CN111559503B - Unmanned aerial vehicle body temperature measuring device and method for smart city - Google Patents
Unmanned aerial vehicle body temperature measuring device and method for smart city Download PDFInfo
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- CN111559503B CN111559503B CN202010458879.XA CN202010458879A CN111559503B CN 111559503 B CN111559503 B CN 111559503B CN 202010458879 A CN202010458879 A CN 202010458879A CN 111559503 B CN111559503 B CN 111559503B
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- 230000036760 body temperature Effects 0.000 title claims abstract description 21
- 238000000034 method Methods 0.000 title claims abstract description 14
- 230000003139 buffering effect Effects 0.000 claims abstract description 20
- 230000009471 action Effects 0.000 claims description 7
- 238000009529 body temperature measurement Methods 0.000 claims description 7
- 230000000149 penetrating effect Effects 0.000 claims description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61B—DIAGNOSIS; SURGERY; IDENTIFICATION
- A61B5/00—Measuring for diagnostic purposes; Identification of persons
- A61B5/01—Measuring temperature of body parts ; Diagnostic temperature sensing, e.g. for malignant or inflamed tissue
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01J—MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
- G01J5/00—Radiation pyrometry, e.g. infrared or optical thermometry
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01K—MEASURING TEMPERATURE; MEASURING QUANTITY OF HEAT; THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR
- G01K13/00—Thermometers specially adapted for specific purposes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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Abstract
The invention discloses an unmanned aerial vehicle body temperature measuring device and method for a smart city, and the device comprises an unmanned aerial vehicle main body, a temperature measurer body, a telescopic assembly, a protection assembly, a buffer assembly, supporting legs and a temperature measurer body mounting seat, wherein the temperature measurer body is mounted on the outer wall of the bottom end of the unmanned aerial vehicle main body; the unmanned aerial vehicle has the advantages that the telescopic assembly, the protection assembly and the buffer assembly are adopted, and the first sliding block, the second connecting rod, the first telescopic rod, the limiting baffle, the second spring, the second sliding block and the third connecting rod in the telescopic assembly are matched, so that the unmanned aerial vehicle has a telescopic function, is simple in structure and convenient to operate, and occupies a small space; the unmanned aerial vehicle has the protection function due to the matching of the second sleeve, the fan, the connecting plate and the third sleeve in the protection assembly; second telescopic link, third spring and buffer stop's cooperation in the buffering subassembly makes this unmanned aerial vehicle have buffering safeguard function, has further protected this unmanned aerial vehicle, has improved this unmanned aerial vehicle's life.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle body temperature measuring device and method for a smart city.
Background
In recent years, due to the occurrence of a plurality of large-scale infectious diseases, a plurality of contactless body temperature measuring devices are used in large quantity, so that the unmanned aerial vehicle body temperature measuring device has certain requirements in the market; but current unmanned aerial vehicle body temperature measuring device structure is complicated, the operation difficulty, most unmanned aerial vehicles can not fold or stretch out and draw back, can not portable, do not set up protector on most unmanned aerial vehicle fans, make the fan damage easily, hinder the crowd easily, and most unmanned aerial vehicles do not have buffer, have reduced unmanned aerial vehicle's life, influence the use.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle body temperature measuring device and method for a smart city, and aims to solve the problems in the background technology.
