CN207007147U - A kind of land survey telescope-type laser range finder - Google Patents
A kind of land survey telescope-type laser range finder Download PDFInfo
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- CN207007147U CN207007147U CN201720582292.3U CN201720582292U CN207007147U CN 207007147 U CN207007147 U CN 207007147U CN 201720582292 U CN201720582292 U CN 201720582292U CN 207007147 U CN207007147 U CN 207007147U
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- laser light
- laser
- transmitter
- forward laser
- range finder
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Abstract
The utility model discloses a kind of land survey telescope-type laser range finder, including fuselage cover, the side of the fuselage cover is provided with forward laser light receiver, the side of the forward laser light receiver is connected with transmitter top cover by axis of rotation, the side of the forward laser light transmitter is connected with receiver top cover by axis of rotation, side opening position inside the fuselage cover close to forward laser light transmitter is provided with lithium battery, and the both sides relative with forward laser light receiver are evenly arranged with anti-slip veins on the fuselage cover.The utility model is scientific and reasonable for structure, it is safe and convenient to use, balance bubble is provided with laser range finder, when hand is taken and measured, the level of rangefinder can be kept according to balance bubble, reduce error, there is provided bottom generating laser and bottom laser pickoff, the distance of vertical height that now rangefinder is picked up and horizontal direction top of the slope can be measured, calculates the length on slope.
Description
Technical field
The utility model belongs to land survey instrument technical field, and in particular to a kind of land survey telescope-type laser
Rangefinder.
Background technology
Laser range finder, it is the instrument for carrying out Accurate Determining to the distance of target using laser.Laser range finder is working
When to target project a branch of very thin laser, receive the laser beam of target reflection by photoelectric cell, timer determine laser beam from
The time of reception is transmitted into, is calculated from observer's range-to-go.Laser range finder is in light weight, small volume, simple to operate
Speed is fast and accurate, and its error is only the one of 1/5th Dao hundreds of points of other optical rangefinders.
Existing laser range finder exists in use to be not provided with balancing in some defects, such as laser range finder
Bubble, when hand is taken and measured, it is difficult to hold the level of rangefinder, cause to produce error, be not provided with bottom Laser emission
Device and bottom laser pickoff, it has not been convenient to measure the length on slope, do not set to laser generator, receiver and eyepiece is taken
Safeguard measure, easily fall ash, scratch, influence to use.
Utility model content
The purpose of this utility model is to provide a kind of land survey telescope-type laser range finder, to solve the above-mentioned back of the body
It is not provided with balancing bubble on the laser range finder proposed in scape technology, when hand is taken and measured, it is difficult to hold rangefinder
Level, cause to produce error, be not provided with bottom generating laser and bottom laser pickoff, it has not been convenient to measure the length on slope
Degree, laser generator, receiver are not set and eyepiece takes safeguard measure, easily falls ash, is scratched, influence to use asks
Topic.
To achieve the above object, the utility model provides following technical scheme：A kind of land survey telescope-type laser
Rangefinder, including fuselage cover, the side of the fuselage cover are provided with forward laser light receiver, the forward laser light receiver
Side transmitter top cover is connected with by axis of rotation, and be provided with below forward laser light receiver forward laser light transmitting
Device, the side of the forward laser light transmitter are connected with receiver top cover by axis of rotation, and the fuselage cover inside is close
The side opening position of forward laser light transmitter is provided with lithium battery, and the side of the lithium battery is provided with processor, the fuselage
The both sides relative with forward laser light receiver are evenly arranged with anti-slip veins on shell, and on fuselage cover with forward laser light receiver
Symmetrical side is provided with observation eyepiece, and the side of the observation eyepiece is provided with eyepiece cap support frame, the eyepiece cap support
Frame is rotatably connected to eyepiece cap by Damping rotation shaft, and the eyepiece cap is fixed with observation eyepiece by clamping rings and vertical columns
Connect, the side of observation eyepiece is provided with balance bubble on the fuselage cover, is provided with below the balance bubble
Mode switching key, the side of the mode switching key are provided with forward laser light device switch, the side of the forward laser light device switch
It is provided with bottom laser switch, the side opening position on the fuselage cover close to forward laser light receiver is provided with bottom and swashed
Optical transmitting set, the side of the bottom generating laser are provided with bottom laser pickoff, close to observation on the fuselage cover
The side opening position of eyepiece is provided with LCDs, and USB charge ports, the bottom are provided with below the LCDs
The side of generating laser is provided with charging indicator light, and the forward laser light transmitter and forward laser light receiver swash with preposition
Light device switch is electrically connected with, and the bottom generating laser and bottom laser pickoff electrically connect with bottom laser switch
Connect, the processor, forward laser light transmitter, forward laser light receiver, bottom generating laser, bottom laser pickoff, liquid
Crystal display screen and charging indicator light are electrically connected with lithium battery.
Preferably, the forward laser light receiver is rotatablely connected with receiver top cover by Damping rotation shaft.
Preferably, the model Cortex M3 microprocessors of the processor.
Preferably, the anti-slip veins and fuselage cover are integral type structure.
