CN213384757U

CN213384757U - Disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function

Info

Publication number: CN213384757U
Application number: CN202022260496.XU
Authority: CN
Inventors: 刘娣
Original assignee: Wuhan Tianjin Technology Co ltd
Current assignee: Wuhan Tianjin Technology Co ltd
Priority date: 2020-10-13
Filing date: 2020-10-13
Publication date: 2021-06-08
Anticipated expiration: 2030-10-13

Abstract

The utility model discloses a relief of disaster unmanned aerial vehicle with infrared induction intelligent recognition function, which comprises a body, the mounting groove has been seted up to the bottom of body, and the activity chamber has all been seted up to the both sides of mounting groove inner chamber, and the equal swing joint in both sides of body bottom has the push rod. The utility model discloses a promote the push rod, the push rod drives the lug up-motion, the lug can contact with the fixed block when the up-motion, the fixed block receives the extrusion of lug, the fixed block can be to the inner chamber motion of spring pocket, the fixed block breaks away from the joint with the inner chamber in activity chamber, thereby can take out the installation piece from the inner chamber of mounting groove, otherwise insert the inner chamber of mounting groove with the installation piece, the fixed block of both sides extends to the inner chamber in activity chamber, thereby fix installation piece and infrared induction body, it is comparatively fixed to have solved the infrared induction equipment mounting structure that unmanned aerial vehicle used at the disaster relief exploration in-process, consequently, it brings inconvenience to dismantle for the maintenance in later stage, thereby the problem of maintenance work efficiency has been.

Description

Disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a relief of disaster unmanned aerial vehicle with infrared induction intelligent recognition function.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle operated by a radio remote control device and a self-contained program control device, or autonomously, either completely or intermittently, by an on-board computer, a drone is often more suitable for tasks that are too foolproof, dirty, or dangerous than a manned aircraft, the drone being able to operate in a very efficient manner, depending on the field of application, can be divided into for military use and civilian use, for military use aspect, unmanned aerial vehicle divide into reconnaissance aircraft and target drone, at present take photo by plane, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observe wild animal, control infectious disease, survey and drawing, news report, electric power are patrolled and examined, the relief of disaster, the film and television is shot, make romantic field and so on field wide application, great expansion unmanned aerial vehicle's usage itself, the infrared induction equipment mounting structure that unmanned aerial vehicle used in the relief of disaster exploration process is comparatively fixed, consequently, it brings the inconvenience to dismantle for the maintenance in later stage, thereby reduced maintenance work efficiency.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a relief of disaster unmanned aerial vehicle with infrared induction intelligent recognition function possesses the advantage of being convenient for to maintain, has solved that the infrared induction equipment mounting structure that unmanned aerial vehicle used in the relief of disaster exploration process is comparatively fixed, consequently brings inconvenience for the maintenance dismantlement in later stage to the problem of maintaining work efficiency has been reduced.

In order to achieve the above object, the utility model provides a following technical scheme: a disaster relief unmanned aerial vehicle with infrared induction intelligent identification function comprises a body, wherein the bottom of the body is provided with a mounting groove, the two sides of the inner cavity of the mounting groove are both provided with movable cavities, the two sides of the bottom of the body are both movably connected with push rods, the top of the push rod extends to the inner cavity of the movable cavity and is fixedly connected with a lug, the surface of one end of the push rod positioned outside the body is sleeved with a first return spring, the inner cavity of the mounting groove is movably connected with a mounting block, the bottom of the mounting block is fixedly connected with an infrared sensing body, spring grooves are arranged on both sides of the mounting block, the inner cavity of each spring groove is fixedly connected with a second return spring, the other side fixedly connected with baffle of second reset spring, the baffle is kept away from one side fixedly connected with fixed block of second reset spring inner chamber, the fixed block extends to the inner chamber in activity chamber.

Preferably, all the peripheries of the bottom of the body are fixedly connected with supporting legs, and the bottoms of the supporting legs are fixedly connected with cushion pads.

Preferably, the locating slot has all been seted up to the top and the bottom of spring groove inner chamber, the both ends of baffle all extend to the inner chamber of locating slot.