In order to solve the technical problems, the invention provides the following technical scheme: the unmanned aerial vehicle body temperature measuring device for the smart city comprises an unmanned aerial vehicle main body, a temperature measuring device body, a telescopic assembly, a protection assembly, a buffering assembly, supporting legs and a temperature measuring device body mounting seat, wherein the temperature measuring device body is mounted on the outer wall of the bottom end of the unmanned aerial vehicle main body;
the telescopic assembly comprises a first sliding chute, a first sliding block, a first spring, a first connecting rod, a second sliding chute, a second connecting rod, a first sleeve, a first telescopic rod, a limiting hole, a limiting baffle, a second spring, a second sliding block, a third sliding chute, a third connecting rod and a limiting retainer ring, the first sliding chute is formed in the outer wall of the top end of the unmanned aerial vehicle main body, the first sliding block is connected to the inner wall of one side of the first sliding chute in a sliding mode, the first spring is sleeved on the outer wall of one side of the first sliding block, the second sliding chute is formed in the outer wall of one side of the unmanned aerial vehicle main body and corresponds to the outer wall of the bottom end of the first sliding block in a penetrating mode, the first connecting rod is connected to the inner wall of one side of the second sliding chute in a sliding mode, the outer wall of one side of the first connecting rod is fixedly connected to the outer wall of the bottom end of the first sliding block, and the outer wall of one end of the first connecting rod is fixedly connected to the second connecting rod, the outer side of the unmanned aerial vehicle main body is fixedly connected with a first sleeve, the outer side of the unmanned aerial vehicle main body is fixedly connected with a first telescopic rod corresponding to the inner wall of the bottom end of the first sleeve, one side outer wall of the first telescopic rod is provided with a limiting hole, one side inner wall of the limiting hole is connected onto one side outer wall of a second connecting rod in a sliding manner, one side outer wall of the first telescopic rod is fixedly connected with a limiting baffle, one side outer wall of the first telescopic rod is sleeved with a second spring, one end of the second spring is fixedly connected onto one side outer wall of the limiting baffle, one end outer wall of the first telescopic rod is fixedly connected with a second sliding block, one side outer wall of the second sliding block is fixedly connected with a third connecting rod, and one side outer wall of the third connecting rod is provided with a protection component;
the protection assembly comprises a motor, a second sleeve, a fan, a connecting plate and a third sleeve, wherein the motor is fixedly installed on the outer wall of one side of the third connecting rod, the second sleeve is fixedly connected onto the outer wall of one side of the third connecting rod, the inner wall of one side of the second sleeve is sleeved on the outer wall of one side of the motor, the fan is installed on the outer wall of one side of the output shaft of the motor, the connecting plate is fixedly connected onto the outer side of the second sleeve, the third sleeve is sleeved on the outer side of the fan, and the inner wall of one side of the third sleeve is fixedly connected onto the outer wall of one side of the connecting plate;
the buffer assembly comprises a fourth chute, a second telescopic rod, a third spring and a buffer baffle plate, the fourth chute is formed in the outer wall of the bottom end of the supporting leg in a distributed mode, the buffer assembly is installed on the outer wall of the bottom end of the supporting leg through the fourth chute, the second telescopic rod is fixedly connected to the inner wall of one side of the fourth chute, the third spring is sleeved on the outer wall of one side of the second telescopic rod, and the buffer baffle plate is fixedly connected to the outer wall of one side of the second telescopic rod.
The using method of the unmanned aerial vehicle body temperature measuring device in the smart city comprises the steps of firstly, opening the device; step two, starting the device; step three, measuring the temperature; step four, descending the device;
in the first step, the first sliding block is pressed, so that the first telescopic rod in the first sleeve drives the third connecting rod to extend out under the action of the second spring;
in the second step, the unmanned aerial vehicle is placed on the ground, and a fan on the unmanned aerial vehicle is started in a remote control mode to enable the unmanned aerial vehicle to ascend to the air;
in the third step, the unmanned aerial vehicle staying in the air is close to the person to be subjected to temperature measurement, and the temperature is measured through the temperature measurer body;
wherein in the fourth step, after the temperature measurement, remote control unmanned aerial vehicle, through the buffering of buffer stop, makes unmanned aerial vehicle get back to ground safely.
According to the technical scheme, the outer wall of the top end of the unmanned aerial vehicle main body, corresponding to the temperature measurer body, is provided with the temperature measurer body mounting seat through bolts.
According to the technical scheme, the inner wall of one side of the first sleeve is provided with the third sliding groove, and the inner wall of one side of the third sliding groove is connected to the outer wall of one side of the second sliding block in a sliding mode.
According to the technical scheme, one end of the first spring is connected to the outer wall of one side of the first sliding block in an inserting mode, and the other end of the first spring is connected to the outer wall of one side of the first sliding groove in an inserting mode.
According to the technical scheme, the third sleeve is in a semi-cylindrical shape.
