CN214560232U - Fan cabin processing tool - Google Patents

Fan cabin processing tool Download PDF

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Publication number
CN214560232U
CN214560232U CN202120330765.7U CN202120330765U CN214560232U CN 214560232 U CN214560232 U CN 214560232U CN 202120330765 U CN202120330765 U CN 202120330765U CN 214560232 U CN214560232 U CN 214560232U
Authority
CN
China
Prior art keywords
hole
panel
cabin
bolt
bottom plate
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
CN202120330765.7U
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Chinese (zh)
Inventor
陈中亚
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.)
Ningbo Changfeng Wind Energy Technology Co ltd
Original Assignee
Ningbo Changfeng Wind Energy 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 Ningbo Changfeng Wind Energy Technology Co ltd filed Critical Ningbo Changfeng Wind Energy Technology Co ltd
Priority to CN202120330765.7U priority Critical patent/CN214560232U/en
Application granted granted Critical
Publication of CN214560232U publication Critical patent/CN214560232U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The invention discloses a fan cabin machining tool which comprises a bottom plate and a panel, wherein the bottom plate and the panel form a certain angle, the bottom plate and the panel are connected through a connecting plate, the bottom surface of a cabin is arranged on the panel, a circle of second through holes are formed in the periphery of the bottom surface of the cabin, at least three limiting columns are arranged on the top surface of the panel, each limiting column is in contact with the inner ring of the bottom surface of the cabin, a first through hole is formed in the panel, and a bolt penetrates through the first through hole and the second through hole and then is connected with a nut. According to the principle that a circle is determined by three points, the position of the engine room can be determined by using three positioning columns, and then a bolt penetrates through the first through hole and the second through hole and is connected with the nut, so that the three positioning columns are always in contact with the inner ring of the bottom surface. Therefore, the positioning of the cabin can be completed, and compared with the prior method that at least three bolts are screwed, the process is greatly simplified.

