CN208723445U - A kind of cable apparatus for examination and repair being installed on telecontrolled aircraft bottom - Google Patents
A kind of cable apparatus for examination and repair being installed on telecontrolled aircraft bottom Download PDFInfo
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- CN208723445U CN208723445U CN201821513825.3U CN201821513825U CN208723445U CN 208723445 U CN208723445 U CN 208723445U CN 201821513825 U CN201821513825 U CN 201821513825U CN 208723445 U CN208723445 U CN 208723445U
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- round block
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Abstract
The utility model embodiment discloses a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom, including plate body, threaded hole, screw, half round block, inner cavity, supporting plate, worm screw, bearing, adjusting knob, anti-skid chequer, shaft, gear, bull stick, telemetering electroprobe and opening.The utility model setting worm screw and turbine can effectively adjust the direction of bull stick, cooperate the original length of bull stick, to allow aircraft test cable in different environments, it is different from traditional aircraft electrical cable test tool detection device and fixes, be not easy the drawbacks of detecting；The end of bull stick is provided with telemetering electroprobe, telemetering electroprobe can induce whether cable internal-internal has electric current process under the premise of not touching cable, it is different from tradition and carries out test electric current it is possible to the problem of causing high-tension current to destroy aircraft using the method for test, the apparatus structure is simple, it is easy to use, it is suitble to promote the use of.
Description
Technical field
The utility model relates to cable repair apparatus technical field more particularly to a kind of electricity for being installed on telecontrolled aircraft bottom
Cable apparatus for examination and repair.
Background technique
Cable is usually by several or several groups of conducting wires form, and outside cable is frequently exposed to field, when being used due to cable
Between it is longer, need periodic detection not just to guarantee that cable can work normally in use, also for preventing
Because of fire condition etc. caused by leaking electricity.
When detecting aerial cables, usually increases a detection device in the bottom end of telecontrolled aircraft and detected, but by
The environment locating for every place's cable and wire is different, when having object around wire and cable, because the position of measuring tool is fixed
, telecontrolled aircraft can be more troublesome for measurement cable；Moreover, when most of progress detection cables using telecontrolled aircraft, usually
It is to be tested using the mode of touching, when encountering cable leakage situation, it is easy to be caused to telecontrolled aircraft and detection device
Damage.Therefore, a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom is proposed regarding to the issue above.
Utility model content
The utility model embodiment provides a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom, including including plate
Body, fixed mechanism and regulating mechanism；
The fixed mechanism includes threaded hole, screw and half round block, the two sides of the plate body symmetrically open up two it is identical
Threaded hole, inner cavity, and the semicircle is arranged inside half round block by affixed half round block of screw in the bottom of the plate body
The side wall of block offers opening；
The regulating mechanism includes worm screw, adjusting knob and gear, and one side of the plate body close to the inner cavity is affixed
There are supporting plate, one end of the side wall rotation connection worm screw of the supporting plate, another end surfaces of the worm screw are socketed with bearing, and institute
The outside that bearing is set to half round block is stated, one end that the worm screw is placed in outside half round block is connected with adjusting knob, described
The inner sidewall of half round block is rotatablely connected gear by shaft, and the bottom of the gear is fixedly connected with bull stick, and the bull stick is separate
One end of the gear is placed in the outside of half round block through opening, and the bull stick be connected with far from one end of the gear it is distant
Test pencil.
Preferably, the plate body, that the central axes of half round block and the inner cavity in the vertical direction are located at same is straight
On line.
Preferably, the embedded side wall for being installed on half round block in the outer ring of the bearing.
Preferably, the side wall of the adjusting knob is carved with anti-skid chequer.
Preferably, the gear is semicircle dentalation.
Preferably, the gear engages connecting worm.
