CN218407612U - Ventilation structure of gas turbine housing - Google Patents
Ventilation structure of gas turbine housing Download PDFInfo
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- CN218407612U CN218407612U CN202222737244.0U CN202222737244U CN218407612U CN 218407612 U CN218407612 U CN 218407612U CN 202222737244 U CN202222737244 U CN 202222737244U CN 218407612 U CN218407612 U CN 218407612U
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- groove
- mounting
- gas turbine
- main body
- guide plate
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Abstract
The utility model provides a ventilation structure of a gas turbine housing, which relates to the technical field of ventilator covers and aims to solve the problems that the structure of the existing gas turbine housing is imperfect, and the housing is usually arranged at the outer end of the gas turbine when in use, so that the housing needs to be dismantled by spending time when the gas turbine is maintained, and the operation is very troublesome, including an installation mechanism; the protective device is characterized in that the mounting mechanism is provided with a protective assembly, a protective plate of the protective assembly is arranged at the upper end of the main body, the protective assembly comprises a clamping groove and a guide plate, and the clamping groove is formed in the front ends of the two sides of the bottom of the protective plate. When the gas turbine inside the protection shield needs to be maintained, the protection shield is pulled upwards to drive the guide plate to move upwards, the bottom of the guide plate is moved out of the fixing groove, at the moment, the elastic piece pushes the guide plate towards the rear end, the protection shield is exposed, and the gas turbine in the protection shield is exposed.
Description
Technical Field
The utility model belongs to the technical field of the ventilator cover, more specifically says, in particular to gas turbine housing ventilation structure.
Background
The gas turbine is usually provided with a housing with a ventilation function at an outer end when in use, so that the gas turbine in operation is protected by the housing.
Based on prior art discovery, the structure of current gas turbine housing is imperfect, and when using, the housing is usually in gas turbine's outer end, and this just makes when maintaining gas turbine, and it takes time to dismantle the housing, and the operation is very troublesome like this, and the heat radiation structure of current gas turbine housing is imperfect, and when using, radiator unit installs on the housing through the bolt usually, so, when maintaining radiator unit, be not convenient for dismantle radiator unit fast.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a gas turbine housing ventilation structure, with the structure that solves current gas turbine housing is imperfect, when using, the housing is usually in gas turbine's outer end, this just makes when maintaining gas turbine, it takes time to dismantle the housing, it is very troublesome to operate like this, and the heat radiation structure of current gas turbine housing is imperfect, when using, radiator unit installs on the housing through the bolt usually, so, when maintaining radiator unit, be not convenient for carry out quick problem of dismantling to radiator unit.
The purpose and the efficacy of the ventilation structure of the gas turbine housing are achieved by the following specific technical means:
a gas turbine shroud ventilation arrangement comprising:
an installation mechanism; the protective device comprises a main body, a mounting mechanism, a protective plate, a clamping groove and guide plates, wherein the mounting mechanism is provided with the protective assembly, the protective plate of the protective assembly is arranged at the upper end of the main body, the protective assembly comprises the clamping groove and the guide plates, the clamping groove is formed in the front ends of the two sides of the bottom of the protective plate, the guide plates are arranged in two groups, the tops of the guide plates are inserted into the clamping groove, a rectangular groove is formed in the guide plates, the guide plates are positioned in sliding grooves in the outer side of the main body, the guide plates are penetrated by round rods in the sliding grooves, and the bottoms of the guide plates are inserted into fixing grooves in the sliding grooves; the protection component is internally provided with two groups of heat dissipation components, the mounting frames of the heat dissipation components are arranged at two ends of the protection plate and clamped in the mounting grooves, and the round rods with moving blocks are inserted into the fixing holes in the outer ends of the mounting frames.
Further, the mounting mechanism includes: a main body and a heat dissipation hole; the main body is of a rectangular structure, and a circular heat dissipation circular hole is clamped in the main body; the radiating holes are formed in the inner end of the main body and penetrate through two sides of the main body, and the radiating holes are communicated with radiating round holes in the main body.
Further, the mounting mechanism further includes: a chute and a fixing groove; the sliding grooves are symmetrically arranged on two sides of the main body, and circular rods are arranged inside the sliding grooves; the fixed slot is arranged at the lower end of the front side of the sliding groove.
Further, the protection component further comprises: a protection plate and a mounting groove; the top of the protection plate is of an arc structure, and pull rods are arranged at two ends of the protection plate; the mounting grooves are two groups, the mounting grooves are symmetrically arranged on two sides of the protection plate, and the mounting grooves penetrate through two sides of the protection plate.