According to the technical scheme, the outer wall of one side of the third connecting rod is sleeved with the limiting check ring, and the outer wall of one side of the limiting check ring is fixedly connected to the outer wall of one side of the first sleeve.
According to the technical scheme, the number of the second telescopic rods is six.
Compared with the prior art, the invention has the following beneficial effects: the unmanned aerial vehicle has the advantages that the telescopic assembly, the protection assembly and the buffer assembly are adopted, and the first sliding block, the second connecting rod, the first telescopic rod, the limiting baffle, the second spring, the second sliding block and the third connecting rod in the telescopic assembly are matched, so that the unmanned aerial vehicle has a telescopic function, is simple in structure and convenient to operate, occupies a small space and is convenient to carry; the second sleeve, the fan, the connecting plate and the third sleeve in the protection assembly are matched, so that the unmanned aerial vehicle has a protection function and a simple structure; second telescopic link, third spring and buffer stop's cooperation in the buffering subassembly makes this unmanned aerial vehicle have buffering safeguard function, has further protected this unmanned aerial vehicle, has improved this unmanned aerial vehicle's life.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:
FIG. 1 is a schematic overall front cut-away construction of the present invention;
FIG. 2 is a schematic overall perspective view of the present invention;
FIG. 3 is a schematic view of the overall top view of the present invention;
FIG. 4 is a schematic top view of the protective assembly of the present invention;
FIG. 5 is an enlarged schematic view of the structure of the area A in FIG. 1 according to the present invention;
FIG. 6 is a flow chart of a method of the present invention;
in the figure: 1. an unmanned aerial vehicle main body; 2. a temperature detector body; 3. a telescoping assembly; 4. a protection component; 5. a buffer assembly; 6. supporting legs; 7. a temperature detector body mounting base; 31. a first chute; 32. a first slider; 33. a first spring; 34. a first connecting rod; 35. a second chute; 36. a second connecting rod; 37. a first sleeve; 38. a first telescopic rod; 39. a limiting hole; 310. a limiting baffle; 311. a second spring; 312. a second slider; 313. a third chute; 314. a third connecting rod; 315. a limiting retainer ring; 41. a motor; 42. a second sleeve; 43. a fan; 44. a connecting plate; 45. a third sleeve; 51. a fourth chute; 52. a second telescopic rod; 53. a third spring; 54. buffer baffle.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a technical solution: the unmanned aerial vehicle body temperature measuring device for the smart city comprises an unmanned aerial vehicle main body 1, a temperature measurer body 2, a telescopic assembly 3, a protection assembly 4, a buffer assembly 5, supporting legs 6 and a temperature measurer body mounting seat 7, wherein the temperature measurer body 2 is mounted on the outer wall of the bottom end of the unmanned aerial vehicle main body 1, the temperature measurer body mounting seat 7 is mounted on the outer wall of the bottom end of the unmanned aerial vehicle main body 1 corresponding to the top end of the temperature measurer body 2 through bolts, the temperature measurer body mounting seat 7 is arranged to facilitate installation of the temperature measurer body 2, the supporting legs 6 are symmetrically mounted and fixed on the outer wall of the bottom end of the unmanned aerial vehicle main body 1, and the telescopic assembly 3 is mounted on the inner wall of one side of the unmanned aerial vehicle main body 1; the telescopic assembly 3 comprises a first chute 31, a first slide block 32, a first spring 33, a first connecting rod 34, a second chute 35, a second connecting rod 36, a first sleeve 37, a first telescopic rod 38, a limiting hole 39, a limiting baffle 310, a second spring 311, a second slide block 312, a third chute 313, a third connecting rod 314 and a limiting retainer ring 315, wherein the first chute 31 is formed on the outer wall of the top end of the main body 1 of the unmanned aerial vehicle, the first slide block 32 is connected to the inner wall of one side of the first chute 31 in a sliding manner, the first spring 33 is sleeved on the outer wall of one side of the first slide block 32, one end of the first spring 33 is inserted on the outer wall of one side of the first slide block 32, the other end of the first spring 33 is inserted on the outer wall of one side of the first chute 31, the first spring 33 is arranged to enable the first slide block 32 to automatically recover to the original position, the outer wall of one side of the main body 1 of the unmanned aerial vehicle corresponding to the outer wall of the bottom end of the first slide block 32 is provided with the second chute 35, a first connecting rod 34 is connected to the inner wall of one