Preferably, the forward laser light transmitter is rotatablely connected with transmitter top cover by Damping rotation shaft.
Compared with prior art, the beneficial effects of the utility model are：The utility model is scientific and reasonable for structure, safe to use
It is convenient, balance bubble is provided with laser range finder, when hand is taken and measured, rangefinder can be kept according to balance bubble
Level, reduce error, there is provided bottom generating laser and bottom laser pickoff, can measure what now rangefinder was picked up
The distance of vertical height and horizontal direction top of the slope, the length on slope is directly calculated by processor, use is more convenient, sets
Receiver top cover, transmitter top cover and eyepiece cap, can anti-falling stop ash, scratch, influence the normal use of rangefinder.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is side view of the present utility model；
Fig. 3 is front view of the present utility model；
Fig. 4 is rearview of the present utility model；
In figure：1- anti-slip veins, 2- fuselage covers, 3- balances bubble, 4- eyepiece caps support frame, 5- Damping rotation shafts, 6- eyepieces
Lid, 7- observations eyepiece, 8- clamping rings, 9- vertical columns, 10- mode switching key, 11- forward laser lights device switch, 12- bottoms are swashed
Light device switch, 13- processors, 14- lithium batteries, 15- forward laser lights transmitter, 16- forward laser lights receiver, 17- bottoms laser
Transmitter, 18- bottoms laser pickoff, 19- LCDs, 20- charging indicator lights, 21-USB charge ports, 22- receivers top
Lid, 23- transmitter top covers.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
Fig. 1-4 are referred to, the utility model provides a kind of technical scheme：A kind of land survey telescope-type laser ranging
Instrument, including fuselage cover 2, the side of fuselage cover 2 are provided with forward laser light receiver 16, the side of forward laser light receiver 16
Transmitter top cover 23 is connected with by axis of rotation, and the lower section of forward laser light receiver 16 is provided with forward laser light transmitter
15, the side of forward laser light transmitter 15 is connected with receiver top cover 22 by axis of rotation, and the inside of fuselage cover 2 is close to preposition
The side opening position of generating laser 15 is provided with lithium battery 14, and the side of lithium battery 14 is provided with processor 13, fuselage cover 2
The upper both sides relative with forward laser light receiver 16 are evenly arranged with anti-slip veins 1, and on fuselage cover 2 with forward laser light receiver
16 symmetrical sides are provided with observation eyepiece 7, and the side of observation eyepiece 7 is provided with eyepiece cap support frame 4, eyepiece cap support frame 4
Eyepiece cap 6 is rotatably connected to by Damping rotation shaft 5, eyepiece cap 6 is fixed with observation eyepiece 7 by clamping rings 8 and vertical columns 9
Connect, the side of observation eyepiece 7 is provided with balance bubble 3 on fuselage cover 2, the lower section of balance bubble 3 is provided with pattern
Switch key 10, the side of mode switching key 10 are provided with forward laser light device switch 11, and the side of forward laser light device switch 11 is set
There is a bottom laser switch 12, the side opening position on fuselage cover 2 close to forward laser light receiver 16 is provided with bottom laser
Transmitter 17, the side of bottom generating laser 17 are provided with bottom laser pickoff 18, close to observation eyepiece on fuselage cover 2
7 side opening position is provided with LCDs 19, and the lower section of LCDs 19 is provided with USB charge ports 21, bottom laser
The side of transmitter 17 is provided with charging indicator light 20, and forward laser light transmitter 15 and forward laser light receiver 16 swash with preposition
Light device switch 11 is electrically connected with, and bottom generating laser 17 and bottom laser pickoff 18 are electrical with bottom laser switch 12
Connection, processor 13, forward laser light transmitter 15, forward laser light receiver 16, bottom generating laser 17, bottom laser pick-off
Device 18, LCDs 19 and charging indicator light 20 are electrically connected with lithium battery 14.
In order that receiver top cover 22 can be with normal use, in the present embodiment, it is preferred that forward laser light receiver 16 is with connecing
Device top cover 22 is received to be rotatablely connected by Damping rotation shaft 5.
In order that this laser range finder can be with normal work, in the present embodiment, it is preferred that the model of processor 13
Cortex M3 microprocessors.
In order that this laser range finder Stability Analysis of Structures, in the present embodiment, it is preferred that anti-slip veins 1 are integrated with fuselage cover 2
Formula structure.
In order that receiver top cover 22 can be with normal use, in the present embodiment, it is preferred that forward laser light transmitter 15 and hair
Emitter top cover 23 is rotatablely connected by Damping rotation shaft 5.
Operation principle and process for using of the present utility model：The land survey is installed well with telescope-type laser range finder
Afterwards, forward laser light device switch 11, eye alignment observation eyepiece 7 are opened, forward laser light transmitter 15 launches laser, runs into measured object
When, laser reflection is returned, and is received by forward laser light receiver 16, you can the distance with testee is drawn, on laser range finder
There is provided balance bubble 3, when hand is taken and measured, can keep the level of rangefinder according to balance bubble 3, reduce and miss
Difference, there is provided bottom generating laser 17 and bottom laser pickoff 18, can measure the vertical height that now rangefinder is picked up
With the distance of horizontal direction top of the slope, the length on slope is directly calculated by processor 13, use is more convenient, and there is provided reception
Device top cover 22, transmitter top cover 23 and eyepiece cap 6, forward laser light transmitter 15, forward laser light receiver 16 can be prevented and seen
Survey eyepiece 7 and fall ash, scratch, influence the normal use of rangefinder.
