elbows penetrates through the outer surface of the flow guide main shell and extends into the inside of the air compression outer ring, and the other water inlet elbow penetrates through the outer surface of the flow guide main shell and extends into the inside of the air compression flow guide ring.

[0013] Preferably, the heat dissipation fire extinguishing mechanism further comprises a second conversion seat, a second flow guide hole, a first electromagnetic switch valve and a drain elbow, the second conversion seat is fixedly connected to the surface of the flow guide main shell and is oppositely distributed with the first conversion seat, the second flow guide hole is provided through the inside of the second conversion seat, the first electromagnetic switch valve is fixedly installed on the outer surface of the second conversion seat, and one end of the first electromagnetic switch valve is in communication with the second flow guide hole, the number of the drain elbows is two, and the two drain elbows are fixedly connected to the two ends of the second flow guide hole, and one of the drain elbows penetrates through the outer surface of the flow guide main shell and extends into the inside of the air compression outer ring, and the other drain elbow penetrates through the outer surface of the flow guide main shell and extends into the inside of the air compression flow guide ring.

[0014] Preferably, the heat dissipation fire extinguishing mechanism further comprises a third conversion seat, a lower through hole, a second electromagnetic switch valve, a connecting pipe and a second one-way valve, the number of the third conversion seats is two, and the two third conversion seats are fixedly connected to the surface of the flow guide main shell and are oppositely distributed, the lower through hole is provided through the outside of the third conversion seat and extends to the inner surface of the flow guide main shell, the second electromagnetic switch valve is fixedly installed on the outside of the third conversion seat, and the output end of the second electromagnetic switch valve is in communication with the lower through hole, the connecting pipe is fixedly connected to the inside of the lower through hole, the second one-way valve is fixedly connected to the inside of the lower through hole and unidirectionally guides to the flow guide main shell, and the second flow guide curved surface is located between the connecting lines of the two connecting pipes.

[0015] Compared with the prior art, the heat dissipation fire extinguishing mechanism has the following beneficial effects:

[0016] The three-inlet passage adjustable outlet air inlet degree volute design can change the original fixed full-circle air inlet into the range adjustment from the air inlet degree of one sixth to the full-circle air inlet, change the original single-channel air inlet and double-channel air inlet design into the three-channel air inlet, freely select the number of air inlet passages when coping with different test states, ensure the test state of the volute inlet in the small state and the large state, and further ensure the turbine rotation efficiency.

[0017] The three-inlet passage adjustable outlet air inlet degree volute design can change the original fixed full-circle air inlet into the range adjustment from the air inlet degree of one sixth to the full-circle air inlet, change the original single-channel air inlet and double-channel air inlet design into the three-channel air inlet, freely select the number of air inlet passages when coping with different test states, ensure the test state of the volute inlet in the small state and the large state, and further ensure the turbine rotation efficiency.

[0018] The three-inlet passage adjustable outlet air inlet degree volute design can change the original fixed full-circle air inlet into the range adjustment from the air inlet degree of one sixth to the full-circle air inlet, change the original single-channel air inlet and double-channel air inlet design into the three-channel air inlet, freely select the number of air inlet passages when coping with different test states, ensure the test state of the volute inlet in the small state and the large state, and further ensure the turbine rotation efficiency.

[0019] The three-inlet passage adjustable outlet air inlet degree volute design can change the original fixed full-circle air inlet into the range adjustment from the air inlet degree of one sixth to the full-circle air inlet, change the original single-channel air inlet and double-channel air inlet design into the three-channel air inlet, freely select the number of air inlet passages when coping with different test states, ensure the test state of the volute inlet in the small state and the large state, and further ensure the turbine rotation efficiency.

[0020] The three-inlet passage adjustable outlet air inlet degree volute design can change the original fixed full-circle air inlet into the range adjustment from the air inlet degree of one sixth to the full-circle air inlet, change the original single-channel air inlet and double-channel air inlet design into the three-channel air inlet, freely select the number of air inlet passages when coping with different test states, ensure the test state of the volute inlet in the small state and the large state, and further ensure the turbine rotation efficiency.

