CN110195810A - A kind of detection part applied to avionic instrument - Google Patents
A kind of detection part applied to avionic instrument Download PDFInfo
- Publication number
- CN110195810A CN110195810A CN201910557515.4A CN201910557515A CN110195810A CN 110195810 A CN110195810 A CN 110195810A CN 201910557515 A CN201910557515 A CN 201910557515A CN 110195810 A CN110195810 A CN 110195810A
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- China
- Prior art keywords
- fixedly connected
- wall
- side wall
- detection part
- support base
- 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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- 238000001514 detection method Methods 0.000 title claims abstract description 27
- 230000007246 mechanism Effects 0.000 claims abstract description 25
- 230000001105 regulatory effect Effects 0.000 claims abstract description 8
- SZVJSHCCFOBDDC-UHFFFAOYSA-N iron(II,III) oxide Inorganic materials O=[Fe]O[Fe]O[Fe]=O SZVJSHCCFOBDDC-UHFFFAOYSA-N 0.000 claims description 17
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 14
- 239000007787 solid Substances 0.000 claims description 5
- 238000009434 installation Methods 0.000 claims description 4
- 238000005096 rolling process Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 2
- UGQMRVRMYYASKQ-KQYNXXCUSA-N Inosine Chemical compound O[C@@H]1[C@H](O)[C@@H](CO)O[C@H]1N1C2=NC=NC(O)=C2N=C1 UGQMRVRMYYASKQ-KQYNXXCUSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/02—Heads
- F16M11/04—Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
- F16M11/041—Allowing quick release of the apparatus
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M11/00—Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
- F16M11/20—Undercarriages with or without wheels
- F16M11/24—Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other
- F16M11/26—Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other by telescoping, with or without folding
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Geophysics And Detection Of Objects (AREA)
Abstract
The present invention relates to detecting instrument technical fields, and disclose a kind of detection part applied to avionic instrument, including support base, receiver, fixed plate, body, focus lamp and detector lens, side wall on the upside of the support base is connected with clamp mechanism, and the four corners of the support base lower surface are respectively connected with height adjustment mechanism；The clamp mechanism includes two fixed plates for being symmetrically fixedly connected on side wall on the upside of support base, the same guide rod is fixedly connected between two fixed plates, the bar wall of the guide rod is slidingly connected, and there are two mobile clamping plates, the side wall of two mobile clamping plate opposite sides offers sliding eye, the guide rod runs through mobile clamping plate by sliding eye, and the side wall of two mobile clamping plate opposite sides offers fixation hole.The present invention can quickly fix electronic instrument, simple to operate, be capable of the height of regulating device according to demand, the effective scope of application for improving device.
Description
Technical field
The present invention relates to detecting instrument technical field more particularly to a kind of detection parts applied to avionic instrument.
Background technique
Avionic instrument is the component part of avionics system, after the completion of avionic instrument production and assembly, is needed
The detection device of profession is used to detect electronic instrument, whether detection avionic instrument can just produce use, surface
With the presence or absence of flaw, guarantee the normal use of aviation list instrument.
Such as Chinese patent grant number is the patent of CN207753781U, discloses a kind of electronic instrument applied to aviation
Detection part, structure include fixing support, receiver, fixed plate, body, focus lamp, lodging bench, support base, detection mirror
Head device, operation panel, control body, support frame, positioning plate, bolt hole, fixture part, the fixing support upper end and support bottom
Seat lower end is mutually welded, and the receiver right end is connected with body left end, and the body insertion is installed in fixed plate, the machine
Body right end is connected with focus lamp left end, and the fixed plate lower end is mutually welded with positioning plate upper end, the lodging bench and bolt hole
It is integrated, the support base upper end is mutually welded with lodging bench lower end, and the detector lens device right end and body are left
End is connected.The electronic instrument detection part that one of above-mentioned patent is applied to aviation has the disadvantage that above-mentioned apparatus
Fixture needs to turn when in use multiple bolts and is clamped fixation, and operation is more inconvenient, and the height of above-mentioned apparatus can not root
It is adjusted according to actual demand, leads to the smaller scope of application of device.
