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CN108657421A - It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights - Google Patents

It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights
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Publication number
CN108657421A
CN108657421ACN201810268369.9ACN201810268369ACN108657421ACN 108657421 ACN108657421 ACN 108657421ACN 201810268369 ACN201810268369 ACN 201810268369ACN 108657421 ACN108657421 ACN 108657421A
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CN
China
Prior art keywords
unmanned plane
main body
wind
wind turbine
undercarriage
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Pending
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CN201810268369.9A
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Chinese (zh)
Inventor
辜晓平
孔利文
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Chengdu Zhongyi Hesheng Science And Technology Co Ltd
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Chengdu Zhongyi Hesheng Science And Technology Co Ltd
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Priority to CN201810268369.9ApriorityCriticalpatent/CN108657421A/en
Publication of CN108657421ApublicationCriticalpatent/CN108657421A/en
Pendinglegal-statusCriticalCurrent

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Abstract

It can solve the problems, such as that prior art mountain forest tour inefficiency, there are security risks and existing unmanned plane to be influenced by natural wind direction when making an inspection tour mountain forest by mountain forest perambulator according to the unmanned plane of both tramp-liner smooth flights the invention discloses a kind of.The present invention includes unmanned plane main body, and wing connecting rod, wing driving motor, two leaf wings, camera, microprocessor, undercarriage, undercarriage includes undercarriage connecting seat, lifting lever, damping spring and universal wheel;Unmanned plane lower body part sets wind turbine, wind turbine block brush, wind direction shaft, wind vane and wind direction brush stick, wind direction brush stick can be in contact with the wind turbine block brush when turning to any one wind turbine block brush with box haul shaft and wind turbine corresponding with the wind turbine block brush can be conducted with the power supply in unmanned plane main body.Mountain forest tour of the present invention is efficient, and can effectively eliminate the security risk of mountain forest perambulator, can effectively reduce and the risk of air crash occurs because of the factor of field wind.

