CN109176395A - A kind of Airbus Aircraft floor screw takes out tool - Google Patents
A kind of Airbus Aircraft floor screw takes out tool Download PDFInfo
- Publication number
- CN109176395A CN109176395A CN201811208992.1A CN201811208992A CN109176395A CN 109176395 A CN109176395 A CN 109176395A CN 201811208992 A CN201811208992 A CN 201811208992A CN 109176395 A CN109176395 A CN 109176395A
- Authority
- CN
- China
- Prior art keywords
- groove
- gripping block
- screw
- handle
- takes out
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B27/00—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for
- B25B27/02—Hand tools, specially adapted for fitting together or separating parts or objects whether or not involving some deformation, not otherwise provided for for connecting objects by press fit or detaching same
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Jigs For Machine Tools (AREA)
Abstract
The invention discloses a kind of Airbus Aircraft floor screws to take out tool, it is related to machine tool technical field, including clamping device, the clamping device includes control mechanism and clamp system, the inside of the control mechanism offers the first groove and the second groove, the inside of first groove is plugged with the first rotary shaft, the internal activity of second groove is equipped with the second rotary shaft, the clamp system includes the first gripping block and the second gripping block, the bottom of first gripping block is fixedly connected with the top side of control mechanism, the bottom of second gripping block and the top of the second rotary shaft are rotatablely connected.The Airbus Aircraft floor screw takes out tool, by holding rod, fixed being equipped with body, through-hole and tilted block, the power being lifted up can be generated to screw and then removed after gripping means grips screw, working strength is greatly reduced, the extraction efficiency of screw is improved.
Description
Technical field
The present invention relates to machine tool technical field, specially a kind of Airbus Aircraft floor screw takes out tool.
Background technique
Air Passenger series cargo aircraft needs to remove when large-scale C is examined the floor in full cabin, and screw total amount is very big, and maintenance personal is removing
After screw, need to pull out on screw, it is direct using hand since resilient cushion and screw hole and the screw rod fitting of floor bottoms are close
Extraction screw is relatively elaborate, and the required working time is longer.
A kind of Airbus Aircraft floor spiral shell disclosed in 205394443 U of Chinese invention patent application prospectus CN
Silk taking-up tool, which takes out tool, although shortening the working time, reduces maintenance personal and extracts spiral shell
The working strength of silk, still, it is that screw is prized by ripping bar when taking out screw which, which takes out tool,
Out, since screw has screw thread and obtains with floor clamping very tight, still there is certain difficulty when pulling out.
Currently, existing for taking out the taking-up tool of Airbus Aircraft floor screw, inconvenient for use, being unfavorable for promoting makes
With.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides a kind of Airbus Aircraft floor screws to take out tool, solves existing
For taking out the taking-up tool of Airbus Aircraft floor screw, the low efficiency of screw is taken out, the screw of different size cannot be taken out, answered
With the small problem of range.
(2) technical solution
In order to achieve the above object, the present invention is achieved by the following technical programs: a kind of Airbus Aircraft floor screw takes out work
Tool, including clamping device, the clamping device include control mechanism and clamp system, and the inside of the control mechanism offers the
One groove and the second groove, the inside of first groove are plugged with the first rotary shaft, the internal activity peace of second groove
Equipped with the second rotary shaft；
The clamp system includes the first gripping block and the second gripping block, the bottom of first gripping block and the top of control mechanism
End side is fixedly connected, and the bottom of second gripping block and the top of the second rotary shaft are rotatablely connected, first gripping block
Tilted block is fixedly connected to one end of the second gripping block, in the middle part of the other end of first gripping block and the second gripping block
Third groove is offered, the inside of the third groove is fixedly installed with fixed link；
The top of the clamping device is equipped with handle, and the bottom end of the handle, which is hinged with, to be fixed body, and the fixation is the upper of body
Through-hole is offered in the middle part of the section of end, one end of the fixed link is fixedly connected with the side cell wall of third groove, the fixed link
The other end is fixedly connected through through-hole and with the other side cell wall of third groove.
Optionally, the opening of first groove is located at the one end of control mechanism far from the first gripping block, and described second is recessed
Slot position is in the center bottom of the first groove.
Optionally, the upper surface of the tilted block is scarf, and the scarf of two tilted blocks is opposite.
Optionally, the fixation is two the quantity of body and handle, and two fixations are symmetrical body, and two
The handle is symmetrical.
Optionally, the handle is that inclined L shape handle, the outer surface of the handle are equipped with screw thread texture outward.
Optionally, the fixation is inclined L body body, and the fixation inwardly tilts body.
(3) beneficial effect
The present invention provides a kind of Airbus Aircraft floor screw take out tool, have it is following the utility model has the advantages that
(1), the Airbus Aircraft floor screw takes out tool, and the cooperation of body, through-hole and tilted block is set by holding rod, fixation
It sets, the power being lifted up can be generated to screw and then removed, it is strong to greatly reduce work after gripping means grips screw
Degree, improves the extraction efficiency of screw.
