CN208819824U - A kind of aircraft fuse seat - Google Patents
A kind of aircraft fuse seat Download PDFInfo
- Publication number
- CN208819824U CN208819824U CN201821802439.6U CN201821802439U CN208819824U CN 208819824 U CN208819824 U CN 208819824U CN 201821802439 U CN201821802439 U CN 201821802439U CN 208819824 U CN208819824 U CN 208819824U
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- plate
- screw rod
- shell
- fuse
- fixed
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Abstract
The utility model discloses a kind of aircraft fuse seats, including pedestal, the middle position of the base top is provided with shell, and the side of case top is hinged with cap, the cap bottom is uniformly equipped with strip far from the side of hinged place, the card slot matched with strip is provided on the shell, and the bottom end of enclosure interior is provided with mounting plate.The utility model is equipped with fixed plate, and it is piled in fixed plate and is provided with sliding slot, the distance between two groups of connecting plates can be changed by the movement of sliding block inside sliding slot, it is limited convenient for the fuse to different length, improve the practicability of device, it is more convenient to use, the setting of second threaded hole in fixed plate, stripper plate is driven to be moved by the second screw rod inside the second threaded hole, different size of fuse can be fixed, the fastness for improving fuse improves the using effect of fuse.
Description
Technical field
The utility model relates to air equipment technical field, specially a kind of aircraft fuse seat.
Background technique
It when circuit malfunctions or exception, is constantly increased along with electric current, and raised electric current is possible to damage electricity
Certain important devices in road, it is also possible to it burns circuit or even causes fire, if correctly having disposed fuse in circuit, that
Fuse will be when current anomaly be increased to certain height and temperature, itself fusing cutting electric current, to play
The effect of circuit safety operation is protected, and needs to be installed and consolidated using special pedestal in the use process of fuse
Fixed, traditional fuse seat during the installation process, can only install the fuse of regular length, and applicability is lower, using compared with
For inconvenience, and in the fixation procedure of fuse, traditional mode is clamped using fixing clip, and stability is poor, is easy
Loosening is generated after long-time use, influences the protecting effect of fuse, in addition traditional fuse seat is in disassembly process
It is more inconvenient, reduce the replacement efficiency of fuse.
Utility model content
The purpose of this utility model is to provide a kind of aircraft fuse seats, to solve to propose in above-mentioned background technique
The problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of aircraft fuse seat, including bottom
Seat, the middle position of the base top is provided with shell, and the side of case top is hinged with cap, the cap bottom
Side far from hinged place is uniformly equipped with strip, and the card slot matched with strip, and enclosure interior are provided on the shell
Bottom end be provided with mounting plate, the two sides at the top of the mounting plate are symmetrically arranged with sliding slot, and the inside of sliding slot is all provided with
One screw rod, first screw rod all extends to the outside of mounting plate, and the first screw rod is all provided with length far from one end of mounting plate
Adjusting knob is spent, the inside of the sliding slot is all provided with sliding block, and the inside of sliding block is all provided with and matches with the first screw rod
First threaded hole, the slider top is all provided with connecting plate close to the side of length adjustment knob, and connecting plate is close to length
The side of adjusting knob is all provided with connecting line, and the connecting line all extends to the outside of shell, and the slider top is far from even
The both ends of fishplate bar side are all provided with fixed plate, and the inside of fixed plate is all provided with the second threaded hole, second threaded hole
Inside be all provided with the second screw rod, be symmetrically arranged with stripper plate on the inside of the slider top fixed plate, and stripper plate is close
The middle position of fixed plate side is all provided with bearing, and second screw rod is all connect with bearing close to one end of stripper plate,
Second screw rod is all provided with fixed knob far from one end of stripper plate.
Preferably, the bottom at the shell both ends is all symmetrically arranged with heat release hole.
Preferably, the shape of the stripper plate is all arc, and the inside of stripper plate is all provided with rubber pad.
Preferably, waterproof coating is provided at the top of the cap.
Preferably, the outside of the length adjustment knob and fixed knob is all provided with anti-skid chequer.
Preferably, the four corners of the base top are all provided with fixed hole.
