CN103831756A - Installation auxiliary locking structure for turbines - Google Patents

Installation auxiliary locking structure for turbines Download PDF

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Publication number
CN103831756A
CN103831756A CN201210471146.5A CN201210471146A CN103831756A CN 103831756 A CN103831756 A CN 103831756A CN 201210471146 A CN201210471146 A CN 201210471146A CN 103831756 A CN103831756 A CN 103831756A
Authority
CN
China
Prior art keywords
cylinder
locked
turbine
air cylinder
turbines
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.)
Pending
Application number
CN201210471146.5A
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Chinese (zh)
Inventor
夏远富
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.)
Vanguard Wuxi Science and Technology Co Ltd
Original Assignee
Vanguard Wuxi Science and Technology 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 Vanguard Wuxi Science and Technology Co Ltd filed Critical Vanguard Wuxi Science and Technology Co Ltd
Priority to CN201210471146.5A priority Critical patent/CN103831756A/en
Publication of CN103831756A publication Critical patent/CN103831756A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B25HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
    • B25BTOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
    • B25B11/00Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
    • B25B11/02Assembly jigs

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Machine Tool Units (AREA)

Abstract

The invention provides an installation auxiliary locking structure for turbines. According to the installation auxiliary locking structure, a head clamping board can not be moved in the locking process and the locking quality is guaranteed. The installation auxiliary locking structure for the turbines comprises the head clamping board. Clamping openings matched with turbine heads in shape and size are formed in the head clamping board. The installation auxiliary locking structure for the turbines further comprises a supporting board, an air cylinder base of an air cylinder is tightly fixed to the upper surface of a base, the bottom face of the supporting board is fastened by an air cylinder arm of the air cylinder, the air cylinder moves perpendicularly, the turbine heads of the turbines to be locked are clamped to the corresponding clamping openings, the middle shaft end of each turbine to be locked is supported by the supporting board, the end to be locked of each turbine to be locked is exposed out of the supporting board, a sliding block is arranged at the bottom of the head clamping board and embedded in a linear rail of the base, and the linear rail is perpendicular to the vertical face of the head clamping board. The installation auxiliary locking structure for the turbines is characterized in that the side, far away from the supporting board, of the head clamping board is connected with the air cylinder arm of the horizontal driving air cylinder in a tightly fixed mode.