(2), the Airbus Aircraft floor screw takes out tool, by the way that clamping device is arranged, can be adjusted by control mechanism
Clamp system is saved, different size of screw can be clamped and then is removed, working range is wide.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention；
Fig. 2 is the top view of clamping device of the present invention；
Fig. 3 is the top cross-sectional view of control mechanism of the present invention；
Fig. 4 is the sectional view of the second gripping block of the invention；
Fig. 5 is holding rod and the fixed structural schematic diagram body.
In figure: 1 clamping device, 2 control mechanisms, 3 clamp systems, 301 first gripping blocks, 302 second gripping blocks, 4 first
Groove, 5 second grooves, 6 first rotary shafts, 7 second rotary shafts, 8 tilted blocks, 9 third grooves, 10 fixed links, 11 handles, 12 are consolidated
Determine body, 13 through-holes.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
In the description of the present invention, it is to be understood that, term " on ", "lower", "vertical", "horizontal", "top", "bottom"
The orientation or positional relationship of the instructions such as "inner", "outside", " clockwise ", " counterclockwise " is that orientation based on the figure or position are closed
System, is merely for convenience of description of the present invention and simplification of the description, rather than the device or element of indication or suggestion meaning must have
Specific orientation is constructed and operated in a specific orientation, therefore is not considered as limiting the invention.
In the present invention unless specifically defined or limited otherwise, term " setting ", " installation ", " connected ", " connection ",
Terms such as " fixations " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection；It can be mechanical connect
It connects；It can be directly connected, it can also be indirectly connected through an intermediary.For the ordinary skill in the art, may be used
To understand the concrete meaning of above-mentioned term in the present invention as the case may be.
In addition, term " first ", " second " etc. are used for description purposes only, it is not understood to indicate or imply relatively important
Property or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Person implicitly includes one or more of the features.
Please refer to Fig. 1-5, the present invention provides a kind of technical solution: a kind of Airbus Aircraft floor screw takes out tool, including
Clamping device 1, clamping device 1 include control mechanism 2 and clamp system 3, and the inside of control mechanism 2 offers 4 He of the first groove
Second groove 5, the inside of the first groove 4 are plugged with the first rotary shaft 6, and the internal activity of the second groove 5 is equipped with the second rotation
Axis 7 rotates the second rotary shaft 7, drives the rotation of the first rotary shaft 6, controls the movement of the second gripping block 302；
Clamp system 3 includes the first gripping block 301 and the second gripping block 302, bottom and the control mechanism 2 of the first gripping block 301
Top side be fixedly connected, the top of the bottom of the second gripping block 302 and the second rotary shaft 7 is rotatablely connected, the first gripping block
301 and second one end of gripping block 302 be fixedly connected to tilted block 8, the first gripping block 301 and the second gripping block 302 it is another
Third groove 9 is offered in the middle part of one end, the inside of third groove 9 is fixedly installed with fixed link 10, and the second gripping block 302 is mobile
To the position for capableing of clamping screw, tilted block 8 is cut between screw and bottom plate, is then slightly reverse and turns the second rotary shaft 7,
The first gripping block 301 and the second gripping block 302 is set to be clamped fixation to screw；
The top of clamping device 1 is equipped with handle 11, and the bottom end of handle 11 is hinged with fixed body 12, the fixed upper end section body 12
Middle part offers through-hole 13, and one end of fixed link 10 is fixedly connected with the side cell wall of third groove 9, the other end of fixed link 10
It is fixedly connected through through-hole 13 and with the other side cell wall of third groove 9, after being clamped to screw, holds handle 11, handle
11 lower end will drive fixation and body 12 moved up, so that the extraction of screw be made to be easier.
As a preferred technical solution of the present invention: the opening of the first groove 4 is located at control mechanism 2 and clamps far from first
One end of block 301, the second groove 5 are located at the center bottom of the first groove 4, can make 7 band of the second rotary shaft in the second groove 5
The first rotary shaft 6 in dynamic first groove 4 moves horizontally.
As a preferred technical solution of the present invention: the upper surface of tilted block 8 is scarf, two tilted blocks 8 it is oblique
Section is opposite, is conducive to cut between screw and floor, blocks the neck of screw, make it easier to extract.
As a preferred technical solution of the present invention: fixing the quantity of body 12 and handle 11 is two, and two solid
Fixed that body 12 is symmetrical, symmetrically, the power for making extraction screw more evenly, is conducive to take out screw two handles 11.
As a preferred technical solution of the present invention: handle 11 is inclined L shape handle outward, the appearance of handle 11
Face is equipped with screw thread texture, is in one's hands when holding 11, prevents rubber sleeve.
