CN216142815U - Gas turbine for gas plant - Google Patents

Gas turbine for gas plant Download PDF

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Publication number
CN216142815U
CN216142815U CN202122028063.6U CN202122028063U CN216142815U CN 216142815 U CN216142815 U CN 216142815U CN 202122028063 U CN202122028063 U CN 202122028063U CN 216142815 U CN216142815 U CN 216142815U
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China
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plate
fixedly connected
gas turbine
placing plate
mounting plates
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CN202122028063.6U
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Chinese (zh)
Inventor
张厚宝
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Beijing Shangzhuang Gas Thermoelectricity Co ltd
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Individual
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Abstract

The utility model discloses a gas turbine for a gas plant, which comprises a gas turbine body and a bottom plate, wherein the top of the bottom plate is fixedly connected with two mounting plates, fixed plates are respectively fixedly connected between the two mounting plates near the front side and the rear side, the bottom of the fixed plate is fixedly connected with the bottom plate, a placing plate is arranged between the two mounting plates, the placing plate is arranged in an arc shape, rectangular openings are respectively arranged on the side walls of the two mounting plates, the left side and the right side of the placing plate respectively penetrate through the rectangular openings and extend out of the mounting plates, one side far away from the two mounting plates is respectively provided with a locking mechanism, the locking mechanisms are fixedly connected with the placing plate, fixed blocks are respectively fixedly connected at the positions near the left side and the right side of the bottom of the placing plate, and the gas turbine body can be fixed on the placing plate through the mutual matching among the mounting plates, the placing plate, a limiting plate, the locking mechanism, a screw rod and the like, can effectively achieve convenient installation.