Summary of the invention
The purpose of the present invention is to solve the problem of can not adjusting with height inconvenient for use of fixture in the prior art, and mention
A kind of detection part applied to avionic instrument out.
To achieve the goals above, present invention employs following technical solutions:
A kind of detection part applied to avionic instrument, including support base, receiver, fixed plate, body, focusing
Mirror and detector lens, the side wall on the upside of the support base are connected with clamp mechanism, the four corners of the support base lower surface
It is respectively connected with height adjustment mechanism；
The clamp mechanism includes two fixed plates for being symmetrically fixedly connected on side wall on the upside of support base, and two described solid
The same guide rod is fixedly connected between fixed board, the bar wall of the guide rod is slidingly connected, and there are two mobile clamping plate, two institutes
The side wall for stating mobile clamping plate opposite side offers sliding eye, and the guide rod is run through by sliding eye moves clamping plate, and two
The side wall of the mobile clamping plate opposite side offers fixation hole, and the hole wall of two fixation holes is fixedly connected to screw thread
Cylinder, the hand of spiral of two thread barrels is on the contrary, two thread barrel inner screw sheaths are connected to same root threaded rod, two institutes
The side wall for stating fixed plate opposite side offers rotation hole, and the hole wall of the rotation hole passes through the bar of ball bearing and threaded rod
The right end of wall rotation connection, the threaded rod stretches out rotation hole.
Preferably, the height adjustment mechanism includes the standing screw for being fixedly connected on support base lower surface, described solid
The bar wall movable sleeve for determining screw rod is equipped with rotary cylinder, and the inner wall of the rotary cylinder is fixedly connected with adjusting nut, the adjusting nut
Thread bush is set to the bar wall of standing screw, and the rotary cylinder is fixedly connected with pedestal far from one end of support base.
Preferably, the right end of the threaded rod is fixedly connected with rotating plate, and side wall of the rotating plate close to fixed plate side is opened
Equipped with mounting hole, pivot bush unit has gag lever post in the mounting hole, and the bar wall of the gag lever post and the hole wall of mounting hole slide and connect
It connects, side wall of the fixed plate close to rotating plate side positioned at right side offers multiple limiting slots corresponding with gag lever post, institute
The setting of limiting slot annular is stated, the bar wall fixing sleeve of the gag lever post is equipped with limit girth sheets, solid between limit girth sheets and the rotating plate
Surely it is connected with same root reset spring, the reset spring is movably set in the bar wall of gag lever post.
Preferably, two mobile clamping plate opposite side side walls are fixedly connected to rubber mat plate.
Preferably, the pedestal is rotatablely connected by rolling bearing and rotary cylinder, and the side wall on the downside of the pedestal is fixed to be connected
It is connected to non-slip mat.
Preferably, the slot bottom of the limiting slot is fixedly connected with the first magnetite, and the gag lever post is located at one in limiting slot
End is fixedly connected with the second magnetite.
Preferably, the hole wall of the mounting hole is symmetrically fixedly connected there are two position limiting slide block, the hole wall pair of the gag lever post
Claim the limit sliding chutes to match there are two opening up with position limiting slide block.
Preferably, the rotary cylinder fixed sleeves are equipped with frosted set.
Preferably, first magnetite is opposite with the polarity of the second magnetite opposite side.
Compared with prior art, the present invention provides a kind of detection part applied to avionic instrument, have following
The utility model has the advantages that
It 1, should be applied to the detection part of avionic instrument, by the clamp mechanism of setting, in use, by electronic instrument
It is placed between two mobile clamping plates, rotating threaded rod by being threadedly engaged between threaded rod and two thread barrels makes two
Thread barrel moves towards, and two thread barrels drive two mobile clamping plates to move towards, and two mobile clamping plates clamp electronic instrument,
Complete the fixation of electronic instrument；After the completion of detection, threaded rod is rotated backward, passes through the screw thread between threaded rod and two thread barrels
Cooperation, is moved away from two thread barrels, and two thread barrels drive two mobile clamping plates to be moved away from, and releases two mobile clamping plates
The limit of electronic instrument is fixed, mechanism can quickly fix electronic instrument, simple to operate.
