CN211954169U - Total powerstation of airport engineering survey and drawing usefulness - Google Patents
Total powerstation of airport engineering survey and drawing usefulness Download PDFInfo
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- CN211954169U CN211954169U CN202021166455.8U CN202021166455U CN211954169U CN 211954169 U CN211954169 U CN 211954169U CN 202021166455 U CN202021166455 U CN 202021166455U CN 211954169 U CN211954169 U CN 211954169U
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Abstract
The utility model discloses a total powerstation of airport engineering survey and drawing usefulness, including the total powerstation main part, the both sides of total powerstation main part all are provided with the protection curb plate, and the protection curb plate comprises a plurality of modules, the protection curb plate is assembled to two following station activities and sets up: the total station main body is inclined towards the X-axis horizontal direction, and any one side protective side plate is stressed and kept elastically contracting towards one side of the total station main body; and a second station, wherein the total station main body is inclined towards the Y-axis horizontal direction, and one side of any one of the two protection side plates is stressed to form stepped shock absorption. This total powerstation of airport engineering survey and drawing usefulness can be impacted and empty to X axle horizontal direction and when empting to Y axle horizontal direction by the air current of both sides at the total powerstation main part, cushions the impact force through buffer gear between total powerstation main part and the protection curb plate and through the protection machanism that protection curb plate both sides set up to the total powerstation main part does not receive the damage.
Description
Technical Field
The utility model relates to an airport engineering survey and drawing technical field specifically is a total powerstation of airport engineering survey and drawing usefulness.
Background
The total station for surveying and mapping airport engineering is a high-tech measuring instrument integrating light, machine and electricity into one body, and is a surveying and mapping instrument system integrating horizontal angle, vertical angle, distance (slant distance and flat distance) and height difference measuring functions into one body. Compared with the optical theodolite, the electronic theodolite changes the optical scale into the photoelectric scanning scale, and replaces manual optical micrometer reading with automatic recording and displaying reading, so that the angle measurement operation is simplified, and the generation of reading errors can be avoided. And the whole measurement work of the airport can be completed by arranging the instrument once.
However, in the use process of the existing total station for airport engineering surveying and mapping, the fact that an airplane frequently takes off and lands in an airport, strong airflow is caused when the airplane takes off and lands, and the total station is impacted, and the total station is easily toppled and damaged under the impact force of the airflow due to strong wind resistance in the horizontal direction of two sides of the total station.
In order to solve the problems, innovative design is urgently needed on the basis of the original total station for mapping airport engineering.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a total powerstation of airport engineering survey and drawing usefulness to the strong air current that the total powerstation of proposing current airport engineering survey and drawing usefulness among the solution above-mentioned background art arouses when the aircraft takes off and descends strikes and lacks buffer gear down, and lacks protector's problem when toppling over under the air current impact force.
Technical scheme
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a total powerstation of airport engineering survey and drawing usefulness, includes the total powerstation main part, the both sides of total powerstation main part all are provided with the protection curb plate, and the protection curb plate comprises a plurality of modules, the protection curb plate is assembled to two following station activities and sets up: the total station main body is inclined towards the X-axis horizontal direction, and any one side protective side plate is stressed and kept elastically contracting towards one side of the total station main body; and a second station, wherein the total station main body is inclined towards the Y-axis horizontal direction, and one side of any one of the two protection side plates is stressed to form stepped shock absorption.
Preferably, the total powerstation main part with be provided with buffer gear between the protection curb plate, buffer gear includes buffer block and buffer beam, the dashpot has been seted up to the inside of buffer block, the one end of buffer beam runs through and extends to the inside of dashpot, the other end of buffer beam with the inner wall of protection curb plate is connected.
Preferably, buffer gear still includes stopper and reset spring, stopper fixed mounting in the buffer beam is located one of dashpot is served, and the opposite side with be provided with between the inner wall of dashpot reset spring.
Preferably, both sides of the protection side plate are provided with protection mechanisms, each protection mechanism comprises a connecting block, a protection block and a sliding block, a plurality of connecting blocks are movably arranged between the protection side plate and the protection blocks, a sliding groove is formed in one end of each connecting block, the sliding block is arranged at the other end of each connecting block, and the connecting blocks are connected in the sliding groove in a pairwise mode through the sliding blocks in an inserting mode.