Description

Gas turbine for gas plant
Technical Field
The utility model relates to the technical field of gas turbines, in particular to a gas turbine for a gas plant.
Background
The gas turbine is an internal combustion type power machine which takes continuously flowing gas as a working medium to drive an impeller to rotate at a high speed and converts the energy of fuel into useful work, and the internal combustion type power machine is a rotary impeller type heat engine and has the advantages of light weight, small volume, high device efficiency, less pollution, flexible start and stop and the like.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome the defects of inconvenient installation, poor protection effect and the like in the prior art and provides the gas turbine for the gas plant. The gas turbine for the gas plant has the characteristics of convenience in installation, good protection effect and the like.
In order to achieve the purpose, the utility model provides the following technical scheme: a gas turbine for a gas plant comprises a gas turbine body and a bottom plate, wherein the top of the bottom plate is fixedly connected with two mounting plates, a fixed plate is respectively fixedly connected between the two mounting plates near the front side and the rear side, the bottom of the fixed plate is fixedly connected with the bottom plate, a placing plate is arranged between the two mounting plates and is in an arc shape, rectangular openings are respectively arranged on the side walls of the two mounting plates, the left side and the right side of the placing plate respectively penetrate through the rectangular openings and extend out of the mounting plates, one side of the two mounting plates far away from each other is respectively provided with a locking mechanism, the locking mechanism is fixedly connected with the placing plate, fixed blocks are respectively fixedly connected at the positions of the bottom of the placing plate near the left side and the right side, the bottom of each fixed block is fixedly connected with a first spring, the bottom end of the first spring is fixedly connected with the bottom plate, and a limit pipe is fixedly connected with the top of the bottom plate, be provided with the standpipe in the spacing pipe, the standpipe top with place board fixed connection, be provided with the second spring in the standpipe, the second spring both ends respectively with place board and bottom plate fixed connection, the gas turbine body is placed in placing the board, gas turbine body top is provided with the limiting plate, the limiting plate is the arc setting, limiting plate top is close to left and right sides department and has seted up spacing hole respectively, it is close to left and right sides department respectively fixedly connected with lead screw, two to place the board top the lead screw bottom passes spacing hole respectively and extends to the limiting plate top, two install the nut on the lead screw respectively.
Preferably, locking mechanical system includes the casing, one side and the mounting panel fixed connection that the casing is relative with the mounting panel, two the casing is provided with the rack respectively, one side that rack and mounting panel are relative is provided with a plurality of evenly distributed's fixed tooth, fixed tooth meshes with the rack mutually, one side that fixed tooth and mounting panel are relative with place board fixed connection, the threaded hole is seted up to one side that the casing was kept away from mutually with the mounting panel, install the threaded rod in the threaded hole, threaded rod one end extends to in the casing with rack swing joint, the other end extends to the outer fixedly connected with dwang of casing.
Preferably, one side of the shell far away from the mounting plate is provided with two T-shaped rods respectively, the side wall of the shell is provided with two round holes matched with the T-shaped rods, and one ends of the T-shaped rods opposite to the shell penetrate through the round holes respectively and extend into the shell to be fixedly connected with the rack.
Preferably, the top of the bottom plate is provided with screw holes close to the left side and the right side respectively, and bolts are installed in the screw holes.
Preferably, the front side wall and the rear side wall of the placing plate are close to the left side and the right side and are respectively fixedly connected with first sliding blocks, and first sliding grooves matched with the first sliding blocks are respectively formed in the front inner wall and the rear inner wall of the rectangular opening.
Preferably, the opposite sides of the placing plate and the limiting plate are respectively and fixedly connected with a heat insulation gasket.
Preferably, the side wall is fixedly connected with second slider respectively about the standpipe, the inner wall is seted up respectively about the spacing pipe with second slider assorted second spout.
Compared with the prior art, the utility model has the beneficial effects that:
1. in the technical scheme, the mounting plate, the placing plate, the limiting plate, the locking mechanism, the screw rod and the like are matched with each other, so that the gas turbine body can be fixed on the placing plate, and convenient and fast installation can be effectively achieved;
2. in this technical scheme, through mutually supporting between first spring, second spring, spacing pipe etc. can realize when placing the gas turbine body, if appear placing when shaking too fast, play the purpose of bradyseism by first spring and second spring, can effectual improvement its protection effect.
Drawings
FIG. 1 is a perspective view of the present invention;
FIG. 2 is a schematic structural view of the present invention;
FIG. 3 is an enlarged view taken at A in FIG. 2;
fig. 4 is an enlarged view of fig. 2 at B.