It 2, should be applied to the detection part of avionic instrument, by the regulating mechanism of setting, in use, rotation rotation
Cylinder, rotary cylinder drive adjusting nut rotation, by being threadedly engaged between adjusting nut and standing screw, move adjusting nut
Dynamic, it is mobile that adjusting nut drives rotary cylinder, thus change the height of support base, the adjusting of complete twin installation height, mechanism
It is capable of the height of regulating device according to demand, the effective scope of application for improving device.
It is not directed to part in the device to be the same as those in the prior art or can be realized by using the prior art, the present invention can
Quickly fixed electronic instrument, it is simple to operate, it is capable of the height of regulating device according to demand, it is effective to improve the suitable of device
Use range.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the detection part applied to avionic instrument proposed by the present invention；
Fig. 2 is the structural schematic diagram of part A in Fig. 1；
Fig. 3 is the structural schematic diagram of part B in Fig. 2；
Fig. 4 is the structural schematic diagram of C portion in Fig. 1.
In figure: 1 support base, 2 clamp mechanisms, 21 fixed plates, 22 guide rods, 23 mobile clamping plates, 24 sliding eyes, 25 are fixed
Hole, 26 thread barrels, 27 threaded rods, 28 rotation holes, 3 regulating mechanisms, 31 standing screws, 32 rotary cylinders, 33 adjusting nuts, 34 feet
Seat, 4 rotating plates, 5 mounting holes, 6 gag lever posts, 7 limiting slots, 8 limit girth sheets, 9 reset springs, 10 rubber mat plates, 11 non-slip mats, 12 the
One magnetite, 13 second magnetites, 14 frosted sets.
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", "front", "rear", "left", "right", "top",
The orientation or positional relationship of the instructions such as "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, merely to just
In description the present invention and simplify description, rather than the device or element of indication or suggestion meaning must have a particular orientation, with
Specific orientation construction and operation, therefore be not considered as limiting the invention.
Referring to Fig.1-4, a kind of detection part applied to avionic instrument, including support base 1, receiver, fixation
The side wall of plate, body, focus lamp and detector lens, 1 upside of support base is connected with clamp mechanism 2,1 lower surface of support base
Four corners are respectively connected with height adjustment mechanism 3；
Clamp mechanism 2 includes two fixed plates 21 for being symmetrically fixedly connected on 1 upside side wall of support base, two fixed plates
The same guide rod 22 is fixedly connected between 21, the bar wall of guide rod 22 is slidingly connected, and there are two mobile clamping plate 23, two shiftings
The side wall of dynamic 23 opposite side of clamping plate offers sliding eye 24, and guide rod 22 is run through by sliding eye 24 moves clamping plate 23, and two
The side wall of a 23 opposite side of mobile clamping plate offers fixation hole 25, and the hole wall of two fixation holes 25 is fixedly connected to screw thread
Cylinder 26, for the hand of spiral of two thread barrels 26 on the contrary, two 26 inner screw sheaths of thread barrel are connected to same root threaded rod 27, two solid
The side wall of 21 opposite side of fixed board offers rotation hole 28, and the hole wall of rotation hole 28 passes through the bar of ball bearing and threaded rod 27
Wall rotation connection, the right end of threaded rod 27 stretch out rotation hole 28, in use, by electronic instrument be placed on two mobile clamping plates 23 it
Between, threaded rod 27 is rotated, by being threadedly engaged between threaded rod 27 and two thread barrels 26, moves two thread barrels 26 in opposite directions
Dynamic, two thread barrels 26 drive two mobile clamping plates 23 to move towards, and two mobile clamping plates 23 clamp electronic instrument, complete electricity
The fixation of sub- instrument；After the completion of detection, threaded rod 27 is rotated backward, passes through the screw thread between threaded rod 27 and two thread barrels 26
Cooperation, is moved away from two thread barrels 26, and two thread barrels 26 drive two mobile clamping plates 23 to be moved away from, and releases two shiftings
Dynamic clamping plate 23 fixes the limit of electronic instrument, and mechanism can quickly fix electronic instrument, simple to operate.