Compared with prior art, the utility model has the beneficial effects that the aircraft fuse seat is equipped with fixed plate,
And piled in fixed plate and be provided with sliding slot, by the movement of sliding block inside sliding slot can change between two groups of connecting plates away from
From, it is limited convenient for the fuse to different length, improves the practicability of device, it is more convenient to use, in fixed plate
The setting of second threaded hole drives stripper plate to be moved by the second screw rod inside the second threaded hole, can be to different big
Small fuse is fixed, and improves the fastness of fuse, improves the using effect of fuse, strip sets on cap
It sets, is used cooperatively by strip and the card slot on shell, so that the opening replacement of shell is more convenient, save fuse replacement
The required time improves replacement efficiency.
Detailed description of the invention
Fig. 1 is the main view schematic cross-sectional view of the utility model；
Fig. 2 is the schematic front view of the utility model；
Fig. 3 is the partial structural diagram of the utility model.
In figure: 1, pedestal；2, shell；3, connecting line；4, cap；5, strip；6, card slot；7, connecting plate；8, length adjustment
Knob；9, the first screw rod；10, the first threaded hole；11, sliding slot；12, stripper plate；13, sliding block；14, fixed plate；15, the second spiral shell
Bar；16, the second threaded hole；17, fixed knob；18, heat release hole；19, mounting plate；20, bearing.
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.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, a kind of embodiment provided by the utility model: a kind of aircraft fuse seat, including pedestal
1, the middle position at 1 top of pedestal is provided with shell 2, and the side at 2 top of shell is hinged with cap 4, and 4 bottom of cap is separate
The side of hinged place is uniformly equipped with strip 5, and the card slot 6 matched with strip 5, and the bottom inside shell 2 are provided on shell 2
End is provided with mounting plate 19, and the two sides at 19 top of mounting plate are symmetrically arranged with sliding slot 11, and the inside of sliding slot 11 is all provided with the
One screw rod 9, the first screw rod 9 all extends to the outside of mounting plate 19, and first one end of screw rod 9 far from mounting plate 19 is all provided with
Length adjustment knob 8, the inside of sliding slot 11 is all provided with sliding block 13, and the inside of sliding block 13 is all provided with and 9 phase of the first screw rod
First threaded hole 10 of cooperation, 13 top of sliding block are all provided with connecting plate 7, and connecting plate 7 close to the side of length adjustment knob 8
It is all provided with connecting line 3 close to the side of length adjustment knob 8, connecting line 3 all extends to the outside of shell 2,13 top of sliding block
Both ends far from 7 side of connecting plate are all provided with fixed plate 14, and the inside of fixed plate 14 is all provided with the second threaded hole 16, the
The inside of two threaded holes 16 is all provided with the second screw rod 15, and the inside of 13 top fixing plate 14 of sliding block is symmetrically arranged with stripper plate
12, and middle position of the stripper plate 12 close to 14 side of fixed plate is all provided with bearing 20, the second screw rod 15 is close to stripper plate
12 one end is all connect with bearing 20, and second one end of screw rod 15 far from stripper plate 12 is all provided with fixed knob 17.
In this embodiment: the bottom at 2 both ends of shell is all symmetrically arranged with heat release hole 18, improves the heat dissipation effect of device,
The shape of stripper plate 12 is all arc, and the inside of stripper plate 12 is all provided with rubber pad, improves the fixed stabilization of fuse
Property, the top of cap 4 is provided with waterproof coating, improves the waterproof effect of device, length adjustment knob 8 and fixed knob 17
Outside is all provided with anti-skid chequer, and convenient for fuse is limited and fixed, the four corners at 1 top of pedestal are all provided with fixed logical
Hole facilitates the installation of device.