Further, the protection component further comprises: a moving groove and a moving block; the movable grooves are symmetrically arranged on two sides of the protection plate and are positioned on two sides of the mounting groove; the moving block is slidably mounted in the moving groove through the elastic piece, and the tail end of a round rod on the moving block penetrates through the protection plate and is located in the mounting groove.
Further, the heat dissipation assembly includes: the mounting frame and the fixing hole; two groups of heat dissipation fans connected with a power supply are arranged in the mounting rack; four groups of fixing holes are formed in the fixing frame, and the fixing holes are symmetrically formed in two sides of the mounting frame.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. in the device, an installation structure and a protection assembly are arranged, sliding grooves are arranged on two sides of a main body, a protection plate is installed at the upper end of the main body, two groups of clamping grooves are arranged at the bottom of the front side of the protection plate, a guide plate with a rectangular through hole is inserted into the clamping grooves to be fixed, the bottom of the guide plate is slidably installed in the sliding grooves, a round rod in each sliding groove penetrates through the guide plate, the front side of the guide plate is in contact with an elastic piece on the round rod in each sliding groove, the bottom of the guide plate is inserted into the fixed groove, so that the guide plate is fixed on the sliding grooves, when a gas turbine in the protection plate needs to be maintained, the protection plate is pulled upwards to drive the guide plate to move upwards and move out of the bottom of the guide plate from the fixed groove, and at the moment, the elastic piece pushes the guide plate towards the rear end and exposes the protection plate, so that the gas turbine in the protection plate is exposed;
2. in this device, protection component and radiator unit have been set up, set up the rectangle mounting groove in the both sides of protection shield board, the mounting bracket that will have the heat dissipation fan is pegged graft in the mounting groove, the shifting chute is seted up in the both sides of mounting groove, pass through elastic component slidable mounting to the shifting chute with the movable block, make the round bar on the movable block run through the protection shield and peg graft in the fixed orifices, make the mount fix in the mounting groove, when needs dismantle radiator unit and maintain, to both sides pulling movable block, make the round bar on the movable block break away from in the fixed orifices, just so make the movable block lose spacing to the mounting bracket, at this moment, can carry out quick dismantlement with radiator unit.
Drawings
Fig. 1 is a schematic perspective view of the present invention.
Fig. 2 is an exploded schematic view of the present invention.
Fig. 3 is a schematic view of the protection assembly according to the present invention.
Fig. 4 is a schematic view of the local connection structure of the present invention.
1. An installation mechanism;
101. a main body; 1011. heat dissipation holes;
102. a chute; 1021. fixing grooves;
2. a protection component;
201. a protection plate; 2011. mounting grooves;
202. a moving groove; 2021. a moving block;
203. a clamping groove; 2031. a guide plate;
3. a heat dissipating component;
301. a mounting frame; 302. and (7) fixing holes.
Detailed Description
The following describes embodiments of the present invention in further detail with reference to the drawings and examples. The following examples are intended to illustrate the present invention, but are not intended to limit the scope of the present invention.
In the description of the present application, unless otherwise specified, "a plurality" means two or more; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present application and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present application. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present application, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as being fixed or detachable or integrally connected; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present application can be understood in a specific case by those skilled in the art.
Example (b):
as shown in figures 1 to 4:
the utility model provides a gas turbine housing ventilation structure, include: an installation mechanism 1; the installation mechanism 1 is provided with a protection component 2, a protection plate 201 of the protection component 2 is arranged at the upper end of the main body 101, the protection component 2 comprises a clamping groove 203 and two guide plates 2031, the clamping groove 203 is arranged at the front end of the two sides of the bottom of the protection plate 201, the guide plates 2031 are provided with two groups, the top of each guide plate 2031 is inserted into the clamping groove 203, a rectangular groove is arranged inside each guide plate 2031, each guide plate 2031 is positioned in the sliding groove 102 at the outer side of the main body 101, each guide plate 2031 is penetrated by a round rod in the corresponding sliding groove 102, and the bottom of each guide plate 2031 is inserted into the corresponding fixing groove 1021 in the corresponding sliding groove 102; be equipped with two sets of radiator unit 3 in the protection component 2, radiator unit 3's mounting bracket 301 is established at the both ends of protection shield 201, and mounting bracket 301 block is in mounting groove 2011 to the fixed orifices 302 of mounting bracket 301 outer end is pegged graft and is had the round bar of movable block 2021.