Description

It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights
Technical field
The present invention relates to it is a kind of can be according to the unmanned plane of both tramp-liner smooth flights.
Background technology
With the development of science and technology, the field that unmanned plane uses is also increasingly wider, when the prior art carries out mountain forest tour, generallyIt is that a piece of mountain forest is maked an inspection tour on foot by one or two people, efficiency is ultralow, and patrols Lin Ren and patrol dangerous generation when woods, existingIt when unmanned plane flight in the wild, is affected by field wind direction, when wind direction is more random sometimes, or even will appear the danger of air crashDanger.
Therefore, design a kind of can efficiently make an inspection tour mountain forest and very big according to the unmanned plane of both tramp-liner smooth flightsThe labor intensity of mountain forest perambulator is reduced, and security risk of the mountain forest perambulator when making an inspection tour mountain forest can also be eliminated, becomes instituteBelong to technical field technical staff technical problem urgently to be resolved hurrily.
Invention content
The technical problem to be solved by the present invention is to:It is a kind of to be solved existing according to the unmanned plane of both tramp-liner smooth flightsTechnology mountain forest tour inefficiency, there are security risks and existing unmanned plane by nature when making an inspection tour mountain forest by mountain forest perambulatorWind direction influences big problem.
To achieve the above object, the technical solution adopted by the present invention is as follows:
It is a kind of can according to the unmanned plane of both tramp-liner smooth flights, including top in triangular prism shaped, middle part be in the cubic bodily form,Lower part is in the unmanned plane main body of hollow cylinder build, and one is removably connected with respectively on three angles of the unmanned plane body topThe free end of a wing connecting rod, each wing connecting rod is fixed there are one wing driving motor, and each wing drivesFixed there are one two leaf wings in the rotary shaft of dynamic motor, the centre on three side of unmanned plane body top is respectively equipped with oneCamera, the unmanned plane body top centre are equipped with the microprocessor being connect respectively with three camera functions, instituteIt states unmanned plane main body on both sides of the middle and is removably connected with a undercarriage respectively, the undercarriage is described including being removably connected toThe undercarriage connecting seat of unmanned plane lower body part side, a pair of of the lifting lever being symmetrically fixed on the undercarriage connecting seat, oneEnd is fixed on the undercarriage connecting seat, the other end is fixed on the lifting lever stretching from being used for when unmanned plane lands and subtractsThe damping spring of shake effect, and the universal wheel set on the lifting lever free end;Unmanned plane lower body part periphery is circumferentialIt is equidistant to set there are four wind turbine, correspond on the unmanned plane lower body part internal chamber wall each wind turbine set there are one wind turbine block brush,The unmanned plane bottom part body central vertical can be relative to unmanned plane main body bottom equipped with one in the unmanned plane bottom part bodyThe wind direction shaft that portion rotates freely, wind direction shaft bottom are fixed with wind vane, and the wind direction shaft passes through the unmanned planeBottom part body stretches to the inner cavity of the unmanned plane lower body part, and wind direction brush is vertically and fixedly provided at the top of the wind direction shaftStick, the wind direction brush stick can be with wind turbine electricity when following the wind direction shaft to turn to any one of wind turbine block brushBrush block is in contact and the wind turbine corresponding with the wind turbine block brush can be conducted with the power supply in the unmanned plane main body.
Further, the universal wheel is soft rubber universal wheel.
Further, the wing connecting rod tilts upward and the angle horizontal by one 30 °.
Further, the frame connecting seat that falls is equipped with fixing axle, and a pair of lifting lever is fixed on institute by fixing axleIt states on undercarriage connecting seat.
Further, the microprocessor is Intel Xeon E5-2699v3 microprocessors.
Compared with prior art, the invention has the advantages that:
(1) the configuration of the present invention is simple, design is scientific and reasonable, easy to use, mountain forest is maked an inspection tour efficient, can effectively reduce mountain forestThe labor intensity of tour personnel, and can effectively eliminate the security risk of mountain forest perambulator, is influenced small by field wind direction, can effectively be droppedIt is low the risk of air crash occur because of the factor of field wind.
(2) for the present invention by setting microprocessor and three cameras in unmanned plane body top, three cameras are located at topThe three sides center in portion, can in real time image unmanned plane body peripheral edge mountain forest scene, and imaged information is sent in real timeMicroprocessor is stored, and such mountain forest perambulator, which need not go deep into mountain forest, to carry out mountain forest tour, Er Qieshan by unmanned planeWoods makes an inspection tour ultrahigh in efficiency, can effectively reduce the labor intensity of mountain forest tour personnel, and can effectively eliminate the safety of mountain forest perambulatorHidden danger.
(3) present invention is connected by setting wing connecting rod, wing driving motor and two leaf wings, wing in unmanned plane main bodyExtension bar tilts upward and the angle horizontal by one 30 °, can effectively improve unmanned plane flying speed and flight it is steadyIt is qualitative, so as to effectively improve the efficiency that unmanned plane makes an inspection tour mountain forest, and it a can ensure that a unmanned plane is maked an inspection tour a mountain forest and is smoothed out.
(4) present invention in unmanned plane main body on both sides of the middle by respectively setting a undercarriage, and undercarriage includes undercarriageConnecting seat, lifting lever, damping spring, universal wheel and fixing axle, universal wheel use soft rubber universal wheel, so can effectively slow down nothingThe impact force generated when man-machine landing faces the impact force of unmanned plane main body, subtracts in which can be effectively reduced when unmanned plane landsThe probability of damage of small airborne equipment.
(5) present invention in unmanned plane lower body part by setting wind turbine, wind turbine block brush, wind direction shaft, wind vane and wind directionBrush stick, when unmanned plane in flight course by side leading wind when, wind vane drives wind direction shaft under the action of the side leading windRotation, wind direction brush stick rotates together with the rotation of wind direction shaft, when wind direction brush stick is rotated to a wind turbine block brushWhen be in contact with the wind turbine block brush, while by wind turbine corresponding with the wind turbine block brush with the power supply in unmanned plane main bodyIt is conducted, the wind turbine brings into operation at this time carries out Contrary compensation with crosswind suffered by unmanned plane, can effectively avoid unmanned plane and is blown offIt is predetermined to patrol woods course line, and can effectively reduce and the risk of air crash occur because of the factor of field wind.
