CN213705815U

CN213705815U - Land space planning terrain measuring device

Info

Publication number: CN213705815U
Application number: CN202022899786.9U
Authority: CN
Inventors: 孙渊
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-12-03
Filing date: 2020-12-03
Publication date: 2021-07-16
Anticipated expiration: 2030-12-03

Abstract

The utility model discloses a territory measuring device of territory space planning relates to the topographic survey technical field. The utility model discloses an aircraft body, aircraft body's bottom is provided with the camera and is located a pair of support that is parallel to each other on camera both sides, two all set up on the support along its length direction's T shape spout, still including setting up respectively two pairs of rectangular of support below are every right all construct on rectangular with the T shape sliding part of T shape spout looks adaptation. The utility model discloses compare in the in-process that the aircraft among the current national soil space planning topography measuring device was flying, often can meet the barrier, the camera suffers the problem that the striking damaged easily and has carried out the improvement, mutually supports through support, T shape spout, rectangular, T shape sliding part, flexible loop bar and reset spring between one to reach the aircraft and carry out fine guard action to the camera at the flight in-process.

Description

Land space planning terrain measuring device

Technical Field

The utility model relates to a topographic survey technical field, concretely relates to territory measuring device of national soil space planning.

Background

At present, management departments of land, planning, forestry, oceans and the like are not linked in place in management due to various reasons, so that the conflict of land planning, city planning, ecological environmental protection planning, ocean zoning and other related industries in a coastline area is large, different purposes are arranged for the same area by each planning, national resources of China lack a unified data information management and application platform, the informatization of the national resource industry is still in a stage of distributed deployment of service systems according to regions at present, a plurality of service systems lack integral linking, aerial photography or unmanned aerial vehicle shooting topographic maps are adopted for national measurement and collection in many times, and a satellite remote sensing technology can also be adopted.

At present, current unmanned aerial vehicle is at the flight in-process, often can meet the barrier, if fly carelessly, the camera suffers the striking and damages, seriously influences the homeland space topography and shoots measuring work, leads to it to have a great deal of unreliability in the use, and the practicality is relatively poor, in order to avoid the emergence of this kind of condition, the utility model provides a homeland space planning topography measuring device with bradyseism effect.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a: for solving the problem that unmanned aerial vehicle suffered the striking damage easily at flight in-process camera, the utility model provides a land and soil space planning topography measuring device.

The utility model discloses a realize above-mentioned purpose and specifically adopt following technical scheme:

the utility model provides a territory measuring device of national soil space planning, includes the aircraft body, the bottom of aircraft body is provided with the camera and is located a pair of support that is parallel to each other on camera both sides, two all set up the T shape spout along its length direction on the support, still including setting up respectively two pairs of rectangular of support below are every to all construct on the strip with the T shape sliding part of T shape spout looks adaptation is to form the edge the length direction of support removes, two the both ends of T shape spout all be fixed with flexible loop bar and cover and establish the outside reset spring of flexible loop bar, two the free end of flexible loop bar and reset spring is respectively with two the T shape sliding part is fixed.

Further, every is every the rectangular one end of keeping away from T shape sliding part all articulates there is the regulation pole, two the free end of adjusting the pole articulates there is the bearing frame.

Furthermore, two the top of bearing the frame all constructs along its length direction's slot, the both ends of slot are fixed with the bull stick, the both ends of slot all are fixed with the cover and establish the outside reset spring two of bull stick, two the free end of reset spring two all is fixed with the movable sleeve and establishes the regulating block on the bull stick, two the regulating block respectively with two the free end of adjusting the pole is articulated.

Further, the bottom of bearing frame all installs the piece of falling to the ground two.

Further, the land falling block is sleeved with a rubber sleeve.

Further, a transparent protective sleeve is arranged outside the camera.

The utility model has the advantages as follows:

1. the utility model discloses compare in the in-process that the aircraft among the current national soil space planning topography measuring device was flying, often can meet the barrier, the camera suffers the problem that the striking damaged easily and has carried out the improvement, mutually supports through support, T shape spout, rectangular, T shape sliding part, flexible loop bar and reset spring between one to reach the aircraft and carry out fine guard action to the camera at the flight in-process.

Drawings

FIG. 1 is a perspective view of the present invention;

FIG. 2 is an enlarged schematic view of the structure at the point I in FIG. 1 according to the present invention;

FIG. 3 is another perspective view of the present invention;

reference numerals: 1. an aircraft body; 2. a camera; 3. a support; 4. a T-shaped chute; 5. a strip; 6. a T-shaped sliding part; 7. a telescopic loop bar; 8. a first return spring; 9. adjusting a rod; 10. a carrier; 11. a trench; 12. a rotating rod; 13. a second return spring; 14. an adjusting block; 15. a land falling block; 16. a rubber sleeve; 17. a transparent protective sleeve.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures. Furthermore, the terms "first," "second," and the like are used merely to distinguish one description from another, and are not to be construed as indicating or implying relative importance.

In the description of the embodiments of the present invention, it should be noted that the terms "inside", "outside", "up", and the like indicate the directions or positional relationships based on the directions or positional relationships shown in the drawings, or the directions or positional relationships that the products of the present invention are conventionally placed when used, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the device or element to which the term refers must have a specific direction, be constructed and operated in a specific direction, and thus, should not be construed as limiting the present invention.