The beneficial effects of the utility model are:
1. the utility model setting worm screw and turbine can effectively adjust the direction of bull stick, cooperate the original length of bull stick
Degree is different from traditional aircraft electrical cable test tool detection to allow aircraft test cable in different environments
Device is fixed, and the drawbacks of detecting is not easy；
2. being provided with telemetering electroprobe in the end of bull stick, telemetering electroprobe can induce electricity under the premise of not touching cable
Whether cable internal-internal has electric current process, is different from tradition using the method for test and carries out test electric current it is possible to leading to height
Current voltage destroys the problem of aircraft, and the apparatus structure is simple, easy to use, is suitble to promote the use of.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
It puts, can also be obtained according to these attached drawings other attached drawings.
Fig. 1 is the utility model schematic diagram of internal structure；
Fig. 2 is the utility model side structure schematic view.
In figure: 1, plate body, 2, threaded hole, 3, screw, 4, half round block, 5, inner cavity, 6, supporting plate, 7, worm screw, 8, bearing, 9,
Adjusting knob, 10, anti-skid chequer, 11, shaft, 12, gear, 13, bull stick, 14, telemetering electroprobe, 15, opening.
Specific embodiment
In order to make those skilled in the art better understand the scheme of the utility model, with reference to the accompanying drawing and specific implementation
The utility model is described in further detail for mode.Obviously, described embodiment is only the utility model a part
Embodiment, instead of all the embodiments.Based on the embodiments of the present invention, those of ordinary skill in the art are not doing
Every other embodiment obtained under the premise of creative work out, fall within the protection scope of the utility model.
It please refers to shown in Fig. 1-2, a kind of cable apparatus for examination and repair being installed on telecontrolled aircraft bottom, including plate body 1, fixed machine
Structure and regulating mechanism；
The fixed mechanism includes threaded hole 2, screw 3 and half round block 4, and the two sides of the plate body 1 symmetrically open up two
Identical threaded hole 2, convenient for that will reequip to the bottom for being fixed on telecontrolled aircraft, the bottom of the plate body 1 is affixed by screw 3
Inner cavity 5 is arranged inside half round block 4 convenient for assembly regulating mechanism in half round block 4, convenient for assembling regulating mechanism, and the semicircle
The side wall of block 4 offers opening 15, rotates convenient for bull stick 13；
The regulating mechanism includes worm screw 7, adjusting knob 9 and gear 12, and the bottom of the plate body 1 is placed in inside inner cavity 5
The side on surface be connected with supporting plate 6, be easily installed worm screw 7, one end of the side wall rotation connection worm screw 7 of the supporting plate 6 is convenient for
Power is transmitted, the other end surface of the worm screw 7 is socketed with bearing 8, and juxtaposition bearing 8 is set to the outside of half round block 4, is convenient for
Operation, and one end that the worm screw 7 is placed in half round block 4 outside is connected with adjusting knob 9, convenient for operating, half round block 4 it is interior
Side wall is rotatablely connected gear 12 by shaft 11, and convenient for adjusting the angle of bull stick 13, the bottom of the gear 12 is connected with bull stick
13, it is easily installed telemetering electroprobe 14, one end of the separate gear 12 of the bull stick 13 is placed in the outer of half round block 4 through opening 15
Portion, and the bull stick 13 is connected with telemetering electroprobe 14 far from one end of gear 12, convenient for detection.
The plate body 1, half round block 4 and the central axes of the inner cavity 5 in the vertical direction are located on the same line,
Convenient for rationally utilizing space；The embedded side wall for being installed on half round block 4 in the outer ring of the bearing 8, rotates convenient for worm screw 7；The tune
The side wall of section knob 9 is carved with anti-skid chequer 10, convenient for anti-skidding；The gear 12 is semicircle dentalation, and the gear 12 engages
Connecting worm 7.
When the utility model is used, the electric elements occurred in the application external connection battery and control when in use
Switch is secured the device to the bottom of telecontrolled aircraft by bolt and threaded hole 2, and is controlled by rotation adjusting knob 9
The position of pawl 13, principle are as follows: after rotation adjusting knob 9, adjusting knob 9 drives worm screw 7 to rotate, and worm screw 7 drives turbine
12 rotations, turbine 12 drive bull stick 13 to rotate, and after bull stick 13 turns to suitable angle, stop operating adjusting knob 9, due to
Turbine 12 and worm screw 13 have self-locking function, so bull stick 13 reversely will not drive worm screw 7 to rotate by turbine 12, open telemetering
Electroprobe 14, and control telecontrolled aircraft and reach corresponding detection position, by telemetering electroprobe 14 close to the cable position for needing to detect
?.