[0021] The three-inlet passage adjustable outlet air inlet degree volute design can change the original fixed full-circle air inlet into the range adjustment from the air inlet degree of one sixth to the full-circle air inlet, change the original single-channel air inlet and double-channel air inlet design into the three-channel air inlet, freely select the number of air inlet passages when coping with different test states, ensure the test state of the volute inlet in the small state and the large state, and further ensure the turbine rotation efficiency. BRIEF DESCRIPTION OF DRAWINGS

[0022] Figure 1 Structure diagram of the present application;

[0023] Figure 2 Structure diagram of the present application;

[0024] Figure 3 Structure diagram of the present application;

[0025] Figure 4 Structure diagram of the present application;

[0026] Figure 5 Structure diagram of the present application;

[0027] Figure 6 Structure diagram of the present application;

[0028] Figure 7 Structure diagram of the present application;

[0029] Figure 8 Structure diagram of the present application;

[0030] Figure 9 Structure diagram of the present application;

[0031] Figure 10 Structure diagram of the present application;

[0032] Figure 11 Structure diagram of the present application;

[0033] In the figure: 101, main guide shell; 102, rotating seat; 103, damping block; 104, heat sink; 105, air compression outer ring; 106, guide end shell; 107, air inlet; 201, secondary guide shell; 202, rotating connecting head; 203, fireproof frame; 204, first air inlet; 205, fireproof net; 206, mounting frame; 207, second air inlet; 208, mounting groove; 209, wind baffle; 210, fixed frame; 211, sealing ring; 212, third air inlet; 213, positioning strip; 214, positioning groove; 301, support cylinder; 302, air inlet curved surface; 303, end support ring; 304, air compression inner ring; 305, support inner ring; 401, air compression guide ring; 402, guide partition; 501, first conversion seat; 502, first guide hole; 503, liquid pump; 504, first one-way valve; 505, water inlet elbow; 506, second conversion seat; 507, second guide hole; 508, first electromagnetic switch valve; 509, water outlet elbow; 510, third conversion seat; 511, lower through hole; 512, second electromagnetic switch valve; 513, connecting pipe; 514, second one-way valve. DETAILED DESCRIPTION

[0034] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0035] Please see Figures 1-11 The three-intake channel adjustable outlet intake volute design includes: a three-intake air pressure equalization mechanism; an intake adjustment flame-retardant mechanism at one end of the three-intake air pressure equalization mechanism; an isolation support mechanism inside the three-intake air pressure equalization mechanism; an air equalization and anti-interference guide mechanism between the three-intake air pressure equalization mechanism and the isolation support mechanism; and a heat dissipation and fire extinguishing mechanism on the surface of the three-intake air pressure equalization mechanism. The three-intake air pressure equalization mechanism includes a guide main shell 101, a rotating seat 102, and a damping block 103. The rotating seat 102 is integrally mounted on the bottom surface of the guide main shell 101. The damping block 103 is fixedly connected inside the rotating seat 102. The air intake adjustment flame-retardant mechanism includes a flow guide sub-shell 201, a rotating connector 202, a mounting bracket 206, a second air intake 207, a mounting groove 208, a wind deflector 209, and a fixing bracket 210. The flow guide sub-shell 201 is located at one end of the flow guide main shell 101. The rotating connector 202 is integrally located on the bottom surface of the flow guide sub-shell 201. The mounting bracket 206 is fixedly connected inside the flow guide main shell 101 near the end of the flow guide sub-shell 201. The fixing bracket 210 is fixedly connected to the end of the flow guide sub-shell 201 near the end of the flow guide sub-shell 201. Inside one end of the main guide shell 101, there are six second air inlets 207, all of which are penetrating and opening on both sides of the secondary guide shell 201. A mounting groove 208 is embedded inside the second air inlets 207 near the fixing bracket 210. Wind deflectors 209 are movably installed inside the mounting groove 208, and the number of wind deflectors 209 can be adjusted between zero and six. Through the configured three-inlet pressure equalization mechanism, air intake adjustment flame-retardant mechanism, isolation support mechanism, air equalization and anti-interference guide mechanism, and heat dissipation and fire extinguishing mechanism, the originally fixed... The full-circumference intake has been changed to a range of adjustment from one-sixth intake to full-circumference intake. The original single-channel and dual-channel intake design has been changed to a three-channel intake. When dealing with different test conditions, the number of intake channels can be freely selected to ensure the test conditions of the volute inlet under both small and large conditions, thereby ensuring the turbine blowing efficiency. In addition, this invention can handle test conditions with large differences in intake size, without the need to process and replace volutes with different intake sizes under different test conditions as with traditional volutes, which greatly reduces the manpower, material resources and time costs in the test.

