CN202895072U - Auxiliary installation structure for turbine locking - Google Patents

Auxiliary installation structure for turbine locking Download PDF

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Publication number
CN202895072U
CN202895072U CN 201220615859 CN201220615859U CN202895072U CN 202895072 U CN202895072 U CN 202895072U CN 201220615859 CN201220615859 CN 201220615859 CN 201220615859 U CN201220615859 U CN 201220615859U CN 202895072 U CN202895072 U CN 202895072U
Authority
CN
China
Prior art keywords
turbine
locked
base
locking
installation structure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN 201220615859
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Chinese (zh)
Inventor
高锡民
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuxi Mingzhu Turbocharger Manufacturing Co Ltd
Original Assignee
Wuxi Mingzhu Turbocharger Manufacturing Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Mingzhu Turbocharger Manufacturing Co Ltd filed Critical Wuxi Mingzhu Turbocharger Manufacturing Co Ltd
Priority to CN 201220615859 priority Critical patent/CN202895072U/en
Application granted granted Critical
Publication of CN202895072U publication Critical patent/CN202895072U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model provides an auxiliary installation structure for turbine locking. A turbine to be locked can be applied to the auxiliary installation structure for turbine locking no matter the shaft of the turbine to be locked is long or short, and the auxiliary installation structure for turbine locking is good in generality. The auxiliary installation structure for turbine locking comprises a clamping head plate, wherein a clamping port is arranged in the clamping head plate, the shape and the size of the clamping port are matched with those of a turbine head, and the bottom of the clamping head plate is supported on the upper surface of a base. The auxiliary installation structure for turbine locking is characterized in that an air cylinder seat of an air cylinder is arranged on a lateral rail on the upper surface of the base, an air cylinder arm of the air cylinder is tightly fixed on the bottom face of a supporting block, the air cylinder moves along the vertical direction, the turbine head of the turbine to be locked is clamped in the corresponding clamping port, a central shaft end of the turbine to be locked is supported on the supporting block, a to-be-locked end of the turbine to be locked is exposed out of the corresponding supporting block, the bottom of the clamping head plate is arranged on a vertical linear rail of the base in a clamping mode, and the vertical linear rail is perpendicular to the vertical face of the clamping head plate and protrudes out of the upper surface of the base.

Description

A kind of auxiliary mounting structure of turbine locking
Technical field
The utility model relates to the booster turbine components fixing device, is specially a kind of auxiliary mounting structure of turbine locking.
Background technology
In the installation process of booster turbine, for locking nut, must fix turbine head, shape owing to turbine head during installation is different, adopt a kind of custom-designed chuck plate on the ground horizontal fix, the bayonet socket of the multiple turbine head shape and size such as circle, triangle, hexagon is arranged on the chuck plate, like this for different turbine heads, do not need the replacing instrument.But practical operation is sometimes not too convenient, this just need to adopt the turbine exemplar horizontal installation, for this reason, we have designed base, support, support, chuck plate are installed on base side by side, be provided with the brace table corresponding with bayonet socket at support, to solve horizontally-mounted problem, yet, the problem that this structure exists is that it only is that sub-fraction rides over the brace table on the support that the turbine exemplar needs an end of locking nut, owing to the distance between existing support, the chuck plate is fixed, inapplicable in short-term when the axle of turbine to be locked, cause its versatility poor.
The utility model content
For above-mentioned situation, the utility model provides a kind of auxiliary mounting structure of turbine locking, no matter the axial length of its turbine to be locked is short, all can be suitable for this structure, and the versatility of this structure is good.
A kind of auxiliary mounting structure of turbine locking, its technical scheme is such, it comprises chuck plate, be provided with the bayonet socket that the shape and size with turbine head are complementary at described chuck plate, described chuck plate bottom supporting is in the upper surface of base, it is characterized in that: the cylinder block of cylinder is installed on the upper surface cross track of described base, the bottom surface of the fastening described rest pad of cylinder arm of described cylinder, described cylinder moves in vertical direction, the turbine head of turbine to be locked is installed in the corresponding described bayonet socket, the middle part axle head of turbine described to be locked is supported on described rest pad, the locking end for the treatment of of turbine described to be locked exposes to described rest pad, the bottom of described chuck plate is installed in vertical rectilinear orbit of described base, described vertical rectilinear orbit is perpendicular to the facade of described chuck plate, and described rectilinear orbit evagination is in the upper surface of described base.
After the utility model adopts said structure, the turbine head of turbine to be locked is installed in corresponding bayonet socket, the middle part axle head of turbine to be locked is supported on rest pad, the locking end for the treatment of of turbine to be locked exposes to described rest pad, and the cylinder up-down adjustment is so that rest pad can adapt to the turbine to be locked of the position of differing heights, and cross track guarantees that the rest pad position is accurate, chuck plate moves along rectilinear orbit, no matter the axial length of turbine to be locked is short, all can be suitable for this structure, the versatility of this structure is good.
Description of drawings
Fig. 1 is main TV structure schematic diagram of the present utility model;
Fig. 2 is that the A of this Fig. 1 is to the view structure schematic diagram;
Fig. 3 is the top view structural representation of Fig. 1.
The specific embodiment
See Fig. 1, Fig. 2, Fig. 3, it comprises chuck plate 1, be provided with the bayonet socket 2 that the shape and size with turbine head are complementary at chuck plate 1, chuck plate 1 bottom supporting is in the upper surface of base 3, it is characterized in that: the cylinder block of cylinder 4 is installed on the upper surface cross track 5 of base 3, the bottom surface of the fastening rest pad 6 of the cylinder arm of cylinder 4, cylinder 4 moves in vertical direction, the turbine head of turbine to be locked is installed in the corresponding bayonet socket 2, the middle part axle head of turbine to be locked is supported on rest pad 6, the locking end for the treatment of of turbine to be locked exposes to rest pad 6, the bottom of chuck plate 1 is installed in vertical rectilinear orbit 7 of base, vertically rectilinear orbit 7 is perpendicular to the facade of chuck plate 1, and rectilinear orbit 7 evaginations are in the upper surface of base 3.

Claims (1)

1. the auxiliary mounting structure of turbine locking, it comprises chuck plate, be provided with the bayonet socket that the shape and size with turbine head are complementary at described chuck plate, described chuck plate bottom supporting is in the upper surface of base, it is characterized in that: the cylinder block of cylinder is installed on the upper surface cross track of described base, the bottom surface of the fastening described rest pad of cylinder arm of described cylinder, described cylinder moves in vertical direction, the turbine head of turbine to be locked is installed in the corresponding described bayonet socket, the middle part axle head of turbine described to be locked is supported on described rest pad, the locking end for the treatment of of turbine described to be locked exposes to described rest pad, the bottom of described chuck plate is installed in vertical rectilinear orbit of described base, described vertical rectilinear orbit is perpendicular to the facade of described chuck plate, and described rectilinear orbit evagination is in the upper surface of described base.
CN 201220615859 2012-11-20 2012-11-20 Auxiliary installation structure for turbine locking Expired - Fee Related CN202895072U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220615859 CN202895072U (en) 2012-11-20 2012-11-20 Auxiliary installation structure for turbine locking

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220615859 CN202895072U (en) 2012-11-20 2012-11-20 Auxiliary installation structure for turbine locking

Publications (1)

Publication Number Publication Date
CN202895072U true CN202895072U (en) 2013-04-24

Family

ID=48115787

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220615859 Expired - Fee Related CN202895072U (en) 2012-11-20 2012-11-20 Auxiliary installation structure for turbine locking

Country Status (1)

Country Link
CN (1) CN202895072U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20130424

Termination date: 20131120