Description

The installation auxiliary lock locking structure of turbine
Technical field
The present invention relates to booster turbine components fixing device, be specially the installation auxiliary lock locking structure of turbine.
Background technology
In the installation process of booster turbine, for locking nut, must fix turbine head, shape due to turbine head when installation is different, adopt a kind of custom-designed chuck plate on the ground horizontal fix, the bayonet socket that has the multiple turbine head shape and size such as circle, triangle, hexagon on chuck plate, like this for different turbine heads, does not need replacing instrument.But practical operation is sometimes not too convenient, this just need to adopt turbine exemplar horizontal installation, for this reason, we have designed base, support, support, chuck plate are installed on to base side by side, on support, be provided with the brace table corresponding with bayonet socket, to solve horizontally-mounted problem, but the problem that this structure exists is that turbine exemplar needs one end of locking nut to ride over the brace table on support, between the base slider of existing chuck plate and guide rail, there is no locking mechanism, cause, in locking process, can producing displacement, thereby have influence on the quality of locking.
Summary of the invention
For above-mentioned situation, the invention provides the installation auxiliary lock locking structure of turbine, it can not move chuck plate in locking process, guarantees to lock quality.
The installation auxiliary lock locking structure of turbine, its technical scheme is such, it comprises chuck plate, on described chuck plate, be provided with the bayonet socket matching with the shape and size of turbine head, it also comprises support plate, the cylinder block of cylinder is anchored on the upper surface of described base, the bottom surface of the fastening described support plate of cylinder arm of described cylinder, described cylinder moves in vertical direction, the turbine head of worm gear to be locked is installed in corresponding described bayonet socket, the middle part axle head of worm gear described to be locked is supported on described support plate, the locking end for the treatment of of worm gear described to be locked exposes to described support plate, the bottom of described chuck plate is provided with slide block, described slide block is flush-mounted in the rectilinear orbit of described base, described rectilinear orbit is perpendicular to the facade of described chuck plate, it is characterized in that: described chuck plate be fastenedly connected the cylinder arm of horizontal drive cylinder away from a side of described support plate, the cylinder block of described horizontal drive cylinder is anchored on the upper surface of described base.
The present invention adopts after said structure, the turbine head of worm gear to be locked is installed in corresponding bayonet socket, the middle part axle head of worm gear to be locked is supported on support plate, the locking end for the treatment of of worm gear to be locked exposes to described support plate, cylinder up-down adjustment makes support plate can adapt to the worm gear to be locked of the position of differing heights, and chuck plate can be along the distance between rectilinear orbit adjustment and support plate by base slider, no matter the axial length of worm gear to be locked is short, all can be suitable for this structure, due to the movement of horizontal drive air cylinder driven chuck plate, it moves to after ad-hoc location, horizontal drive cylinder is fixed the position of chuck plate, it can not move chuck plate in locking process, guarantee to lock quality.
Accompanying drawing explanation
Fig. 1 is main TV structure schematic diagram of the present invention;
Fig. 2 is the left view structural representation of Fig. 1;
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, on chuck plate 1, be provided with the bayonet socket 2 matching with the shape and size of turbine head, it also comprises support plate 3, the cylinder block 4 of cylinder is anchored on the upper surface of base 5, the bottom surface of the fastening support plate 3 of cylinder arm 6 of cylinder, cylinder moves in vertical direction, worm gear to be locked is (not shown in FIG., belong to existing mature structure) turbine head be installed in corresponding bayonet socket 2, the middle part axle head of worm gear to be locked is supported on support plate 3, the locking end for the treatment of of worm gear to be locked exposes to support plate 3, the bottom of chuck plate 1 is provided with slide block 7, slide block 7 is flush-mounted in the rectilinear orbit 8 of base 5, rectilinear orbit 8 is perpendicular to the facade of chuck plate 1, chuck plate 1 be fastenedly connected the cylinder arm of horizontal drive cylinder 9 away from a side of described support plate 3, the cylinder block of horizontal drive cylinder 9 is anchored on the upper surface of base 5.

Claims (1)

1. the installation auxiliary lock locking structure of turbine, it comprises chuck plate, on described chuck plate, be provided with the bayonet socket matching with the shape and size of turbine head, it also comprises support plate, the cylinder block of cylinder is anchored on the upper surface of described base, the bottom surface of the fastening described support plate of cylinder arm of described cylinder, described cylinder moves in vertical direction, the turbine head of worm gear to be locked is installed in corresponding described bayonet socket, the middle part axle head of worm gear described to be locked is supported on described support plate, the locking end for the treatment of of worm gear described to be locked exposes to described support plate, the bottom of described chuck plate is provided with slide block, described slide block is flush-mounted in the rectilinear orbit of described base, described rectilinear orbit is perpendicular to the facade of described chuck plate, it is characterized in that: described chuck plate be fastenedly connected the cylinder arm of horizontal drive cylinder away from a side of described support plate, the cylinder block of described horizontal drive cylinder is anchored on the upper surface of described base.
CN201210471146.5A 2012-11-20 2012-11-20 Installation auxiliary locking structure for turbines Pending CN103831756A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210471146.5A CN103831756A (en) 2012-11-20 2012-11-20 Installation auxiliary locking structure for turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210471146.5A CN103831756A (en) 2012-11-20 2012-11-20 Installation auxiliary locking structure for turbines

Publications (1)

Publication Number Publication Date
CN103831756A true CN103831756A (en) 2014-06-04

Family

ID=50795817

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210471146.5A Pending CN103831756A (en) 2012-11-20 2012-11-20 Installation auxiliary locking structure for turbines

Country Status (1)

Country Link
CN (1) CN103831756A (en)

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C06 Publication
PB01 Publication
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20140604