Reference numbers in the figures: 1. a base plate; 2. mounting a plate; 3. a fixing plate; 4. placing the plate; 5. a rectangular opening; 6. a locking mechanism; 61. a housing; 62. a rack; 63. fixing teeth; 64. a threaded rod; 65. a threaded hole; 66. rotating the rod; 7. a fixed block; 8. a first spring; 9. a limiting pipe; 10. a vertical tube; 11. a second spring; 12. a limiting plate; 13. a nut; 14. a limiting hole; 15. a gas turbine body; 16. a silk hole; 17. a bolt; 18. a screw rod; 19. t-shaped rods.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: a gas turbine for a gas plant comprises a gas turbine body 15 and a bottom plate 1, wherein the top of the bottom plate 1 is fixedly connected with two mounting plates 2, a fixed plate 3 is fixedly connected between the two mounting plates 2 near the front side and the rear side respectively, the bottom of the fixed plate 3 is fixedly connected with the bottom plate 1, a placing plate 4 is arranged between the two mounting plates 2, the placing plate 4 is arranged in an arc shape, rectangular openings 5 are respectively arranged on the side walls of the two mounting plates 2, the left side and the right side of the placing plate 4 respectively penetrate through the rectangular openings 5 and extend out of the mounting plates 2, first sliding blocks are fixedly connected to the front side and the rear side of the placing plate 4 near the left side and the right side respectively, first sliding grooves matched with the first sliding blocks are respectively arranged on the front inner wall and the rear wall of the rectangular openings 5, locking mechanisms 6 are respectively arranged on the far sides of the two mounting plates 2, the locking mechanisms 6 are fixedly connected with the placing plate 4, and fixed blocks 7 are respectively fixedly connected to the bottom of the placing plate 4 near the left side and the right side, the bottom of the fixed block 7 is fixedly connected with a first spring 8, the bottom end of the first spring 8 is fixedly connected with the bottom plate 1, the top of the bottom plate 1 is fixedly connected with a limiting pipe 9, a vertical pipe 10 is arranged in the limiting pipe 9, the top end of the vertical pipe 10 is fixedly connected with a placing plate 4, the left side wall and the right side wall of the vertical pipe 10 are respectively fixedly connected with a second slider, the left inner wall and the right inner wall of the limiting pipe 9 are respectively provided with a second chute matched with the second slider, a second spring 11 is arranged in the vertical pipe 10, two ends of the second spring 11 are respectively fixedly connected with the placing plate 4 and the bottom plate 1, a gas turbine body 15 is placed in the placing plate 4, a limiting plate 12 is arranged above the gas turbine body 15, the limiting plate 12 is arranged in an arc shape, one side opposite to the placing plate 4 and the limiting plate 12 is respectively and fixedly connected with a heat insulation gasket, the top of the limiting plate 12 is respectively provided with a limiting hole 14 near the left side and the right side, the top of the placing plate 4 is respectively and fixedly connected with a lead screw 18 near the left side and the right side, the bottom ends of the two screw rods 18 respectively penetrate through the limiting holes 14 and extend to the upper side of the limiting plate 12, nuts 13 are respectively installed on the two screw rods 18, screw holes 16 are respectively formed in the positions, close to the left side and the right side, of the top of the bottom plate 1, and bolts 17 are installed in the screw holes 16.
Through mutually supporting between first spring 8, second spring 11, spacing pipe 9 etc. can realize when placing gas turbine body 15, if appear placing when shaking too soon, play the purpose of bradyseism by first spring 8 and second spring 11, can its protective effect of effectual improvement.
The locking mechanism 6 comprises a shell 61, one side of the shell 61 opposite to the mounting plate 2 is fixedly connected with the mounting plate 2, the two shells 61 are respectively provided with a rack 62, one side of the rack 62 opposite to the mounting plate 2 is provided with a plurality of fixing teeth 63 which are uniformly distributed, the fixing teeth 63 are meshed with the rack 62, one side of the fixing teeth 63 opposite to the mounting plate 2 is fixedly connected with the placing plate 4, one side of the shell 61 far away from the mounting plate 2 is provided with a threaded hole 65, a threaded rod 64 is arranged in the threaded hole 65, one end of the threaded rod 64 extends into the shell 61 to be movably connected with the rack 62, the other end extends out of the shell 61 to be fixedly connected with a rotating rod 66, one side of the shell 61 far away from the mounting plate 2 is respectively provided with two T-shaped rods 19, the side wall of the shell 61 is provided with two round holes matched with the T-shaped rods 19, one ends of the two T-shaped rods 19 opposite to the shell 61 respectively penetrate through the round holes and extend into the shell 61 to be fixedly connected with the rack 62, through the mutual cooperation between the mounting plate 2, the placing plate 4, the limiting plate 12, the locking mechanism 6, the screw rod 18 and the like, the gas turbine body 15 can be fixed on the placing plate 4, and the convenient installation can be effectively achieved.