As shown in fig. 1-3, an embodiment of the utility model provides a territory measuring device is planned in homeland space, including aircraft body 1, aircraft body 1's bottom is provided with camera 2 and a pair of support 3 that is parallel to each other that is located camera 2 both sides, all set up on two supports 3 along its length direction's T shape spout 4, still include two pairs of rectangular 5 that set up respectively in two supports 3 below, every T shape sliding part 6 with T shape spout 4 looks adaptation is all constructed on rectangular 5, move in order to form the length direction along support 3, the both ends of two T shape spouts 4 all are fixed with flexible loop bar 7 and cover and establish the reset spring 8 outside flexible loop bar 7, the free end of two flexible loop bars 7 and reset spring 8 is fixed with two T shape sliding parts 6 respectively, to often meeting the barrier in the in-process of shooting in flight to planning territory measuring device in the existing homeland space and leading to camera 2 to suffer easily The problem of striking damage has been optimized, installs camera 2 in aircraft body 1's below, and be provided with support 3 on camera 2's both sides, when aircraft body 1 shoots aloft when measuring, if the barrier has been met to the fruit, rectangular 5 can slow down the impact force that the striking brought under the effect of telescopic loop bar 7 and reset spring 8, in order to reach the protection to camera 2, here in order to guarantee rectangular 5 can be smooth realization bradyseism's effect, the utility model discloses T shape spout 4 has been seted up on support 3 to construct the T shape sliding part 6 with 4 looks adaptations of T shape spout on rectangular 5, remove with the length direction who forms along support 3, structural design is simple reasonable, convenient operation, and the practicality is strong.

As shown in fig. 1, every one end of rectangular 5 far away from T shape sliding part 6 all articulates there is the regulation pole 9, and two free ends of adjusting pole 9 articulate there is a frame 10, in order to further increase the bradyseism nature of device, the utility model discloses every one end of rectangular 5 far away from T shape sliding part 6 all articulates there is the regulation pole 9 to two free ends of adjusting pole 9 articulate there is a frame 10, and frame 10 here not only can guarantee the bradyseism nature of device when flight in the air, also can guarantee simultaneously that the device carries out absorbing effect to the device when descending.

As shown in fig. 1-2, the top ends of the two loading ledges 10 are each configured with a groove 11 along the length direction thereof, two ends of the groove 11 are each fixed with a rotating rod 12, two ends of the groove 11 are each fixed with a second return spring 13 sleeved outside the rotating rod 12, the free ends of the two second return springs 13 are each fixed with an adjusting block 14 movably sleeved on the rotating rod 12, the two adjusting blocks 14 are respectively hinged with the free ends of the two adjusting rods 9, in order to further increase the practicability of the device, the utility model is provided with grooves 11 on the top of the two bearing plates, and rotating rods 12 are fixed on the two ends of the grooves 11, two ends of the groove 11 are fixed with two return springs 13 which are sleeved on the rotating rod 12, free ends of the two return springs 13 are respectively fixed with an adjusting block 14 which is sleeved on the rotating rod 12 in a sliding way, the adjusting block 14 and the free end of the adjusting rod 9 are hinged here, so that a better damping effect of the aircraft body 1 in the event of an impact is achieved.

As shown in fig. 1 and 3, the landing blocks 15 are installed at the bottom ends of the two bearing frames 10, and the landing blocks 15 are installed at the bottom ends of the two bearing frames 10, wherein the number of the landing blocks 15 on each bearing plate should be not less than two, so as to ensure that the device is more stable when landing.

As shown in fig. 3, the cover is equipped with rubber sleeve 16 on the piece 15 that falls to the ground, in order to further increase the stability of device when falling to the ground, the utility model discloses the cover is equipped with rubber sleeve 16 on the piece 15 that falls to the ground, increases the frictional force of the piece 15 that falls to the ground when with ground contact, improves stability.

As shown in fig. 3, camera 2 is provided with transparent protective sheath 17 outside, for further protecting camera 2, the utility model discloses be provided with transparent protective sheath 17 in camera 2's outside.

Claims

1. The utility model provides a land and soil space planning topography survey device, includes aircraft body (1), its characterized in that, the bottom of aircraft body (1) is provided with camera (2) and is located a pair of support (3) that are parallel to each other on camera (2) both sides, two all set up T shape spout (4) along its length direction on support (3), still including setting up respectively two pairs of rectangular (5) of support (3) below, every it is every all to construct on rectangular (5) with T shape sliding part (6) of T shape spout (4) looks adaptation, in order to form the edge the length direction of support (3) removes, two the both ends of T shape spout (4) all be fixed with flexible loop bar (7) and cover and establish the outside reset spring one (8) of flexible loop bar (7), two the free end of flexible loop bar (7) and reset spring one (8) respectively with two T shape sliding part (6) are fixed.

2. A geodetic space planning geodetic measuring device according to claim 1, characterized in that the end of each pair of said strips (5) remote from said T-shaped slide (6) is hinged with an adjusting lever (9), the free ends of both said adjusting levers (9) being hinged with a bearing carriage (10).

3. A territorial survey device for territorial planning in territorial space according to claim 2, wherein the top ends of the two bearing frames (10) are respectively provided with a groove (11) along the length direction thereof, rotating rods (12) are fixed at two ends of the groove (11), a second return spring (13) sleeved outside the rotating rods (12) is fixed at two ends of the groove (11), adjusting blocks (14) movably sleeved on the rotating rods (12) are fixed at free ends of the two second return springs (13), and the two adjusting blocks (14) are respectively hinged with the free ends of the two adjusting rods (9).

4. A geospatial planning geodetic surveying device according to claim 2, characterised in that the bottom ends of both carriages (10) are fitted with landings (15).

5. A territorial measuring device for territorial space planning according to claim 4, characterized in that the landmass (15) is sleeved with a rubber sleeve (16).

6. A geodetic space planning topographical measuring device according to claim 1, characterized in that a transparent protective sleeve (17) is provided externally of the camera head (2).