[0036] Wherein; three intake air pressure equalizing mechanism also includes the fin 104 and the air ring 105, the number of the fin 104 is multiple, and multiple fins 104 are integrally arranged on the surface of the flow guide main shell 101, the air ring 105 is fixedly connected to the inner wall of the flow guide main shell 101 away from the flow guide auxiliary shell 201, and the surface of the air ring 105 is provided with a first flow guide curved surface.

[0037] Wherein; three intake air pressure equalizing mechanism also includes the flow guide end shell 106 and the air inlet 107, the flow guide end shell 106 is arranged at the end of the flow guide main shell 101 away from the flow guide auxiliary shell 201, and the end of the flow guide main shell 101 close to the flow guide end shell 106 and the end of the flow guide end shell 106 close to the flow guide main shell 101 are integrally provided with a second flange ring, and the flow guide main shell 101 is fixedly connected with the flow guide end shell 106 through the second flange ring and the bolt, the number of the air inlet 107 is three, and the three air inlets 107 are integrally arranged on the surface of the flow guide main shell 101, and the included angle between adjacent two air inlets 107 is 120 degrees, by setting the flow guide main shell 101, the rotating seat 102, the damping block 103, the fin 104, the air ring 105, the flow guide end shell 106 and the air inlet 107, the number of the air inlet 107 can be adjusted according to the air intake demand, so as to ensure the test state of the volute inlet under the condition that the large state and the small state are greatly different.

[0038] Wherein; the air intake degree adjusting and flame-retardant mechanism further comprises a flame-retardant frame 203, a first air inlet hole 204 and a flame-retardant net 205, the flame-retardant frame 203 is fixedly connected to the inside of the flow guide auxiliary shell 201 away from the flow guide auxiliary shell 201, the number of the first air inlet hole 204 is six, and the six first air inlet holes 204 are all through the two sides of the flame-retardant frame 203, and the six flame-retardant frames 203 correspond to the six second air inlet holes 207 respectively, the flame-retardant net 205 is fixedly connected to the inside of the first air inlet hole 204, the flow guide auxiliary shell 201 is rotatably connected with the flow guide main shell 101 through the rotating connecting head 202 and the rotating seat 102, the surface of the damping block 103 is slidably connected with the surface of the rotating connecting head 202, one end of the flow guide main shell 101 and one end of the flow guide auxiliary shell 201 are integrally provided with a first flange ring, and the flow guide main shell 101 is fixedly connected with the flow guide auxiliary shell 201 through the first flange ring and the bolt.

[0039] Wherein; the air intake degree adjusting flame-retardant mechanism further comprises a sealing ring 211, third air inlet holes 212, a positioning strip 213 and a positioning groove 214, the sealing ring 211 is fixedly connected to the inner wall of the mounting groove 208, and the sealing ring 211 is located between the mounting groove 208 and the wind baffle 209, the number of the third air inlet holes 212 is six, and the six third air inlet holes 212 are all through the two sides of the fixed frame 210, and the six third air inlet holes 212 correspond to the six second air inlet holes 207 respectively, the positioning strip 213 is integrally arranged on the side of the fixed frame 210 close to the mounting frame 206, the positioning groove 214 is arranged on the side of the mounting frame 206 close to the fixed frame 210, and the shape and size of the positioning strip 213 and the positioning groove 214 are matched with each other, through the setting of the flow guide auxiliary shell 201, the rotating connecting head 202, the flame-retardant frame 203, the first air inlet hole 204, the flame-retardant net 205, the mounting frame 206, the second air inlet hole 207, the mounting groove 208, the wind baffle 209, the fixed frame 210, the sealing ring 211, the third air inlet hole 212, the positioning strip 213 and the positioning groove 214, the air intake degree adjusting function can be realized by changing the number and position of the wind baffles 209, without machining and replacing different air intake degree volutes under different test conditions like traditional volutes.

