CN211107960U

CN211107960U - Shock absorption support for lifting of surveying and mapping unmanned aerial vehicle

Info

Publication number: CN211107960U
Application number: CN201922184914.9U
Authority: CN
Inventors: 周小斌; 邓永久
Original assignee: Wuhan Yijia Surveying And Mapping Geographic Information Co ltd
Current assignee: Wuhan Yijia Surveying And Mapping Geographic Information Co ltd
Priority date: 2019-12-09
Filing date: 2019-12-09
Publication date: 2020-07-28
Anticipated expiration: 2029-12-09

Abstract

The utility model discloses a survey and drawing shock absorber support for unmanned aerial vehicle goes up and down, including the unmanned aerial vehicle organism, flight support, rotor protection frame, motor power, the rotor, camera device, L ED illumination, the bradyseism support, a pedestal, the apparatus further comprises a rotating shaft, the end footboard, strengthen the connecting rod, the bradyseism device, flight support body installs rotor protection frame, the rotor is installed in the motor power pivot, L ED illumination is installed to the terminal surface before the unmanned aerial vehicle organism, camera device installs in unmanned aerial vehicle organism bottom, the bradyseism support mounting is in unmanned aerial vehicle organism bottom, support accessible pivot carries out certain angle and rotates, the end footboard of support mounting, the bradyseism device is independently installed on support frame body, a survey and drawing shock absorber support for unmanned aerial vehicle goes up and down, receive the gravity influence when unmanned aerial vehicle organism falls, the support is to both sides motion, strengthen the connecting rod and guarantee support intensity, the elasticity of bradyseism spring is reverse traction pulling support, the direction of.

Description

Shock absorption support for lifting of surveying and mapping unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned aerial vehicle field, especially a shock absorber support is used in survey and drawing unmanned aerial vehicle lift.

Background

Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to overcome prior art's shortcoming, provide a survey and drawing unmanned aerial vehicle goes up and down and uses shock absorber support. In order to realize the purpose, the utility model adopts the following technical scheme:

the utility model provides a survey and drawing unmanned aerial vehicle goes up and down and use shock-absorbing support, including the unmanned aerial vehicle organism, the flight support, rotor protection frame, motor power, the rotor, camera device, L ED illumination, the bradyseism support, a pedestal, the apparatus further comprises a rotating shaft, a support, the end footboard, the reinforcing connecting rod, the bradyseism device, flight support frame body installs rotor protection frame, the rotor is installed in the motor power pivot, L ED illumination is installed to the terminal surface before the unmanned aerial vehicle organism, camera device installs in unmanned aerial vehicle organism bottom, the bradyseism support mounting is in unmanned aerial vehicle organism bottom, certain angle rotation is carried out in the support accessible pivot, end footboard is installed to the support end.

Preferably, the bradyseism device is by preceding pole setting, back pole setting, the spacer pin, guide connecting rod and bradyseism spring are constituteed, preceding pole setting is spliced and is installed on the support, back pole setting is spliced and is installed on the base, preceding pole setting is hung with back pole setting and is put and install the bradyseism spring, install guide connecting rod with the upper end position of bradyseism spring with the centre of a circle, the terminal welding of guide connecting rod has the spacer pin, unmanned aerial vehicle organism whereabouts, receive the gravity influence, the support is to the both sides motion, strengthen the connecting rod and guarantee support intensity, bradyseism spring elasticity is reverse traction pulling support, the direction of motion is guaranteed to guide connecting rod, the bradyseis.

Preferably, the flight support is made of composite plastic.

Preferably, the rotor protection frame radius is greater than the rotor radius.

Compared with the prior art, the utility model has the advantages of it is following: the utility model provides a survey and drawing unmanned aerial vehicle goes up and down and uses shock absorber support, receives the gravity influence when unmanned aerial vehicle organism whereabouts, and the support is to both sides motion, strengthens the connecting rod and guarantees support intensity, and the elasticity of bradyseism spring is reverse traction pulling support, and the direction of motion of support is guaranteed to the direction connecting rod, and the motion distance of direction connecting rod is guaranteed to the spacer pin, steady descending.

Drawings

Fig. 1 is the utility model discloses survey and drawing unmanned aerial vehicle goes up and down with shock absorber support's schematic structure.

Fig. 2 is the utility model discloses survey and drawing unmanned aerial vehicle goes up and down with shock absorber support's mounting structure schematic diagram.

Fig. 3 is a schematic structural view of the shock absorbing support of the present invention.

Fig. 4 is a schematic structural view of the shock absorber of the present invention.

In the figure, the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a flying support 2, a flying support 3, a rotor wing protection frame 4, a power motor 5, a rotor wing 6, a camera shooting device 7, L ED lighting 8, a shock absorption support 9, a base 10, a rotating shaft 11, a support 12, a bottom pedal 13, a reinforcing connecting rod 14, a shock absorption device 15, a front vertical rod 16, a rear vertical rod 17, a limiting pin 18, a guide connecting rod 19 and a shock absorption spring.

Detailed Description

The invention is explained in further detail below with reference to the figures and the embodiments.