Preferably, a sliding groove is formed in one side of the inner cavity of the movable cavity, a sliding block is connected to the inner cavity of the sliding groove in a sliding mode, and one side, far away from the inner cavity of the sliding groove, of the sliding block is fixedly connected with the protruding block.

Preferably, the top of the first return spring is fixedly connected with the body, and the bottom of the first return spring is fixedly connected with the push rod.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses a promote the push rod, the push rod drives the lug up-motion, the lug can contact with the fixed block when the up-motion, the fixed block receives the extrusion of lug, the fixed block can be to the inner chamber motion of spring pocket, the fixed block breaks away from the joint with the inner chamber in activity chamber, thereby can take out the installation piece from the inner chamber of mounting groove, otherwise insert the inner chamber of mounting groove with the installation piece, the fixed block of both sides extends to the inner chamber in activity chamber, thereby fix installation piece and infrared induction body, it is comparatively fixed to have solved the infrared induction equipment mounting structure that unmanned aerial vehicle used at the disaster relief exploration in-process, consequently, it brings inconvenience to dismantle for the maintenance in later stage, thereby the problem of maintenance work efficiency has been.

2. The utility model discloses a set up the constant head tank, played the spacing effect of baffle, through setting up spout and slider, played the spacing effect of lug.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of a partial cross-sectional structure of the mounting block of the present invention;

fig. 3 is a schematic diagram of a partial enlarged structure of fig. 1 according to the present invention.

In the figure: 1. a body; 2. mounting grooves; 3. a movable cavity; 4. a push rod; 5. a bump; 6. a first return spring; 7. mounting blocks; 8. an infrared sensing body; 9. a spring slot; 10. a second return spring; 11. a baffle plate; 12. a fixed block; 13. a support leg; 14. a cushion pad; 15. positioning a groove; 16. a chute; 17. a slide block.

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.

The utility model discloses a body 1, mounting groove 2, activity chamber 3, push rod 4, lug 5, first reset spring 6, installation piece 7, infrared ray induction body 8, spring groove 9, second reset spring 10, baffle 11, fixed block 12, landing leg 13, blotter 14, constant head tank 15, spout 16 and slider 17 part are the general standard or the part that technical staff in the field knows, and its structure and principle all are this technical staff and all can learn through the technical manual or learn through conventional experimental method.

Referring to fig. 1-3, a disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function comprises a body 1, wherein the periphery of the bottom of the body 1 is fixedly connected with supporting legs 13, the bottom of the supporting legs 13 is fixedly connected with a cushion pad 14, the bottom of the body 1 is provided with an installation groove 2, two sides of the inner cavity of the installation groove 2 are provided with movable cavities 3, two sides of the bottom of the body 1 are movably connected with push rods 4, the top of each push rod 4 extends to the inner cavity of the movable cavity 3 and is fixedly connected with a lug 5, one side of the inner cavity of the movable cavity 3 is provided with a sliding groove 16, the inner cavity of the sliding groove 16 is slidably connected with a sliding block 17, one side of the sliding block 17 away from the inner cavity of the sliding groove 16 is fixedly connected with the lug 5, the surface of one end of the push rod 4 positioned outside the body 1 is sleeved with a first return spring, the inner cavity of the mounting groove 2 is movably connected with a mounting block 7, the bottom of the mounting block 7 is fixedly connected with an infrared sensing body 8, both sides of the mounting block 7 are respectively provided with a spring groove 9, the inner cavity of the spring groove 9 is fixedly connected with a second reset spring 10, the other side of the second reset spring 10 is fixedly connected with a baffle plate 11, the top and the bottom of the inner cavity of the spring groove 9 are respectively provided with a positioning groove 15, both ends of the baffle plate 11 are respectively extended to the inner cavity of the positioning groove 15, one side of the baffle plate 11 far away from the inner cavity of the second reset spring 10 is fixedly connected with a fixed block 12, the fixed block 12 is extended to the inner cavity of the movable cavity 3, the push rod 4 is pushed to drive the lug 5 to move upwards, the lug 5 can be contacted with the fixed block 12 when moving upwards, the fixed block 12 is extruded by the lug 5, the, thereby can take out installation piece 7 from the inner chamber of mounting groove 2, otherwise insert installation piece 7 into the inner chamber of mounting groove 2, the fixed block 12 of both sides extends to the inner chamber of activity chamber 3 to fixing installation piece 7 and infrared ray response body 8, it is comparatively fixed to have solved the infrared induction equipment mounting structure that unmanned aerial vehicle used in the disaster relief exploration process, consequently dismantles the inconvenience of bringing for the maintenance in later stage, thereby has reduced the problem of maintaining work efficiency.