[0040] Wherein; the isolation support mechanism comprises a support cylinder 301, an air inlet curved surface 302, an end support ring 303, a gas pressing inner ring 304 and a support inner ring 305, the support cylinder 301 is fixedly connected to the inside of the flow guide end shell 106, and the surface of one end of the support cylinder 301 is fixedly connected to the inner wall of the mounting frame 206, the air inlet curved surface 302 is integrally arranged on the surface of one end of the support cylinder 301 close to the flow guide end shell 106, the end support ring 303 is fixedly connected to the inside of the flame-retardant frame 203 and the fixed frame 210, and the end support ring 303 is located at one end of the support cylinder 301 away from the air inlet curved surface 302, the gas pressing inner ring 304 is fixedly sleeved on the surface of the support cylinder 301, and the surface of the gas pressing inner ring 304 is provided with a second flow guide curved surface and a third flow guide curved surface, the second flow guide curved surface is located on the side of the gas pressing outer ring 105 close to the flow guide auxiliary shell 201, and the third flow guide curved surface is located on the side of the gas pressing outer ring 105 away from the flow guide auxiliary shell 201, and the support inner ring 305 is integrally arranged on one end of the support cylinder 301 close to the end support ring 303 and one end of the end support ring 303 close to the support cylinder 301, through the setting of the support cylinder 301, the air inlet curved surface 302, the end support ring 303, the gas pressing inner ring 304 and the support inner ring 305, the air inlet channel can be guided and isolated, and the mechanical structure of the channel is ensured.

[0041] Wherein; The air disturbance prevention and flow guiding mechanism comprises a gas pressure flow guiding ring 401 and a flow guiding baffle 402, the gas pressure flow guiding ring 401 is fixedly connected to the inner wall of the flow guiding main shell 101, and the surface of the gas pressure flow guiding ring 401 is provided with a fourth flow guiding curved surface, the flow guiding baffle 402 is integrally arranged on the side of the gas pressure flow guiding ring 401 away from the gas pressure outer ring 105, the number of the flow guiding baffles 402 is multiple, the multiple flow guiding baffles 402 are distributed in parallel, the multiple flow guiding baffles 402 are uniformly distributed on one side of the gas pressure flow guiding ring 401, and the surfaces of the multiple flow guiding baffles 402 are fixedly connected to the outer surface of the supporting cylinder 301. Through the gas pressure flow guiding ring 401 and the flow guiding baffle 402, the parallel flow guiding baffles 402 can smoothly guide the uniform airflow to the side of the second air inlet hole 207, and the flow guiding baffle 402 can also increase the area and improve the heat exchange effect during heat dissipation.

[0042] Wherein; The heat dissipation and fire extinguishing mechanism comprises a first conversion seat 501, a first flow guiding hole 502, a liquid pump 503, a first one-way valve 504 and a water inlet elbow 505, the first conversion seat 501 is fixedly connected to the surface of the flow guiding main shell 101 and is located below the flow guiding main shell 101, the first flow guiding hole 502 is formed in the inside of the first conversion seat 501, the liquid pump 503 is fixedly installed on the outside of the first conversion seat 501, the output end of the first conversion seat 501 is in communication with the first flow guiding hole 502, the first one-way valve 504 is fixedly connected to the output end of the first conversion seat 501 and is unidirectionally communicated with the first flow guiding hole 502, the number of the water inlet elbows 505 is two, and the two water inlet elbows 505 are fixedly connected to the two ends of the first flow guiding hole 502, and one of the water inlet elbows 505 penetrates through the outer surface of the flow guiding main shell 101 and extends into the inside of the gas pressure outer ring 105, and the other water inlet elbow 505 penetrates through the outer surface of the flow guiding main shell 101 and extends into the inside of the gas pressure flow guiding ring 401.