Fig. 1, fig. 2, fig. 3 and fig. 4 show, a survey and drawing unmanned aerial vehicle goes up and down and uses shock-absorbing support, including unmanned aerial vehicle organism 1, flight support 2, rotor protection frame 3, motor power 4, rotor 5, camera device 6, L ED illumination 7, bradyseism support 8, base 9, pivot 10, support 11, end pedal 12, strengthen connecting rod 13, bradyseism device 14, unmanned aerial vehicle organism 1 slope connection installs four flight support 2, flight support 2 support body end screw fastening installs rotor protection frame 3, flight support 2 support body end up end connection installs motor power 4, motor power 4 pivot is installed rotor 5, unmanned aerial vehicle organism 1 preceding end central point puts built-in L ED illumination 7 of installing, camera device 6 is installed in unmanned aerial vehicle organism 1 bottom axis position, bradyseism support 8 uses screw fastening to install in unmanned aerial vehicle organism 1 bottom, bradyseism support 8 is by base 9, pivot 10, support 11, end pedal 12, strengthen connecting rod 13 and bradyseism device 14 and constitute, support 11 uses pivot 10 and base 9 to be connected the installation, support 11 accessible pivot 10 rotates certain angle, connecting rod connects between two independent connecting rod support 11 and install and strengthen end screw support body 13, bradyseism device uses end support installation 14.

Bradyseism device 14 is by preceding pole setting 15, back pole setting 16, spacer pin 17, guide link 18 and bradyseism spring 19 are constituteed, 15 splices in preceding pole setting are installed on

support

11, 16 splices in back pole setting are installed on base 9, preceding pole setting 15 is hung with back pole setting 16 and is put and install bradyseism spring 19, guide link 18 is installed with the upper end position of bradyseism spring 19 concentric circles, 18 terminal welding of guide link has spacer pin 17, 1 whereabouts of unmanned aerial vehicle organism, receive the influence of gravity, support 11 is to the both sides motion, strengthen connecting rod 13 and guarantee support 11 intensity, bradyseism spring 19 elasticity is reverse traction pulling support 11, direction of motion is guaranteed to guide link 18, bradyseism device 14 possesses fine bradyseism performance.

The flight support 2 is made of composite plastic.

The radius of the rotor wing protection frame 3 is larger than that of the rotor wing 5.

The utility model discloses the theory of operation: the utility model provides a survey and drawing unmanned aerial vehicle goes up and down and uses shock absorber support, receives the gravity influence when unmanned aerial vehicle organism whereabouts, and the support is to both sides motion, strengthens the connecting rod and guarantees support intensity, and the elasticity of bradyseism spring is reverse traction pulling support, and the direction of motion of support is guaranteed to the direction connecting rod, and the motion distance of direction connecting rod is guaranteed to the spacer pin, steady descending.

The foregoing is a preferred embodiment of the present invention, and for those skilled in the art to understand the teaching of the present invention, the changes, modifications, replacements and variations to the embodiments will still fall within the protection scope of the present invention without departing from the principle and spirit of the present invention.

Claims

1. The utility model provides a survey and drawing unmanned aerial vehicle goes up and down and use shock-absorbing support, a serial communication port, including unmanned aerial vehicle organism (1), flight support (2), rotor protection frame (3), motor power (4), rotor (5), camera device (6), L ED illumination (7), bradyseism support (8), base (9), pivot (10), support (11), end pedal (12), strengthen connecting rod (13), bradyseism device (14), unmanned aerial vehicle organism (1) slope is connected and is installed four flight support (2), flight support (2) support body end screw fastening installs rotor protection frame (3), flight support (2) support body end up end is connected and is installed motor power (4), rotor (5) are installed in motor power (4) pivot, end face central point puts built-in before unmanned aerial vehicle organism (1) installs L ED illumination (7), camera device (6) are installed in unmanned aerial vehicle (1) bottom axis position, bradyseism support (8) use screw fastening to install in unmanned aerial vehicle organism (1) bottom, bradyseism support (8) is by base (9), pivot (10) and connecting rod (11) are connected the support body and are connected, the device (11) and are connected to be connected between pivot (11), the support body (11) and use the rotation support (11).

2. The shock absorption support for surveying and mapping unmanned aerial vehicle lifting according to claim 1, wherein the shock absorption device (14) is composed of a front vertical rod (15), a rear vertical rod (16), a limiting pin (17), a guide connecting rod (18) and a shock absorption spring (19), the front vertical rod (15) is adhesively mounted on the support (11), the rear vertical rod (16) is adhesively mounted on the base (9), the shock absorption spring (19) is mounted on the front vertical rod (15) and the rear vertical rod (16) in a hanging manner, the guide connecting rod (18) is mounted at the upper end position concentric with the shock absorption spring (19), the limiting pin (17) is welded at the tail end of the guide connecting rod (18), the unmanned aerial vehicle body (1) falls and is influenced by gravity, the support (11) moves towards two sides, the reinforcing connecting rod (13) ensures the strength of the support (11), and the shock absorption spring (19) makes reverse traction to pull the support (11), the guide connecting rod (18) ensures the movement direction, and the shock absorption device (14) has good shock absorption performance.

3. The shock absorption support for the lifting of the surveying and mapping unmanned aerial vehicle according to claim 1, wherein the flight support (2) is made of composite plastic.

4. The shock absorbing bracket for lifting of mapping unmanned aerial vehicle according to claim 1, characterized in that the radius of the rotor wing protective frame (3) is larger than the radius of the rotor wing (5).