049 model and its relevant mating electricity that telemetering single 14 is produced using Hedong District Yong Gong hardware tool firm
Source and circuit.
It is related to circuit and electronic component and module is the prior art, those skilled in the art may be implemented completely,
Without superfluous words, the content of the utility model protection is not related to the improvement for software and method yet.
A kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom provided by the utility model has been carried out in detail above
It is thin to introduce, for those of ordinary skill in the art, based on the idea of the embodiment of the present invention, in specific embodiment and answer
With in range, there will be changes, in conclusion the content of the present specification should not be construed as a limitation of the present invention.
Claims (6)
1. a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom, it is characterised in that: including plate body (1), fixed mechanism and
Regulating mechanism；
The fixed mechanism includes threaded hole (2), screw (3) and half round block (4), and the two sides of the plate body (1) symmetrically open up
The bottom of two identical threaded holes (2), the plate body (1) passes through screw (3) affixed half round block (4), half round block (4)
Inside setting inner cavity (5), and the side wall of half round block (4) offers opening (15)；
The regulating mechanism includes worm screw (7), adjusting knob (9) and gear (12), and the plate body (1) is close to the inner cavity (5)
One side be connected with supporting plate (6), one end of the side wall of the supporting plate (6) rotation connection worm screw (7), the worm screw (7) it is another
End surface is socketed with bearing (8), and the bearing (8) is set to the outside of half round block (4), and the worm screw (7) is set
It is connected with adjusting knob (9) in the external one end of half round block (4), the inner sidewall of half round block (4) is rotated by shaft (11)
The bottom of connection gear (12), the gear (12) is fixedly connected with bull stick (13), and the bull stick (13) is far from the gear
(12) one end is placed in the outside of half round block (4) through opening (15), and the bull stick (13) is far from the gear (12)
One end is connected with telemetering electroprobe (14).
2. a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom according to claim 1, it is characterised in that: described
Plate body (1), the central axes of half round block (4) and the inner cavity (5) in the vertical direction are located on the same line.
3. a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom according to claim 1, it is characterised in that: described
The embedded side wall for being installed on half round block (4) in the outer ring of bearing (8).
4. a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom according to claim 1, it is characterised in that: described
The side wall of adjusting knob (9) is carved with anti-skid chequer (10).
5. a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom according to claim 1, it is characterised in that: described
Gear (12) is semicircle dentalation.
6. a kind of cable apparatus for examination and repair for being installed on telecontrolled aircraft bottom according to claim 1, it is characterised in that: described
Gear (12) engages connecting worm (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821513825.3U CN208723445U (en) | 2018-09-14 | 2018-09-14 | A kind of cable apparatus for examination and repair being installed on telecontrolled aircraft bottom |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821513825.3U CN208723445U (en) | 2018-09-14 | 2018-09-14 | A kind of cable apparatus for examination and repair being installed on telecontrolled aircraft bottom |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208723445U true CN208723445U (en) | 2019-04-09 |
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ID=65982181
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821513825.3U Active CN208723445U (en) | 2018-09-14 | 2018-09-14 | A kind of cable apparatus for examination and repair being installed on telecontrolled aircraft bottom |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208723445U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114000489A (en) * | 2021-11-16 | 2022-02-01 | 中建鸿腾建设集团有限公司 | Device and method for monitoring ground settlement value after pressure reduction and precipitation |
-
2018
- 2018-09-14 CN CN201821513825.3U patent/CN208723445U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114000489A (en) * | 2021-11-16 | 2022-02-01 | 中建鸿腾建设集团有限公司 | Device and method for monitoring ground settlement value after pressure reduction and precipitation |
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