Description of the drawings
Fig. 1 is schematic structural view of the invention.
Fig. 2 is landing gear structure schematic diagram of the present invention.
Fig. 3 is unmanned plane lower body part structural schematic diagram of the present invention.
Fig. 4 is unmanned plane body top face schematic diagram of the present invention.
Wherein, reference numeral is corresponding entitled:
1- unmanned planes main body, 2- wings connecting rod, 3- wings driving motor, two leaf wings of 4-, 5- cameras, 6- microprocessorsDevice, 7- undercarriages, 8- wind turbines, 9- wind turbines block brush, 10- wind directions shaft, 11- wind vanes, 12- wind direction brushes stick, 71- undercarriagesConnecting seat, 72- lifting levers, 73- damping springs, 74- universal wheels, 75- fixing axles.
Specific implementation mode
The invention will be further described with embodiment for explanation below in conjunction with the accompanying drawings, and mode of the invention includes but not only limitsIn following embodiment.
As shown in Figs 1-4, it is provided by the invention it is a kind of can according to the unmanned plane of both tramp-liner smooth flights, it is simple in structure,Design is scientific and reasonable, easy to use, and mountain forest tour is efficient, can effectively reduce the labor intensity of mountain forest tour personnel, and can haveEffect eliminates the security risk of mountain forest perambulator.It is in the cubic bodily form, lower part in hollow that the present invention, which includes top in triangular prism shaped, middle part,The unmanned plane main body 1 of cylinder type is removably connected with a wing on three angles at the top of the unmanned plane main body 1 and connects respectivelyThe free end of extension bar 2, each wing connecting rod 2 is fixed there are one wing driving motor 3, each wing driving motorFixed there are one two leaf wings 4 in 3 rotary shaft, the centre on 1 top of the unmanned plane main body, three sides is respectively equipped with one and takes the photographAs head 5, it is equipped with the microprocessor 6 with three 5 function connects of the camera respectively at 1 center of top of unmanned plane main body,1 on both sides of the middle of unmanned plane main body is removably connected with a undercarriage 7 respectively, and the undercarriage 7 includes being detachably connectedIn the undercarriage connecting seat 71 of 1 lower side of unmanned plane main body, one be symmetrically fixed on the undercarriage connecting seat 71To lifting lever 72, one end is fixed on the undercarriage connecting seat 71, the other end is fixed on the lifting lever 72 in nothingThe damping spring 73 of cushioning effect, and the universal wheel 74 set on 72 free end of the lifting lever, institute are stretched from when man-machine landingIt is Intel Xeon E5-2699v3 microprocessors to state microprocessor 6.
1 lower, outer perimeter of unmanned plane main body of the present invention is circumferentially equidistant to be set there are four wind turbine 8, under the unmanned plane main body 1It corresponds to each wind turbine 8 on portion's internal chamber wall to set there are one wind turbine block brush 9,1 bottom center of unmanned plane main body is perpendicular to this1 bottom of unmanned plane main body is equipped with a wind direction shaft 10 that can be rotated freely relative to 1 bottom of unmanned plane main body, the windIt is fixed with wind vane 11 to 10 bottom of shaft, the wind direction shaft 10 stretches to the nothing across 1 bottom of unmanned plane main bodyThe top of the inner cavity of 1 lower part of man-machine main body, the wind direction shaft 10 is vertically and fixedly provided with wind direction brush stick 12, the wind direction brush stick12 can be in contact simultaneously when following the wind direction shaft 10 to turn to any one of wind turbine block brush 9 with the wind turbine block brushThe wind turbine corresponding with the wind turbine block brush 8 can be conducted with the power supply in the unmanned plane main body 1.
Universal wheel 74 of the present invention is soft rubber universal wheel, and the wing connecting rod 2 tilts upward and and horizontal planeIn one 30 ° of angle, the frame connecting seat 71 that falls is equipped with fixing axle 75, and a pair of lifting lever 72 is solid by fixing axle 75Due on the undercarriage connecting seat 71.
For the present invention by setting microprocessor and three cameras in unmanned plane body top, three cameras are located at topThree sides center, can in real time image unmanned plane body peripheral edge mountain forest scene, and imaged information is sent to micro- place in real timeReason device is stored, and such mountain forest perambulator, which need not go deep into mountain forest, to carry out mountain forest tour by unmanned plane, and mountain forest is patrolledApparent efficiency is high, can effectively reduce the labor intensity of mountain forest tour personnel, and can effectively eliminate the security risk of mountain forest perambulator.
The present invention in unmanned plane main body by setting wing connecting rod, wing driving motor and two leaf wings, wing connectionBar tilts upward and the angle horizontal by one 30 °, can effectively improve the flying speed of unmanned plane and the stabilization of flightProperty, so as to effectively improve the efficiency that unmanned plane makes an inspection tour mountain forest, and it a can ensure that a unmanned plane is maked an inspection tour a mountain forest and is smoothed out.
The present invention in unmanned plane lower body part both sides by respectively setting a undercarriage, and undercarriage includes undercarriage connectionSeat, lifting lever, damping spring, universal wheel and fixing axle, universal wheel use soft rubber universal wheel, so can effectively slow down unmanned planeThe impact force generated when landing faces the impact force of unmanned plane main body, reduces machine in which can be effectively reduced when unmanned plane landsCarry the probability of damage of equipment.
The present invention in unmanned plane lower body part by setting wind turbine, wind turbine block brush, wind direction shaft, wind vane and wind direction brushStick, when unmanned plane in flight course by side leading wind when, wind vane driven under the action of the side leading wind wind direction shaft rotate,Wind direction brush stick rotates together with the rotation of wind direction shaft, when wind direction brush stick is rotated to a wind turbine block brush i.e. withThe wind turbine block brush is in contact, while wind turbine corresponding with the wind turbine block brush mutually being led with the power supply in unmanned plane main bodyLogical, the wind turbine brings into operation at this time and crosswind suffered by unmanned plane carries out Contrary compensation, can effectively avoid unmanned plane blown off it is predeterminedWoods course line is patrolled, and can effectively reduce and the risk of air crash occur because of the factor of field wind.
Above-described embodiment is only one of the preferred embodiment of the present invention, should not be taken to limit the protection model of the present inventionEnclose, as long as the present invention body design thought and that mentally makes have no the change of essential meaning or polishing, solvedThe technical issues of it is still consistent with the present invention, should all be included within protection scope of the present invention.