As a preferred technical solution of the present invention: fixing body 12 is inclined L body, and fixed that body 12 is inside
It rolls tiltedly, when 11 pairs of fixations of handle are 12 applied force of body, can guarantee the fixed normal work body 12, screw is lifted upwards
It rises.
In conclusion the Airbus Aircraft floor screw takes out tool, in use, user first rotates the second rotary shaft 7, band
Dynamic first rotary shaft 6 rotation, so that the second gripping block 302 of control moves horizontally, being moved into can be with the first gripping block
301 cooperate and the position of clamping screw, and tilted block 8 is cut between screw and floor, is then slightly reverse and turns the second rotation
Axis 7 makes the first gripping block 301 and the second gripping block 302 be clamped fixation to screw, after being clamped to screw, holds and hold
11 upper end, when drawing close, the lower end of handle 11 can be lifted up two handles 11, can be to fixed generating on body 12
One upward power moves up fixation the upper end of body 12, fixes since fixed link 10 runs through the through-hole 13 on body 12,
Fixed body 12 is moved up will drive the first gripping block 301 and the second gripping block 302 moves up, thus to screw generation one
A power being lifted up reduces the working strength that worker extracts screw, handle 11 can also be rotated while holding handle 11,
It is more advantageous to the taking-up of screw in this way.
It should be noted that in the present invention unless specifically defined or limited otherwise, fisrt feature is in second feature
It can be that the first and second features directly contact or the first and second features are by intermediary mediate contact "up" or "down".
Moreover, fisrt feature can be above the second feature " above ", " above " and " above " fisrt feature right above second feature or tiltedly
Top, or first feature horizontal height is merely representative of higher than second feature.Fisrt feature second feature " under ", " lower section " and
" following " can be fisrt feature and be directly under or diagonally below the second feature, or be merely representative of first feature horizontal height less than
Two features.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
Anyone skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (6)
1. a kind of Airbus Aircraft floor screw takes out tool, including clamping device (1), it is characterised in that: the clamping device (1)
Including control mechanism (2) and clamp system (3), the inside of the control mechanism (2) offers the first groove (4) and the second groove
(5), the inside of first groove (4) is plugged with the first rotary shaft (6), and the internal activity of second groove (5) is equipped with
Second rotary shaft (7)；
The clamp system (3) includes the first gripping block (301) and the second gripping block (302), first gripping block (301)
Bottom is fixedly connected with the top side of control mechanism (2), the bottom and the second rotary shaft (7) of second gripping block (302)
Top rotation connection, one end of first gripping block (301) and the second gripping block (302) is fixedly connected to tilted block
(8), it is offered third groove (9) in the middle part of the other end of first gripping block (301) and the second gripping block (302), it is described
The inside of third groove (9) is fixedly installed with fixed link (10)；
The top of the clamping device (1) is equipped with handle (11), and the bottom end of the handle (11) is hinged with fixed body (12), institute
It states and is offered through-hole (13) in the middle part of the fixed upper end section body (12), one end and third groove (9) of the fixed link (10)
Side cell wall is fixedly connected, and the other end of the fixed link (10) runs through through-hole (13) and another side channel with third groove (9)
Wall is fixedly connected.
2. a kind of Airbus Aircraft floor screw according to claim 1 takes out tool, it is characterised in that: first groove
(4) opening is located at the one end of control mechanism (2) far from the first gripping block (301), and second groove (5) is located at the first groove
(4) center bottom.
3. a kind of Airbus Aircraft floor screw according to claim 1 takes out tool, it is characterised in that: the tilted block
(8) upper surface is scarf, and the scarf of two tilted blocks (8) is opposite.
4. a kind of Airbus Aircraft floor screw according to claim 1 takes out tool, it is characterised in that: the fixation is body
(12) and the quantity of handle (11) is two, two fixations body (12) symmetrically, two handle (11) phases
It is mutually symmetrical.
5. a kind of Airbus Aircraft floor screw according to claim 1 takes out tool, it is characterised in that: the handle (11)
Outer surface for inclined L shape handle outward, the handle (11) is equipped with screw thread texture.
6. a kind of Airbus Aircraft floor screw according to claim 1 takes out tool, it is characterised in that: the fixation is body
It (12) is inclined L body, and the fixation inwardly tilts body (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811208992.1A CN109176395A (en) | 2018-10-17 | 2018-10-17 | A kind of Airbus Aircraft floor screw takes out tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811208992.1A CN109176395A (en) | 2018-10-17 | 2018-10-17 | A kind of Airbus Aircraft floor screw takes out tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109176395A true CN109176395A (en) | 2019-01-11 |
Family
ID=64945724
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811208992.1A Withdrawn CN109176395A (en) | 2018-10-17 | 2018-10-17 | A kind of Airbus Aircraft floor screw takes out tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109176395A (en) |
-
2018
- 2018-10-17 CN CN201811208992.1A patent/CN109176395A/en not_active Withdrawn
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190111 |