[0043] Wherein; The heat dissipation and fire extinguishing mechanism further comprises a second conversion seat 506, a second flow guiding hole 507, a first electromagnetic switch valve 508 and a drain elbow 509, the second conversion seat 506 is fixedly connected to the surface of the flow guiding main shell 101 and is oppositely distributed with the first conversion seat 501, the second flow guiding hole 507 is formed in the inside of the second conversion seat 506, the first electromagnetic switch valve 508 is fixedly installed on the outer surface of the second conversion seat 506, one end of the first electromagnetic switch valve 508 is in communication with the second flow guiding hole 507, the number of the drain elbows 509 is two, and the two drain elbows 509 are fixedly connected to the two ends of the second flow guiding hole 507, one of the drain elbows 509 penetrates through the outer surface of the flow guiding main shell 101 and extends into the inside of the gas pressure outer ring 105, and the other drain elbow 509 penetrates through the outer surface of the flow guiding main shell 101 and extends into the inside of the gas pressure flow guiding ring 401.

[0044] The heat dissipation and fire extinguishing mechanism further comprises two third conversion seats 510, a lower through hole 511, a second electromagnetic switch valve 512, a connecting pipe 513 and a second one-way valve 514. The two third conversion seats 510 are fixedly connected to the surface of the main flow guide shell 101 and are oppositely distributed. The lower through hole 511 is formed through the outer side of the third conversion seat 510 and extends to the inner surface of the main flow guide shell 101. The second electromagnetic switch valve 512 is fixedly installed on the outer side of the third conversion seat 510, and the output end of the second electromagnetic switch valve 512 is in communication with the lower through hole 511. The connecting pipe 513 is fixedly connected to the inside of the lower through hole 511. The second one-way valve 514 is fixedly connected to the inside of the lower through hole 511 and unidirectionally guides to the main flow guide shell 101. The second flow guide curved surface is located between the connecting line of the two connecting pipes 513. The first conversion seat 501, the first flow guide hole 502, the liquid pump 503, the first one-way valve 504, the water inlet elbow 505, the second conversion seat 506, the second flow guide hole 507, the first electromagnetic switch valve 508, the water outlet elbow 509, the third conversion seat 510, the lower through hole 511, the second electromagnetic switch valve 512, the connecting pipe 513 and the second one-way valve 514 can continuously dissipate heat by pumping cold water through the liquid pump 503 during use, avoid the transmission of heat of the gas turbine to the device to cause overheating deformation, and assist in fire extinguishing when the fire is out or the temperature is too high, thereby improving the safety.

[0045] Working principle:

[0046] During use, the bolts on the first flange ring are opened, and then the flow guide auxiliary shell 201 is unfolded. According to the requirements, the corresponding number of wind baffles 209 is arranged in the installation groove 208, and then the flow guide auxiliary shell 201 is closed, so that the positioning strip 213 is embedded in the positioning groove 214, and the third air inlet hole 212 is used to extrude and fix the wind baffle 209. Then the bolts on the first flange ring are installed, so as to realize the switching from "full circumference air inlet" to "local air inlet".

[0047] At the same time, according to the demand, the corresponding number of air inlets 107 is opened for ventilation, and the airflow first enters the inside of the flow guide end shell 106 from the air inlet 107, and then is introduced along the support cylinder 301 and the air inlet curved surface 302 to the surface of the pressure gas outer ring 105. At this time, the space between the pressure gas outer ring 105 and the support cylinder 301 is reduced, and the unevenly distributed airflow in the air inlet 107 will be compressed to a certain extent, so that the airflow cannot pass through at the same time. This forces the airflow to pass through other positions between the pressure gas outer ring 105 and the support cylinder 301, so that the airflow is more evenly distributed around the surface of the support cylinder 301. Then the airflow passes between the pressure gas inner ring 304 and the flow guide main shell 101 in the same way, and also makes the airflow more evenly distributed around the surface of the support cylinder 301. Then the uniform airflow is uniformly distributed between the flow guide baffles 402 along the pressure gas flow guide ring 401 and is transported inward. Due to the blocking of the flow guide baffles 402, the airflow between the flow guide baffles 402 does not interfere with each other, so that the airflow evenly distributed around the surface of the support cylinder 301 can reach the other end uniformly. Then the airflow passes from the inside of the corresponding second air inlet hole 207 which is not covered by the wind deflector 209, and then the airflow passes through the fire-retardant net 205 and is discharged into the turbine. Thus, it can be ensured that the airflow passing through the second air inlet hole 207 is uniform when the number of air inlets 107 is one, two or three.