The working principle is as follows: when the technical scheme is used, firstly, the nut 13 is rotated, the nut 13 and the limit plate 12 are taken down, then the gas turbine body 15 is placed on the placing plate 4, when the gas turbine body 15 is placed on the placing plate 4, the gravity of the gas turbine body 15 enables the placing plate 4 to descend to compress the first spring 8 and the second spring 11, the purpose of cushioning the gas turbine body 15 is achieved, then the limit plate 12 is installed above the gas turbine body 15 through the screw rod 18, then the limit plate 12 is fixed above the gas turbine body 15 through the nut 13, the purpose of fixing the gas turbine body 15 is achieved, then the rotating rod 66 rotates, make rack 62 inward movement combine together with fixed tooth 63, reach the fixed position's that will place board 4 purpose, prevent that gas turbine body 15 from appearing rocking's purpose when using, can effectually reach its convenient purpose of installing.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. A gas turbine for a gas plant, comprising a gas turbine body (15) and a base plate (1), characterized in that: the top of the bottom plate (1) is fixedly connected with two mounting plates (2), a fixing plate (3) is fixedly connected between the two mounting plates (2) near the front side and the rear side respectively, the bottom of the fixing plate (3) is fixedly connected with the bottom plate (1), a placing plate (4) is arranged between the two mounting plates (2), the placing plate (4) is arranged in an arc shape, rectangular openings (5) are respectively arranged on the side walls of the two mounting plates (2), the left side and the right side of the placing plate (4) respectively penetrate through the rectangular openings (5) and extend out of the mounting plates (2), one sides of the two mounting plates (2) far away are respectively provided with a locking mechanism (6), the locking mechanism (6) is fixedly connected with the placing plate (4), the bottom of the placing plate (4) near the left side and the right side are respectively fixedly connected with a fixing block (7), and the bottom of the fixing block (7) is fixedly connected with a first spring (8), the bottom end of the first spring (8) is fixedly connected with the bottom plate (1), the top of the bottom plate (1) is fixedly connected with a limiting pipe (9), a vertical pipe (10) is arranged in the limiting pipe (9), the top end of the vertical pipe (10) is fixedly connected with the placing plate (4), a second spring (11) is arranged in the vertical pipe (10), two ends of the second spring (11) are respectively fixedly connected with the placing plate (4) and the bottom plate (1), the gas turbine body (15) is placed in the placing plate (4), a limiting plate (12) is arranged above the gas turbine body (15), the limiting plate (12) is arranged in an arc shape, limiting holes (14) are respectively formed in the positions, close to the left side and the right side, of the top of the limiting plate (12), lead screws (18) are respectively fixedly connected with the positions, close to the left side and the right side, of the top of the placing plate (4), two lead screws (18) pass through the limiting holes (14) respectively and extend to the tops of the limiting plate (12), and nuts (13) are respectively arranged on the two screw rods (18).
2. The gas turbine for a gas plant according to claim 1, wherein: the locking mechanism (6) comprises a shell (61), one side of the shell (61) opposite to the mounting plate (2) is fixedly connected with the mounting plate (2), the two shells (61) are respectively provided with a rack (62), one side of the rack (62) opposite to the mounting plate (2) is provided with a plurality of uniformly distributed fixed teeth (63), the fixed teeth (63) are meshed with the racks (62), one side of the fixed teeth (63) opposite to the mounting plate (2) is fixedly connected with the placing plate (4), a threaded hole (65) is arranged on one side of the shell (61) far away from the mounting plate (2), install threaded rod (64) in screw hole (65), threaded rod (64) one end extend to casing (61) in with rack (62) swing joint, the other end extends to the outer fixedly connected with dwang (66) of casing (61).
3. The gas turbine for a gas plant according to claim 2, wherein: casing (61) and mounting panel (2) keep away from one side mutually and be provided with two T shape poles (19) respectively, set up two on casing (61) lateral wall and T shape pole (19) assorted round hole, two the one end that T shape pole (19) and casing (61) are relative passes the round hole respectively and extends to casing (61) in with rack (62) fixed connection.
4. The gas turbine for a gas plant according to claim 1, wherein: the top of the bottom plate (1) is provided with screw holes (16) close to the left side and the right side respectively, and bolts (17) are installed in the screw holes (16).
5. The gas turbine for a gas plant according to claim 1, wherein: the front side wall and the rear side wall of the placing plate (4) are close to the left side and the right side and are respectively fixedly connected with first sliding blocks, and first sliding grooves matched with the first sliding blocks are respectively formed in the front inner wall and the rear inner wall of the rectangular opening (5).
6. The gas turbine for a gas plant according to claim 1, wherein: and one sides of the placing plate (4) opposite to the limiting plate (12) are fixedly connected with heat insulation gaskets respectively.
7. The gas turbine for a gas plant according to claim 1, wherein: the side wall is fixedly connected with second slider respectively about standpipe (10), inner wall is seted up respectively about spacing pipe (9) with second slider assorted second spout.
CN202122028063.6U 2021-08-26 2021-08-26 Gas turbine for gas plant Active CN216142815U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122028063.6U CN216142815U (en) 2021-08-26 2021-08-26 Gas turbine for gas plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122028063.6U CN216142815U (en) 2021-08-26 2021-08-26 Gas turbine for gas plant

Publications (1)

Publication Number Publication Date
CN216142815U true CN216142815U (en) 2022-03-29

Family

ID=80808249

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202122028063.6U Active CN216142815U (en) 2021-08-26 2021-08-26 Gas turbine for gas plant

Country Status (1)

Country Link
CN (1) CN216142815U (en)

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20221026

Address after: 100094 West bungalow in the village committee yard of Ximafang Village, Shangzhuang Town, Haidian District, Beijing

Patentee after: BEIJING SHANGZHUANG GAS THERMOELECTRICITY CO.,LTD.

Address before: 518000 Room 201, building A, 1 front Bay Road, Shenzhen Qianhai cooperation zone, Shenzhen, Guangdong

Patentee before: Zhang Houbao

TR01 Transfer of patent right