side of the second chute 35 in a sliding manner, the outer wall of one side of the first connecting rod 34 is fixedly connected to the outer wall of the bottom end of the first slider 32, a second connecting rod 36 is fixedly connected to the outer wall of one end of the first connecting rod 34, a first sleeve 37 is fixedly connected to the outer side of the unmanned aerial vehicle main body 1, a first telescopic rod 38 is fixedly connected to the inner wall of the bottom end of the unmanned aerial vehicle main body 1 corresponding to the first sleeve 37, a limiting hole 39 is formed in the outer wall of one side of the first telescopic rod 38, the inner wall of one side of the limiting hole 39 is connected to the outer wall of one side of the second connecting rod 36 in a sliding manner, a limiting baffle 310 is fixedly connected to the outer wall of one side of the first telescopic rod 38, a second spring 311 is sleeved to the outer wall of one side of the first telescopic rod 38, one end of the second spring 311 is fixedly connected to the outer wall of one side of the limiting baffle 310, a second slider 312 is fixedly connected to the outer wall of one end of the first telescopic rod 38, a third sliding groove 313 is formed in the inner wall of one side of the first sleeve 37, the inner wall of one side of the third sliding groove 313 is connected to the outer wall of one side of the second sliding block 312 in a sliding manner, the arrangement of the third sliding groove 313 ensures that the second sliding block 312 slides stably in the first sleeve 37, a third connecting rod 314 is fixedly connected to the outer wall of one side of the second sliding block 312, a limit check ring 315 is sleeved on the outer wall of one side of the third connecting rod 314, the outer wall of one side of the limit check ring 315 is fixedly connected to the outer wall of one side of the first sleeve 37, the arrangement of the limit check ring 315 prevents the third connecting rod 314 from being separated from the first sleeve 37, and a protection component 4 is mounted on the outer wall of one side of the third connecting rod 314; the protection component 4 comprises a motor 41, a second sleeve 42, a fan 43, a connecting plate 44 and a third sleeve 45, the motor 41 is fixedly installed on the outer wall of one side of a third connecting rod 314, the second sleeve 42 is fixedly connected onto the outer wall of one side of the third connecting rod 314, the inner wall of one side of the second sleeve 42 is sleeved on the outer wall of one side of the motor 41, the fan 43 is installed on the outer wall of one side of an output shaft of the motor 41, the connecting plate 44 is fixedly connected onto the outer side of the second sleeve 42, the third sleeve 45 is sleeved on the outer side of the fan 43, the inner wall of one side of the third sleeve 45 is fixedly connected onto the outer wall of one side of the connecting plate 44, and the third sleeve 45 is in a semi-cylindrical shape, so that the purpose of protecting the fan 43 is achieved, and the overall weight of the unmanned aerial vehicle is reduced; buffering subassembly 5 includes fourth spout 51, second telescopic link 52, third spring 53 and buffering baffle 54, fourth spout 51 has been seted up to the distribution on the bottom outer wall of supporting leg 6, buffering subassembly 5 is installed on the 6 bottom outer walls of supporting leg through fourth spout 51, fixedly connected with second telescopic link 52 on one side inner wall of fourth spout 51, third spring 53 has been cup jointed on one side outer wall of second telescopic link 52, fixedly connected with buffering baffle 54 on one side outer wall of second telescopic link 52, the number of second telescopic link 52 is six, the cooperation of a plurality of second telescopic links 52, the stability of this unmanned aerial vehicle when descending has been improved.
Referring to fig. 6, the present invention provides a technical solution: the using method of the unmanned aerial vehicle body temperature measuring device in the smart city comprises the steps of firstly, opening the device; step two, starting the device; step three, measuring the temperature; step four, descending the device;
in the first step, the first slide block 32 is pressed, so that the first telescopic rod 38 in the first sleeve 36 drives the third connecting rod 314 to extend out under the action of the second spring 311;
in the second step, the unmanned aerial vehicle is placed on the ground, and a fan 43 on the unmanned aerial vehicle is started in a remote control mode to enable the unmanned aerial vehicle to ascend to the air;
in the third step, the unmanned aerial vehicle staying in the air is close to the person to be subjected to temperature measurement, and the temperature is measured through the temperature measurer body 2;
wherein in the fourth step, after the temperature measurement, remote control unmanned aerial vehicle, through the buffering of buffer stop 54, make unmanned aerial vehicle get back to ground safely.