Height adjustment mechanism 3 includes the standing screw 31 for being fixedly connected on 1 lower surface of support base, the bar of standing screw 31
Wall movable sleeve is equipped with rotary cylinder 32, and the inner wall of rotary cylinder 32 is fixedly connected with adjusting nut 33, and 33 thread bush of adjusting nut is set to
The bar wall of standing screw 31, rotary cylinder 32 are fixedly connected with pedestal 34 far from one end of support base 1, in use, rotation rotation
Cylinder 32, rotary cylinder 32 drive adjusting nut 33 to rotate, by being threadedly engaged between adjusting nut 33 and standing screw 31, make to adjust
It is mobile to save nut 33, it is mobile that adjusting nut 33 drives rotary cylinder 32, to change the height of support base 1, complete twin installation is high
The adjusting of degree, mechanism are capable of the height of regulating device according to demand, the effective scope of application for improving device.
The right end of threaded rod 27 is fixedly connected with rotating plate 4, and side wall of the rotating plate 4 close to 21 side of fixed plate offers mounting hole
5, pivot bush unit has gag lever post 6 in mounting hole 5, and the bar wall and the hole wall of mounting hole 5 of gag lever post 6 are slidably connected, positioned at right side
Side wall of the fixed plate 21 close to 4 side of rotating plate offers multiple limiting slots 7 corresponding with gag lever post 6, and 7 annular of limiting slot is set
It sets, the bar wall fixing sleeve of gag lever post 6 is equipped with limit girth sheets 8, limits and is fixedly connected with same root reset between girth sheets 8 and rotating plate 4
Spring 9, reset spring 9 are movably set in the bar wall of gag lever post 6, in use, pulling gag lever post 6, gag lever post 6 are made to be detached from limiting slot
7, it releases gag lever post 6 and the limit of rotating plate 4 is fixed, rotation rotating plate 4 can be such that threaded rod 27 rotates, when threaded rod 27 uses completion
Afterwards, so that gag lever post 6 is directed at limiting slot 7, unclamp gag lever post 6, under the action of 9 selfer power of reset spring, 9 band of reset spring
Dynamic limit girth sheets 8 is mobile, and limit girth sheets 8 drives gag lever post 6 mobile, springs into gag lever post 6 in corresponding limiting slot 7, gag lever post 6
Threaded rod 27 can be fixed, prevent threaded rod 27 from voluntarily rotating.
Two mobile 23 opposite side side walls of clamping plate are fixedly connected to rubber mat plate 10 and protect to electronic instrument, keep away
Exempt from mobile clamping plate 23 surface of electronic instrument is caused to scratch.
Pedestal 34 is rotatablely connected by rolling bearing and rotary cylinder 32, and the side wall of 34 downside of pedestal is fixedly connected with non-slip mat
11, non-slip mat 11 can be improved the frictional resistance between pedestal 34 and ground, improve the stability of device.
The slot bottom of limiting slot 7 is fixedly connected with the first magnetite 12, and one end that gag lever post 6 is located in limiting slot 7 is fixedly connected
There is the second magnetite 13, is cooperated by the first magnetite 12 and the second magnetite 13, can be improved the stability of gag lever post 6.