[0048] First, one end of the first electromagnetic switch valve 508 is connected with the external drain pipe, the input end of the liquid pump 503 is connected with the cold water pipe, and the input end of the second electromagnetic switch valve 512 is connected with the fire extinguishing agent pipeline. When dissipating heat, the first electromagnetic switch valve 508 is opened, and the liquid pump 503 is started. The liquid pump 503 pumps cold water into the first conversion seat 501, and then the cold water enters the pressure gas outer ring 105 and the pressure gas flow guide ring 401 along the water inlet elbow 505. At this time, the flow guide baffles 402 guide heat into the pressure gas flow guide ring 401, and the flow guide main shell 101 and the support cylinder 301 guide heat into the pressure gas outer ring 105 and the pressure gas flow guide ring 401. The cold water passing through the two absorbs heat and becomes hot water, so that the water flow reaches from the lower part to the upper part of the pressure gas outer ring 105 and the pressure gas flow guide ring 401, then enters the second conversion seat 506, and finally is discharged from the first electromagnetic switch valve 508, thereby realizing continuous heat dissipation inside the device. When extinguishing fire, the second electromagnetic switch valve 512 is opened after receiving a signal from an external sensor or an external controller. At this time, the fire extinguishing agent enters the connecting pipe 513 from the second electromagnetic switch valve 512, and then enters the inside of the flow guide main shell 101. Then the second flow guide curved surface along the surface of the pressure gas inner ring 304 enters between the flow guide main shell 101 and the support cylinder 301 to cool and extinguish the inside.

[0049] While embodiments of the application have been shown and described, it is to be understood that the embodiments described are merely exemplary of the principles and application of the present application. Numerous modifications and adaptions can be effected without departing from the spirit and scope of the present application, which is not limited to the exact construction and arrangement described. It is intended, therefore, to cover all modifications and adaptions that fall within the scope of the claims and their equivalents.

Claims

1. A three-intake-channel adjustable outlet intake volute design, characterized in that, include: The three-intake air pressure equalization mechanism has an air intake adjustment flame-retardant mechanism at one end, an isolation support mechanism inside the three-intake air pressure equalization mechanism, an air equalization anti-interference and flow guiding mechanism between the three-intake air pressure equalization mechanism and the isolation support mechanism, and a heat dissipation and fire extinguishing mechanism on the surface of the three-intake air pressure equalization mechanism. The three-intake air pressure equalization mechanism includes a main guide shell (101), a rotating seat (102), and a damping block (103). The rotating seat (102) is integrally disposed on the bottom surface of the main guide shell (101), and the damping block (103) is fixedly connected to the inside of the rotating seat (102). The air intake adjustment flame retardant mechanism includes a secondary guide shell (201), a rotating connector (202), a mounting bracket (206), a second air intake hole (207), a mounting groove (208), a wind deflector (209), and a fixing bracket (210). The secondary guide shell (201) is disposed at one end of the main guide shell (101), and the rotating connector (202) is integrally disposed on the secondary guide shell (201). 1) On the bottom surface, the mounting bracket (206) is fixedly connected to the interior of the main guide shell (101) near the end of the secondary guide shell (201), and the fixing bracket (210) is fixedly connected to the interior of the secondary guide shell (201) near the end of the main guide shell (101). There are six second air inlets (207), and all six second air inlets (207) are opened through both sides of the secondary guide shell (201). The mounting groove (208) is embedded in the interior of the second air inlet (207) near the end of the fixing bracket (210). The wind deflector (209) is movably installed inside the mounting groove (208). The number of wind deflectors (209) is adjusted between zero and six. The three-intake air pressure equalization mechanism also includes a guide end shell (106) and an air intake (107). The guide end shell (106) is located at the end of the main guide shell (101) away from the secondary guide shell (201). The end of the main guide shell (101) near the guide end shell (106) and the end of the guide end shell (106) near the main guide shell (101) are both integrally provided with a second flange ring. The main guide shell (101) is fixedly connected to the guide end shell (106) by the second flange ring and bolts. There are three air intakes (107). All three air intakes (107) are integrally provided on the surface of the main guide shell (101). The included angle between two adjacent air intakes (107) is 120 degrees.