Based on the above, the unmanned aerial vehicle has the advantages that when the unmanned aerial vehicle is used, the first sliding block 32 is pressed to slide the first sliding block 32 in the first sliding groove 31, the first connecting rod 34 is driven to move, the first connecting rod 34 is further driven to be separated from the limiting hole 39, the first telescopic rod 38 in the first sleeve 37 drives the third connecting rod 314 to extend under the action of the second spring 311, and the whole unmanned aerial vehicle is opened; the unmanned aerial vehicle is placed on the ground, the unmanned aerial vehicle is started to lift off through remote control, contactless temperature measurement is carried out on remote people through the thermoscope body 2 installed on the unmanned aerial vehicle, and the unmanned aerial vehicle is prevented from crashing to damage the fan 43 when the unmanned aerial vehicle fails in remote control through the protection effect of the third sleeve 45 installed on the motor 41, and meanwhile, the fan 43 is prevented from rotating to hurt the people; after the unmanned aerial vehicle finishes the measurement task, remotely controlling the unmanned aerial vehicle through a second telescopic rod 52; the third spring 53; buffering baffle 54's cooperation makes this unmanned aerial vehicle advance the buffering and descends to ground, accomplishes the unmanned aerial vehicle body temperature measuring device's in this wisdom city measurement work.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. Unmanned aerial vehicle body temperature measuring device in wisdom city, including unmanned aerial vehicle main part (1), thermoscope body (2), flexible subassembly (3), protection subassembly (4), buffering subassembly (5), supporting leg (6) and thermoscope body mount pad (7) its characterized in that: the temperature detector body (2) is installed on the outer wall of the bottom end of the unmanned aerial vehicle main body (1), the supporting legs (6) are symmetrically installed and fixed on the outer wall of the bottom end of the unmanned aerial vehicle main body (1), and the telescopic assembly (3) is installed on the inner wall of one side of the unmanned aerial vehicle main body (1);
the telescopic component (3) comprises a first sliding groove (31), a first sliding block (32), a first spring (33), a first connecting rod (34), a second sliding groove (35), a second connecting rod (36), a first sleeve (37), a first telescopic rod (38), a limiting hole (39), a limiting baffle (310), a second spring (311), a second sliding block (312), a third sliding groove (313), a third connecting rod (314) and a limiting retainer ring (315), wherein the outer wall of the top end of the unmanned aerial vehicle main body (1) is provided with the first sliding groove (31), the inner wall of one side of the first sliding groove (31) is connected with the first sliding block (32) in a sliding manner, the outer wall of one side of the first sliding block (32) is sleeved with the first spring (33), the outer wall of one side of the unmanned aerial vehicle main body (1) is provided with the second sliding groove (35) corresponding to the outer wall of the bottom end of the first sliding block (32) in a penetrating manner, a first connecting rod (34) is connected to the inner wall of one side of the second sliding groove (35) in a sliding manner, the outer wall of one side of the first connecting rod (34) is fixedly connected to the outer wall of the bottom end of the first sliding block (32), a second connecting rod (36) is fixedly connected to the outer wall of one end of the first connecting rod (34), a first sleeve (37) is fixedly connected to the outer side of the unmanned aerial vehicle main body (1), a first telescopic rod (38) is fixedly connected to the inner wall of the bottom end of the unmanned aerial vehicle main body (1) corresponding to the first sleeve (37), a limiting hole (39) is formed in the outer wall of one side of the first telescopic rod (38), the inner wall of one side of the limiting hole (39) is connected to the outer wall of one side of the second connecting rod (36) in a sliding manner, a limiting baffle (310) is fixedly connected to the outer wall of one side of the first telescopic rod (38), and a second spring (311) is sleeved on the outer wall of one side of the first telescopic rod (38), one end of a second spring (311) is fixedly connected to the outer wall of one side of the limiting baffle (310), a second sliding block (312) is fixedly connected to the outer wall of one end of the first telescopic rod (38), a third connecting rod (314) is fixedly connected to the outer wall of one side of the second sliding block (312), and a protection assembly (4) is mounted on the outer wall of one side of the third connecting rod (314);