Preferably, the protection mechanism further comprises a first pressure spring, a second pressure spring and a rubber sleeve, the first pressure spring and the second pressure spring are symmetrically arranged between the sliding block and the inner wall of the sliding groove, and the rubber sleeve is fixedly mounted on the outer wall of the protection block.
Preferably, the top of total powerstation main part is provided with protection mechanism, protection mechanism includes protective bracket and protection roof, protective bracket fixed mounting in the top of total powerstation main part, and top fixed mounting have the protection roof.
Compared with the prior art, the beneficial effects of the utility model are that:
1. this total powerstation of airport engineering survey and drawing usefulness adopts the mode that sets up the protection curb plate in the both sides of total powerstation main part, can be in order to receive the air current of both sides to strike and when empting to X axle horizontal direction at the total powerstation main part, cushion the impact force with protection total powerstation main part not damaged through buffer gear between total powerstation main part and the protection curb plate.
2. This total powerstation of airport engineering survey and drawing usefulness adopts the mode that sets up protection mechanism in the both sides of protection curb plate, can be in order to receive the air current of both sides to strike and when toppling over to Y axle horizontal direction at the total powerstation main part, the protection mechanism through protection curb plate both sides setting cushions the impact force in order to protect the total powerstation main part not to receive the damage.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the disclosure.
This document provides an overview of various implementations or examples of the technology described in this disclosure, and is not a comprehensive disclosure of the full scope or all features of the disclosed technology.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic front sectional view of the present invention;
FIG. 3 is a schematic top view of the present invention;
fig. 4 is an enlarged schematic view of a point a in fig. 3 according to the present invention.
In the figure: 1. a total station body; 2. a buffer block; 3. a buffer tank; 4. a buffer rod; 5. a limiting block; 6. a return spring; 7. a protective side plate; 8. connecting blocks; 9. a chute; 10. a protection block; 11. a slider; 12. a first pressure spring; 13. a second pressure spring; 14. a rubber sleeve; 15. a protective bracket; 16. a protective roof; 17. a buffer mechanism; 18. a protection mechanism; 19. and a protection mechanism.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Unless otherwise defined, technical or scientific terms used herein shall have the ordinary meaning as understood by one of ordinary skill in the art to which this disclosure belongs. The use of the word "comprising" or "comprises", and the like, in this disclosure is intended to mean that the elements or items listed before that word, include the elements or items listed after that word, and their equivalents, without excluding other elements or items. The terms "connected" or "coupled" and the like are not restricted to physical or mechanical connections, but may also include electrical connections, whether direct or indirect. "upper", "lower", "left", "right", and the like are used merely to indicate relative positional relationships, and when the absolute position of the object being described is changed, the relative positional relationships may also be changed accordingly.
To maintain the following description of the embodiments of the present disclosure clear and concise, a detailed description of known functions and known components have been omitted from the present disclosure.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a total powerstation of airport engineering survey and drawing usefulness, includes total powerstation main part 1, the both sides of total powerstation main part 1 all are provided with protection curb plate 7, and protection curb plate 7 comprises a plurality of modules, and protection curb plate 7 is assembled for following two station activities and sets up: in the first station, the total station main body 1 is inclined towards the X-axis horizontal direction, and the protective side plate 7 on any one side is stressed and kept elastically contracting towards one side of the total station main body 1; and a second station, wherein the total station main body 1 is inclined towards the Y-axis horizontal direction, one side of any one of the two protection side plates 7 is stressed to form a stepped shock absorber, namely, when the total station main body 1 is impacted by airflow at two sides and inclined towards the X-axis horizontal direction and inclined towards the Y-axis horizontal direction, the impact force is buffered through a buffer mechanism 17 between the total station main body 1 and the protection side plates 7 and a protection mechanism 18 arranged at two sides of the protection side plates 7, so that the total station main body 1 is protected from being damaged.
As shown in fig. 1 and 2, be provided with buffer gear 17 between total powerstation main part 1 and the protection curb plate 7, buffer gear 17 includes buffer block 2 and buffer beam 4, buffer slot 3 has been seted up to buffer block 2's inside, the one end of buffer beam 4 runs through and extends to the inside of buffer slot 3, the other end of buffer beam 4 is connected with the inner wall of protection curb plate 7, when the air current was too big and drive total powerstation main part 1 and empty to the X axle horizontal direction, protection curb plate 7 that total powerstation main part 1 both sides set up at first contacts to ground, protection curb plate 7 drives the buffer slot 3 internalization that buffer beam 4 that the inboard set up was seted up in buffer block 2 this moment.