The hole wall of mounting hole 5 is symmetrically fixedly connected there are two position limiting slide block, the hole wall of gag lever post 6 symmetrically open up there are two with
The limit sliding chutes that position limiting slide block matches are cooperated by position limiting slide block and limit sliding chutes, can be limited gag lever post 6
Position, inclination when preventing gag lever post 6 mobile are inserted into limiting slot 7 convenient for gag lever post 6.
32 fixed sleeves of rotary cylinder are equipped with frosted set 14, convenient for rotation rotary cylinder 32, improve the convenience of operation.
First magnetite 12 is opposite with the polarity of 13 opposite side of the second magnetite, contacts the first magnetite 12 with the second magnetite 13
When can be attached together.
In the present invention, in use, electronic instrument is placed between two mobile clamping plates 23, threaded rod 27 is rotated, is passed through
Being threadedly engaged between threaded rod 27 and two thread barrels 26 moves towards two thread barrels 26, and two thread barrels 26 drive
Two mobile clamping plates 23 move towards, and two mobile clamping plates 23 clamp electronic instrument, complete the fixation of electronic instrument；It has detected
Cheng Hou rotates backward threaded rod 27, by being threadedly engaged between threaded rod 27 and two thread barrels 26, makes two thread barrels 26
It is moved away from, two thread barrels 26 drive two mobile clamping plates 23 to be moved away from, and release two mobile clamping plates 23 to electronic instrument
Limit fix, mechanism can quickly fix electronic instrument, simple to operate；In use, rotation rotary cylinder 32, rotation
Cylinder 32 drives adjusting nut 33 to rotate, and by being threadedly engaged between adjusting nut 33 and standing screw 31, makes adjusting nut 33
Mobile, it is mobile that adjusting nut 33 drives rotary cylinder 32, thus change the height of support base 1, the adjusting of complete twin installation height,
Mechanism is capable of the height of regulating device according to demand, the effective scope of application for improving device.
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 (9)
1. a kind of detection part applied to avionic instrument, including it is support base (1), receiver, fixed plate, body, poly-
Burnt mirror and detector lens, which is characterized in that the side wall on the upside of the support base (1) is connected with clamp mechanism (2), the support
The four corners of pedestal (1) lower surface are respectively connected with height adjustment mechanism (3)；
The clamp mechanism (2) includes two fixed plates (21) for being symmetrically fixedly connected on side wall on the upside of support base (1), and two
It is fixedly connected with the same guide rod (22) between the fixed plate (21), the bar wall movable sleeve of the guide rod (22) is equipped with two
The side wall of a mobile clamping plate (23), two mobile clamping plate (23) opposite sides offers sliding eye (24), the guiding
Bar (22) runs through mobile clamping plate (23) by sliding eye (24), and the side wall of two mobile clamping plate (23) opposite sides opens up
Have fixation hole (25), the hole wall of two fixation holes (25) is fixedly connected to thread barrel (26), two thread barrels
(26) for hand of spiral on the contrary, two thread barrel (26) inner screw sheaths are connected to same root threaded rod (27), two described solid
The side wall of fixed board (21) opposite side offers rotation hole (28), and the hole wall of the rotation hole (28) passes through ball bearing and spiral shell
The bar wall of rasp bar (27) is rotatablely connected, and the right end of the threaded rod (27) stretches out rotation hole (28).
2. a kind of detection part applied to avionic instrument according to claim 1, which is characterized in that the height
Regulating mechanism (3) includes the standing screw (31) for being fixedly connected on support base (1) lower surface, the bar of the standing screw (31)
Wall movable sleeve is equipped with rotary cylinder (32), and the inner wall of the rotary cylinder (32) is fixedly connected with adjusting nut (33), the adjusting spiral shell
Female (33) thread bush is set to the bar wall of standing screw (31), and the one end of the rotary cylinder (32) far from support base (1) is fixed to be connected
It is connected to pedestal (34).