the protection assembly (4) comprises a motor (41), a second sleeve (42), a fan (43), a connecting plate (44) and a third sleeve (45), wherein the motor (41) is fixedly installed on the outer wall of one side of the third connecting rod (314), the second sleeve (42) is fixedly connected onto the outer wall of one side of the third connecting rod (314), the inner wall of one side of the second sleeve (42) is sleeved on the outer wall of one side of the motor (41), the fan (43) is installed on the outer wall of one side of an output shaft of the motor (41), the connecting plate (44) is fixedly connected onto the outer side of the second sleeve (42), the third sleeve (45) is sleeved on the outer side of the fan (43), and the inner wall of one side of the third sleeve (45) is fixedly connected onto the outer wall of one side of the connecting plate (44);
buffering subassembly (5) include fourth spout (51), second telescopic link (52), third spring (53) and buffering baffle (54), fourth spout (51) have been seted up in the distribution on the bottom outer wall of supporting leg (6), buffering subassembly (5) are installed on supporting leg (6) bottom outer wall through fourth spout (51), fixedly connected with second telescopic link (52) on one side inner wall of fourth spout (51), third spring (53) have been cup jointed on one side outer wall of second telescopic link (52), fixedly connected with buffering baffle (54) on one side outer wall of second telescopic link (52).
2. The unmanned aerial vehicle body temperature measuring device in wisdom city of claim 1, characterized in that: the bottom outer wall of the unmanned aerial vehicle main body (1) corresponds to the top outer wall of the temperature measurer body (2) and is provided with a temperature measurer body mounting seat (7) through bolts.
3. The unmanned aerial vehicle body temperature measuring device in wisdom city of claim 1, characterized in that: and a third sliding groove (313) is formed in the inner wall of one side of the first sleeve (37), and the inner wall of one side of the third sliding groove (313) is connected to the outer wall of one side of the second sliding block (312) in a sliding mode.
4. The unmanned aerial vehicle body temperature measuring device in wisdom city of claim 1, characterized in that: one end of the first spring (33) is inserted into the outer wall of one side of the first sliding block (32), and the other end of the first spring (33) is inserted into the outer wall of one side of the first sliding groove (31).
5. The unmanned aerial vehicle body temperature measuring device in wisdom city of claim 1, characterized in that: the third sleeve (45) is in the shape of a semi-cylinder.
6. The unmanned aerial vehicle body temperature measuring device in wisdom city of claim 1, characterized in that: and a limiting check ring (315) is sleeved on the outer wall of one side of the third connecting rod (314), and the outer wall of one side of the limiting check ring (315) is fixedly connected to the outer wall of one side of the first sleeve (37).
7. The unmanned aerial vehicle body temperature measuring device in wisdom city of claim 1, characterized in that: the total number of the second telescopic rods (52) on the two supporting legs (6) is six.
8. The method for using the unmanned aerial vehicle body temperature measuring device in the smart city according to claim 1, comprising the steps of firstly, opening the device; step two, starting the device; step three, measuring the temperature; step four, descending the device; the method is characterized in that:
in the first step, the first sliding block (32) is pressed, so that the first telescopic rod (38) in the first sleeve (37) drives the third connecting rod (314) to extend out under the action of the second spring (311);
in the second step, the unmanned aerial vehicle is placed on the ground, and a fan (43) on the unmanned aerial vehicle is started in a remote control mode to enable the unmanned aerial vehicle to ascend to the air;
in the third step, the unmanned aerial vehicle staying in the air is close to the person to be subjected to temperature measurement, and the temperature is measured through the temperature measurer body (2);
wherein in the fourth step, after the temperature measurement, the unmanned aerial vehicle is remotely controlled, and the unmanned aerial vehicle safely returns to the ground through the buffering of the buffering baffle (54).
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