Wherein, buffer gear 17 still includes stopper 5 and reset spring 6, stopper 5 fixed mounting is served in buffer beam 4 is located dashpot 3, and be provided with reset spring 6 between the inner wall of opposite side and dashpot 3, when buffer beam 4 that protection curb plate 7 drove the inboard setting during the dashpot 3 internalization of seting up in buffer block 2, accessible stopper 5 compresses reset spring 6, can cushion the impact force that protection curb plate 7 conducted to protect total powerstation main part 1 not damaged.
As shown in fig. 1-4, both sides of the protective side plate 7 are provided with protective mechanisms 18, each protective mechanism 18 comprises a connecting block 8, a protective block 10 and a sliding block 11, a plurality of connecting blocks 8 are movably arranged between the protective side plate 7 and the protective block 10, one end of each connecting block 8 is provided with a sliding groove 9, the other end of each connecting block 8 is provided with a sliding block 11, the connecting blocks 8 are connected in pairs in the sliding grooves 9 through the sliding blocks 11 in an inserting manner, when the total station main body 1 is inclined towards the Y-axis horizontal direction, the protective side plates 7 arranged at two sides of the total station main body 1 firstly contact the ground, at the moment, the protective blocks 10 arranged at two sides of the protective side plates 7 firstly contact the ground, the impact force is primarily buffered through the rubber sleeve 14 arranged on the surface, meanwhile, the protective block 10 pulls the first compression spring 12 through the sliding groove 9 formed in the connecting block 8 through the sliding block 11 and compresses the second compression spring 13 to buffer the impact force again.
Wherein, protection machanism 18 still includes first pressure spring 12, second pressure spring 13 and rubber sleeve 14, the symmetry is provided with first pressure spring 12 and second pressure spring 13 between the inner wall of slider 11 and spout 9, fixed mounting has rubber sleeve 14 on the outer wall of protective block 10, slider 11 through connecting block 8 opposite side draws first pressure spring 12 and compresses in order to cushion the impact force once more in the spout 9 pulling that adjacent connecting block 8 is inside to second pressure spring 13, connecting block 8 through a plurality of quantity is fallen the impact force buffering, can be in order to protect total powerstation main part 1 not to receive the damage.
Further, as shown in fig. 1, a protection mechanism 19 is disposed at the top end of the total station main body 1, the protection mechanism 19 includes a protection support 15 and a protection top plate 16, the protection support 15 is fixedly mounted at the top end of the total station main body 1, and the protection top plate 16 is fixedly mounted at the top end of the total station main body 1, the protection top plate 16 disposed at the top end of the total station main body 1 enables an airflow to flow through, so as to generate a downward pressure to enhance the stability of the total station main body 1, and at the same time, the airflow can be prevented from bringing small stones into the air to fall and hit the total station main.
The working principle is as follows: when the present arrangement is used, as shown in figures 1-3, when the total station body 1 is impacted by an airflow generated by the take-off and landing of an airport aircraft, the airflow can be divided by the protective side plates 7 arranged on the two sides, and the airflow flows through the total station main body 1 from the two sides of the protective side plates 7, meanwhile, a downward pressure is generated when the airflow passes through the top-arranged protective top plate 16 so as to enhance the stability of the total station main body 1, when the total station main body 1 is driven to tilt towards the X-axis horizontal direction due to overlarge airflow, the protective side plates 7 arranged at the two sides of the total station main body 1 firstly contact the ground, at the moment, the protective side plates 7 drive the buffer rods 4 arranged at the inner sides to move in the buffer grooves 3 arranged in the buffer blocks 2, and the return springs 6 are compressed through the limiting blocks 5, the impact force conducted by the protective side plate 7 can be buffered to protect the total station main body 1 from being damaged.