2. The three-intake-channel adjustable outlet intake volute design according to claim 1, characterized in that, The three-intake air pressure equalization mechanism also includes heat sinks (104) and an outer air pressure ring (105). There are multiple heat sinks (104), which are integrally disposed on the surface of the main air-guiding shell (101). The outer air pressure ring (105) is fixedly connected to the inner wall of the main air-guiding shell (101) away from the secondary air-guiding shell (201). The surface of the outer air pressure ring (105) is provided with a first air-guiding curved surface.

3. The three-intake-channel adjustable outlet intake volute design according to claim 1, characterized in that, The air intake adjustment flame-retardant mechanism further includes a flame-retardant frame (203), a first air intake (204), and a flame-retardant mesh (205). The flame-retardant frame (203) is fixedly connected to the interior of the flow guide sub-shell (201) at the end away from the flow guide sub-shell (201). There are six first air intakes (204), all of which are opened through both sides of the flame-retardant frame (203). The six flame-retardant frames (203) correspond to the six second air intakes (207), respectively. The flame-retardant mesh (205) The flow guide sub-shell (201) is fixedly connected inside the first air inlet (204). The flow guide sub-shell (201) is rotatably connected to the flow guide main shell (101) through the rotating connector (202) and the rotating seat (102). The surface of the damping block (103) is slidably connected to the surface of the rotating connector (202). One end of the flow guide main shell (101) and one end of the flow guide sub-shell (201) are integrally provided with a first flange ring. The flow guide main shell (101) is fixedly connected to the flow guide sub-shell (201) through the first flange ring and bolts.

4. The three-intake-channel adjustable outlet intake volute design according to claim 3, characterized in that, The air intake adjustment flame retardant mechanism also includes a sealing ring (211), a third air intake hole (212), a positioning strip (213), and a positioning groove (214). The sealing ring (211) is fixedly connected to the inner wall of the mounting groove (208). The sealing ring (211) is located between the mounting groove (208) and the wind deflector (209). There are six third air intake holes (212). All six third air intake holes (212) are opened through both sides of the fixed frame (210). The six third air intake holes (212) correspond to the six second air intake holes (207) respectively. The positioning strip (213) is integrally set on the side of the fixed frame (210) near the mounting frame (206). The positioning groove (214) is opened on the side of the mounting frame (206) near the fixed frame (210). The shape and size of the positioning strip (213) match the shape and size of the positioning groove (214).

5. The three-intake-channel adjustable outlet intake volute design according to claim 1, characterized in that, The isolation support mechanism includes a support cylinder (301), an air intake curved surface (302), an end support ring (303), a compressor inner ring (304), and a support inner connecting ring (305). The support cylinder (301) is fixedly connected to the inside of the guide end shell (106), and the surface of one end of the support cylinder (301) is fixedly connected to the inner wall of the mounting bracket (206). The air intake curved surface (302) is integrally disposed on the surface of the support cylinder (301) near the end of the guide end shell (106). The end support ring (303) is fixedly connected to the inside of the flame retardant bracket (203) and the fixing bracket (210). The end support ring (303) is located in the support... The cylinder (301) is located away from the intake curved surface (302). The inner air ring (304) is fixedly sleeved on the surface of the support cylinder (301). The surface of the inner air ring (304) is respectively provided with a second flow guiding surface and a third flow guiding surface. The second flow guiding surface is located on the side of the outer air ring (105) close to the flow guiding sub-shell (201). The third flow guiding surface is located on the side of the outer air ring (105) away from the flow guiding sub-shell (201). The inner support ring (305) is integrally set at the end of the support cylinder (301) close to the end support ring (303) and the end support ring (303) close to the support cylinder (301).