As shown in fig. 1-2, among other things, the mounting mechanism 1 includes: a main body 101 and heat dissipation holes 1011; the main body 101 is of a rectangular structure, and a circular heat dissipation circular hole is clamped in the main body 101; the heat dissipation hole 1011 is formed at the inner end of the main body 101, the heat dissipation hole 1011 penetrates through two sides of the main body 101, and the heat dissipation hole 1011 is communicated with a heat dissipation round hole in the main body 101; the gas engine wheel fixing device is characterized in that a rectangular main body 101 is arranged, a gas engine wheel can be installed on the main body 101, a rectangular heat dissipation hole 1011 is arranged, the heat dissipation hole 1011 is communicated with a circular heat dissipation through hole in the main body 101, and when the gas engine wheel fixing device is used, heat dissipated by the gas engine wheel can be dissipated through the heat dissipation hole 1011, a sliding groove 102 and a fixing groove 1021; the sliding grooves 102 are provided with two groups, the sliding grooves 102 are symmetrically arranged on two sides of the main body 101, and a circular rod is arranged inside the sliding grooves 102; the fixing groove 1021 is provided at the lower end of the front side of the slide groove 102, the rectangular slide groove 102 is provided, the guide plate 2031 on the protection plate 201 can be slidably attached to both sides of the main body 101, the rectangular fixing groove 1021 is provided, and the guide plate 2031 can be fixed in the slide groove 102 by inserting the bottom of the guide plate 2031 into the fixing groove 1021.
As shown in fig. 2-3, wherein the protection assembly 2 further comprises: a protection plate 201 and a mounting groove 2011; the top of the protection plate 201 is of an arc structure, and pull rods are arranged at two ends of the protection plate 201; the mounting grooves 2011 are provided with two groups, the mounting grooves 2011 are symmetrically arranged on two sides of the protection plate 201, and the mounting grooves 2011 penetrate through two sides of the protection plate 201; the protection plate 201 is arranged, the gas turbine is placed inside the protection plate 201 for protection, the rectangular installation groove 2011 is arranged, the heat dissipation assembly 3 can be placed in the protection plate 201 through the installation groove 2011 for fixation, and the moving groove 202 and the moving block 2021 are arranged; the moving grooves 202 are provided with four groups, the moving grooves 202 are symmetrically arranged on two sides of the protection plate 201, and the moving grooves 202 are arranged on two sides of the mounting groove 2011; the moving block 2021 is slidably mounted in the moving groove 202 through an elastic member, the end of a round rod on the moving block 2021 penetrates through the protection plate 201 and is located in the mounting groove 2011, the rectangular moving groove 202 is provided, the moving block 2021 can be mounted inside two sides of the protection plate 201 through the moving groove 202, the rectangular moving block 2021 with the round rod is provided, and the round rod on the moving block 2021 penetrates through the protection plate 201 and is inserted into the fixing hole 302, so that the mounting rack 301 can be fixed in the mounting groove 2011 of the protection plate 201.
As shown in fig. 4, the heat sink assembly 3 includes: a mounting bracket 301 and a fixing hole 302; two groups of heat dissipation fans connected with a power supply are arranged inside the mounting rack 301; the fixing holes 302 are provided with four groups, the fixing holes 302 are symmetrically arranged on two sides of the mounting frame 301, the rectangular mounting frame 301 is arranged, the heat dissipation fan connected with the power supply can be mounted in the mounting frame 301, and the heat dissipation fan can be used for heat dissipation and ventilation of the gas turbine inside the protection plate 201.
The specific use mode and function of the embodiment are as follows:
the utility model discloses in, as shown in fig. 1-4, place gas turbine and hold on main part 101, mounting bracket 301 that will have the heat dissipation fan is pegged graft in the mounting groove 2011 of protection shield 201 both sides, set up shifting chute 202 in protection shield 201 both sides, run through protection shield 201 and peg graft in fixed orifices 302 with the round bar on the inboard movable block 2021 of shifting chute 202, thereby fix mounting bracket 301 in mounting groove 2011, install main part 101 upper end with protection shield 201, make protection shield 201 lock in gas turbine's the outside, set up spout 102 in main part 101's both sides, peg graft in protection shield 201's front side bottom two sets of deflectors 2031 with deflector 2031 bottom slidable mounting in spout 102, make the front side of deflector 2031 and the elastic component on the round bar contact in spout 102, to front end pulling 201, after pulling a certain position, through pressing protection shield 201 downwards, make deflector 2031 bottom peg graft in fixed slots 1021, just so can fix protection shield 201 on main part 101, make gas turbine 201 carry out the heat dissipation on main part, start the heat dissipation fan, make the protection shield 201, make the heat dissipation fan in the heat dissipation fan carry out the protection shield 201.