3. a kind of detection part applied to avionic instrument according to claim 1, which is characterized in that the screw thread
The right end of bar (27) is fixedly connected with rotating plate (4), and side wall of the rotating plate (4) close to fixed plate (21) side offers mounting hole
(5), the interior pivot bush unit of the mounting hole (5) has gag lever post (6), and the bar wall of the gag lever post (6) and the hole wall of mounting hole (5) are sliding
Dynamic connection, the side wall of close rotating plate (4) side of the fixed plate (21) positioned at right side offer multiple opposite with gag lever post (6)
The limiting slot (7) answered, limiting slot (7) the annular setting, the bar wall fixing sleeve of the gag lever post (6) are equipped with limit girth sheets (8),
It is fixedly connected with same root reset spring (9) between the limit girth sheets (8) and rotating plate (4), reset spring (9) movable sleeve
Set on the bar wall of gag lever post (6).
4. a kind of detection part applied to avionic instrument according to claim 1, which is characterized in that described in two
Mobile clamping plate (23) opposite side side wall is fixedly connected to rubber mat plate (10).
5. a kind of detection part applied to avionic instrument according to claim 2, which is characterized in that the pedestal
(34) it is rotatablely connected by rolling bearing and rotary cylinder (32), the side wall on the downside of the pedestal (34) is fixedly connected with non-slip mat
(11)。
6. a kind of detection part applied to avionic instrument according to claim 3, which is characterized in that the limit
The slot bottom of slot (7) is fixedly connected with the first magnetite (12), and one end that the gag lever post (6) is located in limiting slot (7) is fixedly connected
There are the second magnetite (13).
7. a kind of detection part applied to avionic instrument according to claim 3, which is characterized in that the installation
The hole wall in hole (5) is symmetrically fixedly connected there are two position limiting slide block, the hole wall of the gag lever post (6) symmetrically open up there are two with limit
The limit sliding chutes that sliding block matches.
8. a kind of detection part applied to avionic instrument according to claim 2, which is characterized in that the rotation
Cylinder (32) fixed sleeves are equipped with frosted set (14).
9. a kind of detection part applied to avionic instrument according to claim 6, which is characterized in that described first
Magnetite (12) is opposite with the polarity of the second magnetite (13) opposite side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910557515.4A CN110195810A (en) | 2019-06-26 | 2019-06-26 | A kind of detection part applied to avionic instrument |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910557515.4A CN110195810A (en) | 2019-06-26 | 2019-06-26 | A kind of detection part applied to avionic instrument |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110195810A true CN110195810A (en) | 2019-09-03 |
Family
ID=67755213
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910557515.4A Withdrawn CN110195810A (en) | 2019-06-26 | 2019-06-26 | A kind of detection part applied to avionic instrument |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110195810A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112944136A (en) * | 2021-02-03 | 2021-06-11 | 天津海旺海上石油工程技术服务有限公司 | F-type frequency conversion antiscaling instrument |
| CN113074682A (en) * | 2021-03-09 | 2021-07-06 | 机械工业第九设计研究院有限公司 | Line side vehicle species detection mechanism |
| CN115072117A (en) * | 2022-07-22 | 2022-09-20 | 四川科斯特自动化设备有限公司 | Automatic change packagine machine with automatic mark device that pastes |
-
2019
- 2019-06-26 CN CN201910557515.4A patent/CN110195810A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112944136A (en) * | 2021-02-03 | 2021-06-11 | 天津海旺海上石油工程技术服务有限公司 | F-type frequency conversion antiscaling instrument |
| CN112944136B (en) * | 2021-02-03 | 2022-06-17 | 天津嘉许石油工程技术有限公司 | F-type frequency conversion antiscaling instrument |
| CN113074682A (en) * | 2021-03-09 | 2021-07-06 | 机械工业第九设计研究院有限公司 | Line side vehicle species detection mechanism |
| CN115072117A (en) * | 2022-07-22 | 2022-09-20 | 四川科斯特自动化设备有限公司 | Automatic change packagine machine with automatic mark device that pastes |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190903 |