6. The three-intake-channel adjustable outlet intake volute design according to claim 5, characterized in that, The gas equalization and anti-interference guiding mechanism includes a compressed air guiding ring (401) and a guiding baffle (402). The compressed air guiding ring (401) is fixedly connected to the inner wall of the guiding main shell (101). The surface of the compressed air guiding ring (401) is provided with a fourth guiding curved surface. The guiding baffle (402) is integrally set on the side of the compressed air guiding ring (401) away from the compressed air outer ring (105). There are multiple guiding baffles (402). The multiple guiding baffles (402) are distributed in parallel and are evenly distributed on one side of the compressed air guiding ring (401). The surfaces of the multiple guiding baffles (402) are all fixedly connected to the outer surface of the support cylinder (301).

7. The three-intake-channel adjustable outlet intake volute design according to claim 5, characterized in that, The heat dissipation and fire extinguishing mechanism includes a first conversion seat (501), a first guide hole (502), a liquid pump (503), a first one-way valve (504), and an inlet bend (505). The first conversion seat (501) is fixedly connected to the surface of the main guide shell (101) and is located below the main guide shell (101). The first guide hole (502) is opened through the interior of the first conversion seat (501). The liquid pump (503) is fixedly installed on the outside of the first conversion seat (501). The output end of the first conversion seat (501) is connected to the first guide hole (502). The first one-way valve (504) is fixedly connected to the output end of the first conversion seat (501). The first one-way valve (504) unidirectionally guides the flow to the first guide hole (502). There are two water inlet bends (505). The two water inlet bends (505) are fixedly connected to the two ends of the first guide hole (502). One water inlet bend (505) penetrates the outer surface of the guide main shell (101) and extends to the inside of the compressed air outer ring (105). The other water inlet bend (505) penetrates the outer surface of the guide main shell (101) and extends to the inside of the compressed air guide ring (401).

8. The three-intake-channel adjustable outlet intake volute design according to claim 7, characterized in that, The heat dissipation and fire extinguishing mechanism includes a second conversion seat (506), a second guide hole (507), a first electromagnetic switch valve (508), and a drain bend (509). The second conversion seat (506) is fixedly connected to the surface of the guide main shell (101), and the second conversion seat (506) is distributed opposite to the first conversion seat (501). The second guide hole (507) is opened through the interior of the second conversion seat (506), and the first electromagnetic switch valve (508) is fixedly installed on the second conversion seat (506). On the outer surface of the first electromagnetic switch valve (508), one end of the first electromagnetic switch valve (508) is connected to the second guide hole (507). There are two drain bends (509). The two drain bends (509) are fixedly connected to the two ends of the second guide hole (507). One drain bend (509) penetrates the outer surface of the guide main shell (101) and extends into the interior of the compressed air outer ring (105). The other drain bend (509) penetrates the outer surface of the guide main shell (101) and extends into the interior of the compressed air guide ring (401).

9. The three-intake-channel adjustable outlet intake volute design according to claim 8, characterized in that, The heat dissipation and fire extinguishing mechanism includes a third conversion seat (510), a lower through hole (511), a second electromagnetic switch valve (512), a connecting pipe (513), and a second one-way valve (514). There are two third conversion seats (510), both of which are fixedly connected to the surface of the main flow guide shell (101). The two third conversion seats (510) are distributed opposite to each other. The lower through hole (511) is opened through the outside of the third conversion seat (510) and extends to the main flow guide shell (101). The inner surface of the second electromagnetic switch valve (512) is fixedly installed on the outside of the third conversion seat (510). The output end of the second electromagnetic switch valve (512) is connected to the lower through hole (511). The connecting pipe (513) is fixedly connected inside the lower through hole (511). The second one-way valve (514) is fixedly connected inside the lower through hole (511). The second one-way valve (514) guides the main housing (101) to unidirectionally. The second guide surface is located between the lines connecting the two connecting pipes (513).

Citation Information

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