Description

Fan cabin processing tool
Technical Field
The invention relates to processing equipment of a wind driven generator, in particular to a processing tool of a fan engine room.
Background
As shown in fig. 1, in a blower nacelle 1, a bottom surface 1a and a machined surface 1b of the nacelle 1 have a certain angle difference, and are positioned by the bottom surface when in use. The original mode is that a circle of first through holes are processed on the top surface of the tool, the first through holes are arranged opposite to second through holes on the bottom surface of the engine room, then bolts penetrate through the first through holes and then penetrate out of the second through holes, and then the first through holes are connected with the bolts. In this way, in order to fix the position of the nacelle, it is generally necessary to screw at least 4 bolts, which is troublesome, and therefore, improvement is necessary.
Disclosure of Invention
Aiming at the defects in the prior art, the invention provides the fan engine room machining tool, and the positioning of the engine room can be completed only by screwing one bolt.
The invention is realized by the following technical scheme: the utility model provides a fan cabin processing frock, includes bottom plate and panel, bottom plate and panel are certain angle, bottom plate and panel pass through the connecting plate and link to each other, and the bottom surface setting in cabin is in on the panel, the bottom surface border in cabin is provided with round second through-hole, be provided with at least three spacing post on the top surface of panel, every spacing post with the bottom surface inner circle in cabin contacts, be provided with a first through-hole on the panel, the bolt passes first through-hole with link to each other with the nut behind the second through-hole. According to the principle that a circle is determined by three points, the position of the engine room can be determined by using three positioning columns, and then a bolt penetrates through the first through hole and the second through hole and is connected with the nut, so that the three positioning columns are always in contact with the inner ring of the bottom surface. Therefore, the positioning of the cabin can be completed, and compared with the prior method that at least three bolts are screwed, the process is greatly simplified.
In the above technical solution, preferably, there are three limiting posts, three of the limiting posts and the bottom surface contact point are located in the same semicircle, and the second through hole communicated with the first through hole is located in the other semicircle. The bolt can be tensioned, and the limit column is ensured to be in close contact with the inner ring of the bottom surface.
In the above technical solution, preferably, the arc lengths between the adjacent limiting columns are the same, and the limiting column located in the middle is arranged opposite to the first through hole with respect to the center of the bottom surface.
In the above technical solution, preferably, the bolt includes a bolt head with magnetism and a bolt column without magnetism, and the bolt is magnetically attracted to the bottom of the panel. Set up like this, the bolt need not all be taken off from the frock, has removed the trouble of workman's installation bolt every time from. Once the bolt is not fixed on the panel, if the first through hole and the second through hole are not aligned, the bolt can be pressed down, and the bolt cannot be clamped. Secondly, if first through-hole and second through-hole have aimed at, also prevent that the bolt post from adsorbing on the second through-hole inner wall, let the second through-hole can't be worn out to the bolt post, lead to the nut to connect the difficulty.
Compared with the prior art, the invention has the beneficial effects that: when the blade is installed at the end part of the fan blade, the protrusion is inserted into the hole at the end part of the blade matched with the protrusion, at this time, the axis of the protrusion is coaxial with the axis of the end part of the blade, and the protrusion is coaxial with the variable pitch disc body, so that the variable pitch disc and the blade can be ensured to be coaxial. Then we rotate certain angle again, until the through-hole that the annular circled is relative with the screw of blade tip, reuse the bolt locking, just so accomplished and become the whole process of oar dish installation on the fan blade, compare with original mounting means, we can ensure to become the oar dish and be in same axis with the fan blade after the installation, let the fan blade more stable when the rotation.
Drawings
FIG. 1 is a schematic view of a nacelle.
Fig. 2 is a schematic diagram of the present invention.
Fig. 3 is a schematic view of the present invention in cooperation with a nacelle.
FIG. 4 is a schematic view of the junction of a first via and a second via.
Detailed Description
The invention is described in further detail below with reference to the following detailed description and accompanying drawings:
referring to fig. 2 and 4, the machining tool for the fan engine room comprises a bottom plate 2 and a panel 3, wherein the bottom plate 2 and the panel 3 form a certain angle, the bottom plate 2 and the panel 3 are connected through a connecting plate 4, the bottom surface 1a of the engine room 1 is arranged on the panel 3, a circle of second through holes 11 are formed in the periphery of the bottom surface 1a of the engine room 1, and three limiting columns 5 are arranged on the top surface of the panel 3. Each limiting column is in contact with the inner ring of the bottom surface of the engine room, three contact points of the limiting columns 5 and the bottom surface 1a are located in the same semicircle, the arc lengths between the adjacent limiting columns 5 are the same, and the limiting column located in the middle and the first through hole are arranged opposite to the circle center of the bottom surface.
The panel 3 is provided with a first through hole 31, and the bolt 6 passes through the first through hole 31 and the second through hole 11 and then is connected with the nut 7. The second through hole 11 communicating with the first through hole 31 is located in the other semicircle. The bolt can be tensioned, and the limit column is ensured to be in close contact with the inner ring of the bottom surface.
According to the principle that a circle is determined by three points, the position of the engine room can be determined by using three positioning columns, and then a bolt penetrates through the first through hole and the second through hole and is connected with the nut, so that the three positioning columns are always in contact with the inner ring of the bottom surface. Therefore, the positioning of the cabin can be completed, and compared with the prior method that at least three bolts are screwed, the process is greatly simplified.
The bolt 6 comprises a magnetic bolt 61 head and a non-magnetic bolt column 62, and the bolt 6 is magnetically attracted to the bottom of the panel 3. Set up like this, the bolt need not all be taken off from the frock, has removed the trouble of workman's installation bolt every time from. Once the bolt is not fixed on the panel, if the first through hole and the second through hole are not aligned, the bolt can be pressed down, and the bolt cannot be clamped. Secondly, if first through-hole and second through-hole have aimed at, also prevent that the bolt post from adsorbing on the second through-hole inner wall, let the second through-hole can't be worn out to the bolt post, lead to the nut to connect the difficulty.

Claims (4)

1. The utility model provides a fan cabin processing frock, includes bottom plate and panel, bottom plate and panel are certain angle, bottom plate and panel pass through the connecting plate and link to each other, and the bottom surface setting in cabin is in on the panel, the bottom surface border in cabin is provided with round second through-hole, its characterized in that: the top surface of the panel is provided with at least three limiting columns, each limiting column is in contact with the inner ring of the bottom surface of the engine room, the panel is provided with a first through hole, and a bolt penetrates through the first through hole and the second through hole and then is connected with a nut.
2. The fan nacelle machining tool according to claim 1, wherein: the number of the limiting columns is three, the three limiting columns and the bottom surface contact point are positioned in the same semicircle, and the second through hole communicated with the first through hole is positioned in the other semicircle.
3. The fan nacelle machining tool according to claim 2, wherein: the arc length between the adjacent limiting columns is the same, and the limiting column positioned in the middle and the first through hole are arranged opposite to each other relative to the circle center of the bottom surface.
4. The fan nacelle machining tool according to claim 1, wherein: the bolt comprises a magnetic bolt head and a non-magnetic bolt column, and is magnetically attracted to the bottom of the panel.
CN202120330765.7U 2021-02-05 2021-02-05 Fan cabin processing tool Expired - Fee Related CN214560232U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120330765.7U CN214560232U (en) 2021-02-05 2021-02-05 Fan cabin processing tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120330765.7U CN214560232U (en) 2021-02-05 2021-02-05 Fan cabin processing tool

Publications (1)

Publication Number Publication Date
CN214560232U true CN214560232U (en) 2021-11-02

Family

ID=78315752

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120330765.7U Expired - Fee Related CN214560232U (en) 2021-02-05 2021-02-05 Fan cabin processing tool

Country Status (1)

Country Link
CN (1) CN214560232U (en)

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20211102