During the use, through promoting push rod 4, push rod 4 drives lug 5 upward movement, lug 5 can contact with fixed block 12 when the upward movement, fixed block 12 receives the extrusion of lug 5, fixed block 12 can be to the inner chamber motion of spring groove 9, fixed block 12 breaks away from the joint with the inner chamber in activity chamber 3, thereby can take out installation piece 7 from the inner chamber of mounting groove 2, otherwise insert the inner chamber of mounting groove 2 with installation piece 7, the fixed block 12 of both sides extends to the inner chamber in activity chamber 3, thereby fix installation piece 7 and infrared sensing body 8, it is comparatively fixed to have solved the infrared sensing equipment mounting structure that unmanned aerial vehicle used at the disaster relief exploration in-process, consequently, it brings inconvenience to dismantle for the maintenance in later stage, thereby the problem of maintenance work efficiency has been reduced.

The standard parts used in the present application document can be purchased from the market, and can be customized according to the description of the specification and the accompanying drawings, the specific connection mode of each part adopts the conventional means of mature bolt, rivet, welding and the like in the prior art, the machines, parts and equipment adopt the conventional models in the prior art, the control mode is automatically controlled by a controller, the control circuit of the controller can be realized by simple programming of technicians in the field, the control circuit belongs to the common knowledge in the field, and the present application document is mainly used for protecting mechanical devices, so the control mode and the circuit connection are not explained in detail in the present application.

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

1. The utility model provides a relief of disaster unmanned aerial vehicle with infrared induction intelligent recognition function, includes body (1), its characterized in that: the bottom of the body (1) is provided with a mounting groove (2), both sides of an inner cavity of the mounting groove (2) are provided with movable cavities (3), both sides of the bottom of the body (1) are movably connected with push rods (4), the tops of the push rods (4) extend to the inner cavity of the movable cavities (3) and are fixedly connected with lugs (5), the surface of one end, located outside the body (1), of each push rod (4) is sleeved with a first reset spring (6), the inner cavity of the mounting groove (2) is movably connected with a mounting block (7), the bottom of the mounting block (7) is fixedly connected with an infrared sensing body (8), both sides of the mounting block (7) are provided with spring grooves (9), the inner cavity of each spring groove (9) is fixedly connected with a second reset spring (10), and the other side of each second reset spring (10) is fixedly connected with a baffle (11, one side fixedly connected with fixed block (12) of baffle (11) keep away from second reset spring (10) inner chamber, fixed block (12) extend to the inner chamber in activity chamber (3).

2. The disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function of claim 1, characterized in that: all fixedly connected with landing leg (13) around body (1) bottom, the bottom fixedly connected with blotter (14) of landing leg (13).

3. The disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function of claim 1, characterized in that: constant head tank (15) have all been seted up to the top and the bottom of spring groove (9) inner chamber, the both ends of baffle (11) all extend to the inner chamber of constant head tank (15).

4. The disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function of claim 1, characterized in that: one side of the inner cavity of the movable cavity (3) is provided with a sliding groove (16), the inner cavity of the sliding groove (16) is connected with a sliding block (17) in a sliding manner, and one side, far away from the inner cavity of the sliding groove (16), of the sliding block (17) is fixedly connected with the bump (5).

5. The disaster relief unmanned aerial vehicle with infrared induction intelligent recognition function of claim 1, characterized in that: the top of the first return spring (6) is fixedly connected with the body (1), and the bottom of the first return spring (6) is fixedly connected with the push rod (4).