CN204871599U - Four shaft air vehicle - Google Patents

Abstract

The utility model provides a four shaft air vehicle, including the aircraft body, be provided with the support frame on the aircraft body, this support frame is provided with four arms that are criss -cross, and the tip of every arm is provided with the screw, the screw passes through its rotation of driving motor drive, propeller shaft top at every screw is provided with ultrasonic sensor, install atmospheric pressure height sensor at the support frame in the face of the one side on ground, be provided with the control box on the aircraft body, install the chip of integrated control ware in this control box, still be provided with an overhang on the support frame, be provided with the industry camera on this overhang. The utility model provides a four shaft air vehicle can realize automatically detecting the inspection to the bridge crackle to saved a large amount of manpower and materials, and measure convenient, this aircraft low in manufacturing cost moreover, measurement of efficiency is high.

Description

Four-axle aircraft

Technical field

The utility model relates to a kind of detecting devices, particularly relates to a kind of four-axle aircraft.

Background technology

China's communication develops rapidly in recent years, and for alleviating traffic pressure, the bridge on urban interchange, overpass and highway at different levels increases year by year.As time goes on, the appearance of various situation can cause the danger coefficient of bridge to rise, as: traffick increase causes bridge load to increase, existing defects in design process, bridge pavement unfairness causes vibratility partial failure, material aging, the existence of the factors such as the impact of rough ambient climate environment.The existence of factor like this and cause bridge to occur crackle, as found, maintenance is easy to cause bridge structure to damage not in time, and cause bridge collapse time serious and produce serious safety misadventure, the report of this type of accident is of common occurrence.

Therefore, Timeliness coverage also takes maintenance remedial measures extremely important to bridge security, current method of inspection is artificial congnition method mainly, by means of high magnified glass and microscope, survey record is carried out to bridge, the method depends on manpower, there is the defects such as measuring period is long, cost is high, artificial sense datum is stronger, simultaneously need by means of equipment such as scaffolds when subsidiary, there is large discharge vehicle pass-through in the larger overpass of traffic capacity, overpass region, also considerable influence is produced to the safety of survey crew and efficiency.

Utility model content

The purpose of this utility model is the defect solving the existence of above-mentioned prior art, provides a kind of four-axle aircraft that automatically can carry out survey record to bridge.

A kind of four-axle aircraft, comprise aircraft body, described aircraft body is provided with bracing frame, this bracing frame is provided with four mechanical arms in square crossing, the end of each mechanical arm is provided with screw propeller, and described screw propeller controls drive motor driving by brushless electric-regulating device makes it rotate; The prop shaft top of each screw propeller is provided with sonac; In the one side of bracing frame in the face of ground, pressure-altitude sensor is installed, aircraft body is provided with control box, the chip of integrated manipulator is installed in this control box; Bracing frame is also provided with a jag, this jag is provided with industrial camera.

Further, four-axle aircraft as above, each mechanical arm its two sections is wide, middle narrow.

The four-axle aircraft that the utility model provides, can realize automatically carrying out detection inspection to bridge crack, thus save a large amount of manpower and materials, and measure conveniently, and this aircraft manufacture cost is low, measures efficiency high.

Accompanying drawing explanation

Fig. 1 is the utility model four-axle aircraft structural representation.

Detailed description of the invention

For making the purpose of this utility model, technical scheme and advantage clearly, below technical scheme in the utility model be clearly and completely described, obviously, described embodiment is the utility model part embodiment, instead of whole embodiments.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.

Fig. 1 is the utility model four-axle aircraft structural representation, as shown in Figure 1, the four-axle aircraft that the utility model provides, comprise aircraft body 1, described aircraft body 1 is provided with bracing frame 11, this bracing frame 11 is provided with four mechanical arms 12 in square crossing, and the end of each mechanical arm 12 is provided with screw propeller 13, and described screw propeller 13 drives it to rotate by drive motor 14; Prop shaft 131 top of each screw propeller 13 is provided with sonac; In the one side on 11 pairs of ground, bracing frame face, pressure-altitude sensor is installed, aircraft body 1 is provided with control box 16, the chip of integrated manipulator is installed in this control box 16.Bracing frame 11 is also provided with a jag 17, this jag 17 is provided with industrial camera 15.

Particularly, the chip of described controller is integrated with dsp processor, GPS module, three-axis gyroscope, triaxial accelerometer, radio receiving transmitting module, wireless image transmission module, described dsp processor is connected with described drive motor, described radio receiving transmitting module, wireless image transmission module are corresponding with handheld device, and handheld device is for inputting various parameter to make normal vehicle operation.

Aircraft of the present utility model can realize 2 kinds of measurement patterns, one is automatic measurement pattern, one is manual measurement pattern, wherein, automatic measurement pattern is that the control box by aircraft body is arranged realizes controlling, and manual measurement pattern controls ball by the heading corresponding with handheld device to realize.

When aircraft is in automatic measurement pattern, survey crew is first by handheld device setpoint distance bridge bottom safety Distance geometry flight altitude datum.Different bridge height is different, and for adapting to all types of bridge structure, this aircraft can by handheld device by means of pressure-altitude sensor setting flight altitude datum, and aircraft flies all the time near this height.The setting of this height needs the focal length combining industrial camera of taking pictures simultaneously, to ensure best photo angle and distance.Because uneven and creep plant and other obstacles existence may appear in some position bottom bridge, the distance bottom sense aircraft and bridge is not stopped at the one side installation pressure-altitude sensor of bracing frame in the face of ground of aircraft body, when distance is less than setting safety distance time, automatic adjustment aircraft does low amplitude pitching flying in measurement simultaneously, until safety distance reaches rear recovery normal flight attitude, thus ensure aircraft avoid while being in best picture-taking position with bridge bottom obstacle collide, ensure that measuring safety and precise carries out.

