CN209319674U - 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
- CN209319674U CN209319674U CN201821682301.7U CN201821682301U CN209319674U CN 209319674 U CN209319674 U CN 209319674U CN 201821682301 U CN201821682301 U CN 201821682301U CN 209319674 U CN209319674 U CN 209319674U
- 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.)
- Expired - Fee Related
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Abstract
The utility model 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 utility model 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 disclosed in 205394443 U of Chinese utility model patent ublic specification of application CN
Plate screw takes out tool, which takes out tool and reduce maintenance personal although shortening the working time and pull out
The working strength of screw out, still, it is by ripping bar spiral shell when taking out screw which, which takes out tool,
Silk pulls out, and since screw has screw thread and obtains with floor clamping very tight, still has 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.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of Airbus Aircraft floor screw and takes out tool, solves
It is existing for taking out the taking-up tool of Airbus Aircraft floor screw, take out the low efficiency of screw, different size cannot be taken out
Screw, the small problem of application range.
(2) technical solution
In order to achieve the above object, the utility model is achieved by the following technical programs: a kind of Airbus Aircraft floor spiral shell
Silk taking-up tool, including clamping device, the clamping device include control mechanism and clamp system, the inside of the control mechanism
Offer the first groove and the second groove, the inside of first groove is plugged with the first rotary shaft, second groove it is interior
Portion is movably installed 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 control mechanism
Top side be fixedly connected, the top of the bottom of second gripping block and the second rotary shaft is rotatablely connected, first folder
One end of tight block and the second gripping block is fixedly connected to tilted block, in the other end of first gripping block and the second gripping block
Portion offers third groove, and 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 body
Upper end section in the middle part of offer through-hole, one end of the fixed link is fixedly connected with the side cell wall of third groove, the fixation
The other end of bar 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 utility model provide 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, passes through holding rod, the fixed cooperation body, through-hole and tilted block
Setting can generate the power being lifted up to screw and then remove, 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 a schematic structural view of the utility model;
Fig. 2 is the top view of the utility model clamping device;
Fig. 3 is the top cross-sectional view of the utility model control mechanism;
Fig. 4 is the sectional view of the second gripping block of the utility model;
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
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
In the description of the present invention, it should be understood that term " on ", "lower", "vertical", "horizontal", "top",
The orientation or positional relationship of the instructions such as "bottom" "inner", "outside", " clockwise ", " counterclockwise " is orientation based on the figure or position
Relationship is set, is merely for convenience of describing the present invention and simplifying the description, rather than the device or element of indication or suggestion meaning
It must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.
In the present invention unless specifically defined or limited otherwise, term " setting ", " connected ", " connects " installation "
Connect ", the terms such as " fixation " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection;It can be machine
Tool connection;It can be directly connected, it can also be indirectly connected through an intermediary.For those of ordinary skill in the art and
Speech, can 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 utility model provides a kind of technical solution: a kind of Airbus Aircraft floor screw takes out tool,
Including clamping device 1, clamping device 1 includes control mechanism 2 and clamp system 3, and the inside of control mechanism 2 offers the first groove
4 and second groove 5, the inside of the first groove 4 be plugged with the first rotary shaft 6, the internal activity of the second groove 5 is equipped with the second rotation
Shaft 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 machine of the first gripping block 301
The top side of structure 2 is fixedly connected, and the top of the bottom of the second gripping block 302 and the second rotary shaft 7 is rotatablely connected, and first clamps
One end of block 301 and the second gripping block 302 is fixedly connected to tilted block 8, the first gripping block 301 and the second gripping block 302
Third groove 9 is offered in the middle part of the other end, the inside of third groove 9 is fixedly installed with fixed link 10, and the second gripping block 302 is moved
The position for capableing of clamping screw is moved, tilted block 8 is cut between screw and bottom plate, is then slightly reverse and turns the second rotary shaft
7, so that the first gripping block 301 and the second gripping block 302 is clamped fixation to screw;
The top of clamping device 1 is equipped with handle 11, and the bottom end of handle 11, which is hinged with, to be fixed body 12, fixed the upper of body 12
End section in the middle part of offer through-hole 13, one end of fixed link 10 is fixedly connected with the side cell wall of third groove 9, fixed link 10 it is another
One end 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,
The lower end of handle 11 will drive fixation and body 12 moved up, so that the extraction of screw be made to be easier.
A kind of optimal technical scheme as the utility model: the opening of the first groove 4 is located at control mechanism 2 far from first
One end of gripping block 301, the second groove 5 are located at the center bottom of the first groove 4, and second in the second groove 5 can be made to rotate
Axis 7 drives the first rotary shaft 6 in the first groove 4 to move horizontally.
A kind of optimal technical scheme as the utility model: the upper surface of tilted block 8 is scarf, two tilted blocks 8
Scarf it is opposite, be conducive to cut between screw and floor, block the neck of screw, make it easier to extract.
A kind of optimal technical scheme as the utility model: fixed the quantity of body 12 and handle 11 is two, and two
A fixed that body 12 is symmetrical, symmetrically, the power for making extraction screw more evenly, is conducive to take out screw two handles 11.
A kind of optimal technical scheme as the utility model: handle 11 is inclined L shape handle outward, handle 11
Outer surface is equipped with screw thread texture, is in one's hands when holding 11, prevents rubber sleeve.
A kind of optimal technical scheme as the utility model: fixing body 12 is inclined L body, and fixed body 12
Tilt inwardly, when 11 pairs of fixations of handle are 12 applied force of body, can guarantee the fixed normal work body 12, screw to
On lift.
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 the second spy
It can be that the first and second features directly contact or the first and second features are connect indirectly by intermediary "above" or "below" sign
Touching.Moreover, fisrt feature can be above the second feature " above ", " above " and " above " fisrt feature right above second feature or
Oblique upper, or first feature horizontal height is merely representative of higher than second feature.Fisrt feature second feature " under ", " lower section "
" following " can be fisrt feature and be directly under or diagonally below the second feature, or is merely representative of first feature horizontal height and is less than
Second feature.
The preferable specific embodiment of the above, only the utility model, but the protection scope of the utility model is not
It is confined to this, anyone skilled in the art is within the technical scope disclosed by the utility model, practical according to this
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
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 |
---|---|---|---|
CN201821682301.7U CN209319674U (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 |
---|---|---|---|
CN201821682301.7U CN209319674U (en) | 2018-10-17 | 2018-10-17 | A kind of Airbus Aircraft floor screw takes out tool |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209319674U true CN209319674U (en) | 2019-08-30 |
Family
ID=67708096
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201821682301.7U Expired - Fee Related CN209319674U (en) | 2018-10-17 | 2018-10-17 | A kind of Airbus Aircraft floor screw takes out tool |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN209319674U (en) |
-
2018
- 2018-10-17 CN CN201821682301.7U patent/CN209319674U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190830 Termination date: 20201017 |
|
CF01 | Termination of patent right due to non-payment of annual fee |