As shown in fig. 1-4, when the airflow is too large to drive the total station main body 1 to tilt to the Y-axis horizontal direction, the protective side plates 7 disposed on both sides of the total station main body 1 first contact the ground, at this time, the protective blocks 10 disposed on both sides of the protective side plates 7 first contact the ground, and primarily buffer the impact force through the rubber sleeves 14 disposed on the surface, meanwhile, the protective blocks 10 pull the first compression springs 12 through the chutes 9 formed in the connecting blocks 8 by the sliders 11 and compress the second compression springs 13 to buffer the impact force again, pull the first compression springs 12 through the chutes 9 formed in the adjacent connecting blocks 8 by the sliders 11 on the other side of the connecting blocks 8 and compress the second compression springs 13 to buffer the impact force again, and buffer the impact force through a plurality of connecting blocks 8, so as to protect the total station main body 1 from being damaged.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a total powerstation of airport engineering survey and drawing usefulness, includes total powerstation main part (1), its characterized in that:
the both sides of total powerstation main part (1) all are provided with protection curb plate (7), and protection curb plate (7) comprise a plurality of modules, protection curb plate (7) are assembled for following two station activities and set up: the total station main body (1) is inclined towards the X-axis horizontal direction, and any one side protection side plate (7) is stressed and kept to elastically contract towards one side of the total station main body (1); and a second station, wherein the total station main body (1) is inclined towards the Y-axis horizontal direction, and one side of each of the two protection side plates (7) is stressed to form stepped shock absorption.
2. The total station for mapping of airport engineering of claim 1, wherein: total powerstation main part (1) with be provided with buffer gear (17) between protection curb plate (7), buffer gear (17) are including buffer block (2) and buffer beam (4), buffer slot (3) have been seted up to the inside of buffer block (2), the one end of buffer beam (4) is run through and is extended to the inside of buffer slot (3), the other end of buffer beam (4) with the inner wall of protection curb plate (7) is connected.
3. A total station for airport engineering surveying according to claim 2, wherein: buffer gear (17) still include stopper (5) and reset spring (6), stopper (5) fixed mounting in buffer pole (4) are located one in buffer slot (3) is served, and the opposite side with be provided with between the inner wall of buffer slot (3) reset spring (6).
4. The total station for mapping of airport engineering of claim 1, wherein: both sides of protection curb plate (7) all are provided with protection machanism (18), protection machanism (18) are including connecting block (8), protection piece (10) and slider (11), protection curb plate (7) with the activity is provided with a plurality of quantity between protection piece (10) connecting block (8), spout (9) have been seted up to the one end of connecting block (8), the other end of connecting block (8) is provided with slider (11), pass through between connecting block (8) slider (11) peg graft in two liang link to each other in spout (9).
5. The total station for mapping of airport engineering according to claim 4, wherein: protection machanism (18) still include first pressure spring (12), second pressure spring (13) and rubber sleeve (14), slider (11) with the symmetry is provided with first pressure spring (12) and second pressure spring (13) between the inner wall of spout (9), fixed mounting has on the outer wall of protection piece (10) rubber sleeve (14).
6. The total station for mapping of airport engineering of claim 1, wherein: the top of total powerstation main part (1) is provided with protection mechanism (19), protection mechanism (19) are including protection support (15) and protection roof (16), protection support (15) fixed mounting in the top of total powerstation main part (1), and top fixed mounting have protection roof (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021166455.8U CN211954169U (en) | 2020-06-22 | 2020-06-22 | Total powerstation of airport engineering survey and drawing usefulness |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021166455.8U CN211954169U (en) | 2020-06-22 | 2020-06-22 | Total powerstation of airport engineering survey and drawing usefulness |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211954169U true CN211954169U (en) | 2020-11-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021166455.8U Expired - Fee Related CN211954169U (en) | 2020-06-22 | 2020-06-22 | Total powerstation of airport engineering survey and drawing usefulness |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211954169U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112945215A (en) * | 2021-02-25 | 2021-06-11 | 邵成坤 | Anti-reflection total station convenient to adjust |
| CN114659508A (en) * | 2022-04-13 | 2022-06-24 | 黄石市久弘测绘有限公司 | Total powerstation is used in engineering survey and drawing with shock attenuation and buffer gear |
-
2020
- 2020-06-22 CN CN202021166455.8U patent/CN211954169U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112945215A (en) * | 2021-02-25 | 2021-06-11 | 邵成坤 | Anti-reflection total station convenient to adjust |
| CN114659508A (en) * | 2022-04-13 | 2022-06-24 | 黄石市久弘测绘有限公司 | Total powerstation is used in engineering survey and drawing with shock attenuation and buffer gear |
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| 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: 20201117 Termination date: 20210622 |
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| CF01 | Termination of patent right due to non-payment of annual fee |