Described dsp controller controls four drive motor by four brushless electric-regulating devices and drives four corresponding screw propellers to rotate, four screw propellers are symmetrically distributed in around aircraft body by four mechanical arms of bracing frame, the utility model aircraft body is rotated and reverse by four screw propellers and makes aircraft realize front and back, up and down, pitching, roll, driftage, the flare maneuvers such as hovering, dsp controller Real-time Collection three-axis gyroscope and the signal of triaxial accelerometer are with the attitude on the current relative ground of calculating aircraft and acceleration/accel simultaneously, cireular frequency, and calculated by special algorithm analysis meter and keep rotational force needed for state of flight and lift, above-mentioned action is realized by the rotation direction and rotating speed that change screw wing.

The collection of bridge crack information realizes the collection of picture signal mainly through the industrial area array cameras being carried at aircraft body jag, the mode that the driving employing dsp controller of industrial camera and FPGA driving governor combine, described FPGA driving governor is controlled to start by dsp controller, FPGA controller is responsible for that camera drives, acquisition of signal, signal parallel is transferred to the analysis that dsp controller is used for view data by LVDS bus simultaneously, the graphicinformation that dsp processor analytical industry collected by camera arrives, calculate in current position image and whether occur crackle, crack length is how many and the width of crackle and maximum width are how many, keep when detecting that crackle occurs aircraft to be in floating state and occur crack position with instruction, by by crackle maximum width, crack length information sends handheld device to by radio receiving transmitting module, send by wireless image transmission module the graphicinformation that correspondence is sampled to handheld device simultaneously, so that survey crew makes preliminary crackle degree analyzing and the later stage files, service record data.In the handheld device mass-memory unit is housed, graphicinformation can be uploaded to PC server by USB interface and file by handheld device.And send after survey crew completes analytic record and continue to patrol and examine signal, aircraft continues to patrol and examine according to original set model, patrol and examine route to be decided by coordinate information in handheld device, chip in described control box is also integrated with a GPS module, is used to indicate the coordinate position residing for current flight device.After receiving each coordinate position, automatically regulate flight attitude to fly towards desired location, automatically return according to original route behind position of reaching home and to have landed measurement process at start position.

The utility model is provided with sonac at the prop shaft top of each screw propeller, described sonac is for measuring the distance of carry-on screw propeller distance peripheral obstacle, then send this range information to dsp processor, then dsp processor adjusts according to the flight condition of this range information to aircraft.Particularly, in aircraft flight process, rough structure may be there is on the one hand at bridge bottom construction, or even the obstacle such as plant and branch of creeping, if do not set the safety distance bottom aircraft and bridge, then aircraft and obstacle may be caused to collide thus cause obstacle impaired.On the other hand, likely there will be the existence of the objects such as the branch of landscape tree in bridge surrounding, if do not consider that intelligence keeps in obscurity, then aircraft also may be caused impaired.Therefore, in the automatic cruising aerocraft system of aircraft, sonac group is extremely important.

Survey crew portable hand-held equipment, this equipment controls the action of aircraft by radio receiving transmitting module, realize by wireless image transmission module the view data accepting suspected bridge crackle simultaneously, and the data message such as crack length, maximum crack width of current doubtful position.Handheld device, with customizing keyboard and wide LED display, requiring first to set bridge height, aircraft altitude and flight safety distance by keyboard, and sets vehicle flight speeds, for simplifying the operation, speed being divided into five class.Need setting flight to detect route simultaneously, the coordinate position detecting starting point, crucial intermediate point, terminal is provided in conjunction with GPS, coordinate position by handheld device internal processes according to gps signal automatic acquisition, and the coordinate detecting all set points in course is issued aircraft sequentially through radio receiving transmitting module with protocol form, in traveling process, automatically adjust flight attitude according to coordinate position after aircraft receives.Set rear startup aircraft, aircraft will rise to flying height from start position, start industrial camera detect according to setting path.Can hover when doubtful crackle being detected, handheld device receives again by startup work after corresponding signal, and aircraft can fly according to setting path and detect from hovering position continues.The built-in bulk memory of handheld device simultaneously, crackle relevant information (crack length, crackle maximum width, crack detection time) and crackle existence place image information fusion can be stored by database management language together, PC end can be uploaded to by USB port and be further analyzed and confirm.

Further, in order to alleviate the utility model the weight of four-axle aircraft, the utility model institute described each mechanical arm 12 its two sections is wide, middle narrow, and can also be engraved structure by the vibrational power flow of aircraft body.

Last it is noted that above embodiment is only in order to illustrate the technical solution of the utility model, be not intended to limit; Although be described in detail the utility model with reference to previous embodiment, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment technical scheme of the utility model.

Claims (2)

1. a four-axle aircraft, it is characterized in that, comprise aircraft body (1), described aircraft body (1) is provided with bracing frame (11), this bracing frame (11) is provided with four mechanical arms (12) in square crossing, the end of each mechanical arm (12) is provided with screw propeller (13), and described screw propeller (13) controls drive motor (14) driving by brushless electric-regulating device makes it rotate; Prop shaft (131) top of each screw propeller (13) is provided with sonac; In the one side of bracing frame (11) in the face of ground, pressure-altitude sensor is installed, aircraft body (1) is provided with control box (16), the chip of integrated manipulator is installed in this control box (16); Bracing frame (11) is also provided with a jag (17), this jag (17) is provided with industrial camera (15).

2. four-axle aircraft according to claim 1, is characterized in that, each mechanical arm (12) its two sections is wide, middle narrow.