While there has been shown and described that embodiment of the present utility model, for the ordinary skill in the art,
It is appreciated that these embodiments can be carried out with a variety of changes in the case where not departing from principle of the present utility model and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of land survey telescope-type laser range finder, including fuselage cover（2）, it is characterised in that：Outside the fuselage
Shell（2）Side be provided with forward laser light receiver（16）, the forward laser light receiver（16）Side pass through axis of rotation
It is connected with transmitter top cover（23）, and forward laser light receiver（16）Lower section be provided with forward laser light transmitter（15）, it is described
Forward laser light transmitter（15）Side receiver top cover is connected with by axis of rotation（22）, the fuselage cover（2）It is internal
Close to forward laser light transmitter（15）Side opening position be provided with lithium battery（14）, the lithium battery（14）Side be provided with
Processor（13）, the fuselage cover（2）Upper and forward laser light receiver（16）Relative both sides are evenly arranged with anti-slip veins
（1）, and fuselage cover（2）Upper and forward laser light receiver（16）Symmetrical side is provided with observation eyepiece（7）, the observation mesh
Mirror（7）Side be provided with eyepiece cap support frame（4）, the eyepiece cap support frame（4）Pass through Damping rotation shaft（5）It is rotatably connected to
Eyepiece cap（6）, the eyepiece cap（6）With observing eyepiece（7）Pass through clamping rings（8）And vertical columns（9）It is fixedly connected, it is described
Fuselage cover（2）Upper close observation eyepiece（7）Side be provided with balance bubble（3）, the balance bubble（3）Lower section set
There is mode switching key（10）, the mode switching key（10）Side be provided with forward laser light device switch（11）, it is described preposition sharp
Light device switchs（11）Side be provided with bottom laser switch（12）, the fuselage cover（2）It is upper to be received close to forward laser light
Device（16）Side opening position be provided with bottom generating laser（17）, the bottom generating laser（17）Side be provided with
Bottom laser pickoff（18）, the fuselage cover（2）Upper close observation eyepiece（7）Side opening position be provided with liquid crystal display
Screen（19）, the LCDs（19）Lower section be provided with USB charge ports（21）, the bottom generating laser（17）One
Side is provided with charging indicator light（20）, the forward laser light transmitter（15）With forward laser light receiver（16）And forward laser light
Device switchs（11）It is electrically connected with, the bottom generating laser（17）With bottom laser pickoff（18）Opened with bottom laser
Close（12）It is electrically connected with, the processor（13）, forward laser light transmitter（15）, forward laser light receiver（16）, bottom laser
Transmitter（17）, bottom laser pickoff（18）, LCDs（19）And charging indicator light（20）And lithium battery（14）Electricity
Property connection.
A kind of 2. land survey telescope-type laser range finder according to claim 1, it is characterised in that：It is described preposition
Laser pickoff（16）With receiver top cover（22）Pass through Damping rotation shaft（5）Rotation connection.
A kind of 3. land survey telescope-type laser range finder according to claim 1, it is characterised in that：The processing
Device（13）Model Cortex M3 microprocessors.
A kind of 4. land survey telescope-type laser range finder according to claim 1, it is characterised in that：It is described anti-skidding
Line（1）With fuselage cover（2）For integral type structure.
A kind of 5. land survey telescope-type laser range finder according to claim 1, it is characterised in that：It is described preposition
Generating laser（15）With transmitter top cover（23）Pass through Damping rotation shaft（5）Rotation connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720582292.3U CN207007147U (en) | 2017-05-24 | 2017-05-24 | A kind of land survey telescope-type laser range finder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720582292.3U CN207007147U (en) | 2017-05-24 | 2017-05-24 | A kind of land survey telescope-type laser range finder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207007147U true CN207007147U (en) | 2018-02-13 |
Family
ID=61444657
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720582292.3U Active CN207007147U (en) | 2017-05-24 | 2017-05-24 | A kind of land survey telescope-type laser range finder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207007147U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115031681A (en) * | 2022-08-11 | 2022-09-09 | 盐城发特集团公司 | Simple optical ranging device for land development |
-
2017
- 2017-05-24 CN CN201720582292.3U patent/CN207007147U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115031681A (en) * | 2022-08-11 | 2022-09-09 | 盐城发特集团公司 | Simple optical ranging device for land development |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20200520 Address after: Room 1101 and 1102, building 2, Tian'an headquarters center, No. 555, North Panyu Avenue, Donghuan street, Panyu District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Zhongke Seattle Information Technology Co. Ltd. Address before: Qinyuan road 453400 Jiyuan city Henan city of Zhengzhou province Jinjiang 135 business mansion Patentee before: HENAN HUATAI PLANNING SURVEY AND DESIGN CONSULTING Co.,Ltd. |
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| TR01 | Transfer of patent right |