Working principle: before use, pedestal is fixed by fixture nut, then, strip 5 is pressed, strip 5 is stretched
Into the inside of shell 2, then opens cap 4 and fuse is placed on to the top of two groups of sliding blocks 13, so after cap 4 is opened
Afterwards, rotation length adjustment knob 8 drives the first screw rod 9 to be rotated, and passes through the first screw rod 9 and the first threaded hole on sliding block 13
10 match, and band movable slider 13 is close to fuse, connecting plate 7 are bonded with the both ends of fuse, fuse length adjustment is complete
At then, rotation fixed knob 17 drives the second screw rod 15 to be rotated, and passes through the second screw rod 15 and stripper plate 12 is pushed to carry out
It is mobile, the two sides of fuse are clamped, degree fuse is fixed, and after fuse is installed, covers cap 4, so
Cap 4 is pressed afterwards, strip 5 is inserted into the inside of card slot 6, the sealing of cap 4 is completed.
Although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic into
Row equivalent replacement, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on should all
It is included within the scope of protection of this utility model.
Claims (6)
1. a kind of aircraft fuse seat, including pedestal (1), it is characterised in that: the middle position at the top of the pedestal (1)
Be provided with shell (2), and the side at the top of shell (2) is hinged with cap (4), cap (4) bottom far from hinged place one
Side is uniformly equipped with strip (5), the card slot (6) matched with strip (5) is provided on the shell (2), and shell (2) is internal
Bottom end be provided with mounting plate (19), the two sides at the top of the mounting plate (19) are symmetrically arranged with sliding slot (11), and sliding slot (11)
Inside be all provided with the first screw rod (9), first screw rod (9) all extends to the outside of mounting plate (19), and the first screw rod
(9) one end far from mounting plate (19) is all provided with length adjustment knob (8), and the inside of the sliding slot (11) is all provided with sliding block
(13), and the inside of sliding block (13) is all provided with the first threaded hole (10) matched with the first screw rod (9), the sliding block (13)
Top is all provided with connecting plate (7) close to the side of length adjustment knob (8), and connecting plate (7) is close to length adjustment knob (8)
Side be all provided with connecting line (3), the connecting line (3) all extends to the outside of shell (2), remote at the top of the sliding block (13)
Both ends from connecting plate (7) side are all provided with fixed plate (14), and the inside of fixed plate (14) is all provided with the second threaded hole
(16), the inside of second threaded hole (16) is all provided with the second screw rod (15), sliding block (13) top fixing plate (14)
Inside be symmetrically arranged with stripper plate (12), and stripper plate (12) is all provided with close to the middle position of fixed plate (14) side
Bearing (20), second screw rod (15) all connect with bearing (20) close to the one end of stripper plate (12), second screw rod
(15) one end far from stripper plate (12) is all provided with fixed knob (17).
2. a kind of aircraft fuse seat according to claim 1, it is characterised in that: the bottom at shell (2) both ends
Portion is all symmetrically arranged with heat release hole (18).
3. a kind of aircraft fuse seat according to claim 1, it is characterised in that: the shape of the stripper plate (12)
It is all arc, and the inside of stripper plate (12) is all provided with rubber pad.
4. a kind of aircraft fuse seat according to claim 1, it is characterised in that: set at the top of the cap (4)
It is equipped with waterproof coating.
5. a kind of aircraft fuse seat according to claim 1, it is characterised in that: the length adjustment knob (8)
Anti-skid chequer is all provided with the outside of fixed knob (17).
6. a kind of aircraft fuse seat according to claim 1, it is characterised in that: four at the top of the pedestal (1)
Fixed hole is all provided at angle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821802439.6U CN208819824U (en) | 2018-11-02 | 2018-11-02 | A kind of aircraft fuse seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821802439.6U CN208819824U (en) | 2018-11-02 | 2018-11-02 | A kind of aircraft fuse seat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208819824U true CN208819824U (en) | 2019-05-03 |
Family
ID=66280548
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821802439.6U Active CN208819824U (en) | 2018-11-02 | 2018-11-02 | A kind of aircraft fuse seat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208819824U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111740316A (en) * | 2020-07-10 | 2020-10-02 | 李翠霞 | Automatic device of changing of block terminal sealed fuse-element |
-
2018
- 2018-11-02 CN CN201821802439.6U patent/CN208819824U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111740316A (en) * | 2020-07-10 | 2020-10-02 | 李翠霞 | Automatic device of changing of block terminal sealed fuse-element |
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