The embodiments of the present application have been presented for purposes of illustration and description, and are not intended to be exhaustive or limited to the invention in the form disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art. The embodiment was chosen and described in order to best explain the principles of the invention and the practical application, and to enable others of ordinary skill in the art to understand the invention for various embodiments with various modifications as are suited to the particular use contemplated.
Claims (6)
1. A gas turbine shroud ventilation structure, comprising: an installation mechanism (1); the protective assembly (2) is arranged on the installation mechanism (1), the protective plate (201) of the protective assembly (2) is arranged at the upper end of the main body (101), the protective assembly (2) comprises a clamping groove (203) and a guide plate (2031), the clamping groove (203) is formed in the front end of two sides of the bottom of the protective plate (201), the guide plate (2031) is provided with two groups, the top of the guide plate (2031) is inserted into the clamping groove (203), a rectangular groove is formed in the guide plate (2031), the guide plate (2031) is located in the sliding groove (102) on the outer side of the main body (101), the guide plate (2031) is penetrated through by a round rod in the sliding groove (102), and the bottom of the guide plate (2031) is inserted into a fixing groove (1021) in the sliding groove (102); be equipped with two sets of radiator unit (3) in protection component (2), the both ends at protection shield (201) are established in mounting bracket (301) of radiator unit (3), and mounting bracket (301) block is in mounting groove (2011) to the fixed orifices (302) of mounting bracket (301) outer end are pegged graft and are had the round bar of movable block (2021).
2. A gas turbine casing ventilating structure according to claim 1, wherein said mounting mechanism (1) comprises: a main body (101) and heat dissipation holes (1011); the main body (101) is of a rectangular structure, and circular heat dissipation round holes are clamped in the main body (101); the heat dissipation hole (1011) is formed in the inner end of the main body (101), the heat dissipation hole (1011) penetrates through two sides of the main body (101), and the heat dissipation hole (1011) is communicated with a heat dissipation round hole in the main body (101).
3. A gas turbine casing ventilating structure according to claim 2, wherein said mounting mechanism (1) further comprises: a sliding chute (102) and a fixing groove (1021); the sliding grooves (102) are arranged in two groups, the sliding grooves (102) are symmetrically arranged on two sides of the main body (101), and circular rods are arranged inside the sliding grooves (102); the fixing groove (1021) is arranged at the lower end of the front side of the sliding groove (102).
4. A gas turbine casing ventilation arrangement as claimed in claim 1, characterised in that said protection assembly (2) further comprises: a protection plate (201) and a mounting groove (2011); the top of the protection plate (201) is of an arc structure, and pull rods are arranged at two ends of the protection plate (201); the mounting grooves (2011) are provided with two groups, the mounting grooves (2011) are symmetrically arranged on two sides of the protection plate (201), and the mounting grooves (2011) penetrate through two sides of the protection plate (201).
5. A gas turbine casing ventilation arrangement as claimed in claim 4, characterised in that said protection assembly (2) further comprises: a moving groove (202) and a moving block (2021); the movable grooves (202) are provided with four groups, the movable grooves (202) are symmetrically arranged on two sides of the protection plate (201), and the movable grooves (202) are positioned on two sides of the mounting groove (2011); the moving block (2021) is slidably mounted in the moving groove (202) through an elastic piece, and the tail end of a round rod on the moving block (2021) penetrates through the protection plate (201) and is located in the mounting groove (2011).
6. A gas turbine casing ventilation structure according to claim 1, characterised in that said heat dissipating assembly (3) comprises: a mounting frame (301) and a fixing hole (302); two groups of heat dissipation fans connected with a power supply are arranged in the mounting rack (301); the fixed holes (302) are provided with four groups, and the fixed holes (302) are symmetrically arranged on two sides of the mounting rack (301).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222737244.0U CN218407612U (en) | 2022-10-18 | 2022-10-18 | Ventilation structure of gas turbine housing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222737244.0U CN218407612U (en) | 2022-10-18 | 2022-10-18 | Ventilation structure of gas turbine housing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218407612U true CN218407612U (en) | 2023-01-31 |
Family
ID=85002321
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222737244.0U Active CN218407612U (en) | 2022-10-18 | 2022-10-18 | Ventilation structure of gas turbine housing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218407612U (en) |
-
2022
- 2022-10-18 CN CN202222737244.0U patent/CN218407612U/en active Active
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| GR01 | Patent grant |