Claims (5)

1. a kind of can be according to the unmanned plane of both tramp-liner smooth flights, it is characterised in that:It is in triangular prism shaped, middle part including topThe cubic bodily form, lower part are in the unmanned plane main body (1) of hollow cylinder build, are divided on three angles at the top of the unmanned plane main body (1)It is not removably connected with a wing connecting rod (2), there are one wings to drive for the free end fixation of each wing connecting rod (2)Dynamic motor (3), each fixed in the rotary shaft of the wing driving motor (3) there are one two leaf wings (4), the unmanned ownersThe centre on three sides is respectively equipped with a camera (5) at the top of body (1), is equipped with and divides at unmanned plane main body (1) center of topNot with the microprocessor (6) of three camera (5) function connects, unmanned plane main body (1) on both sides of the middle is distinguished removableConnection is unloaded there are one undercarriage (7), the undercarriage (7) includes being removably connected to unmanned plane main body (1) lower sideUndercarriage connecting seat (71), a pair of of the lifting lever (72) being symmetrically fixed on the undercarriage connecting seat (71), one end is fixedIn on the undercarriage connecting seat (71), the other end be fixed on the lifting lever (72) for landing in unmanned plane stretchThe damping spring (73) of cushioning effect, and the universal wheel (74) set on the lifting lever (72) free end;The unmanned ownerBody (1) lower, outer perimeter is circumferentially equidistant to be set there are four wind turbine (8), each is corresponded on unmanned plane main body (1) the lower lumen wallWind turbine (8) is set there are one wind turbine block brush (9), and unmanned plane main body (1) bottom center is perpendicular to unmanned plane main body (1) bottomPortion is equipped with a wind direction shaft (10) that can be rotated freely relative to unmanned plane main body (1) bottom, the wind direction shaft(10) bottom is fixed with wind vane (11), and the wind direction shaft (10) stretches to described across unmanned plane main body (1) bottomThe inner cavity of unmanned plane main body (1) lower part is vertically and fixedly provided with wind direction brush stick (12), the wind at the top of the wind direction shaft (10)The wind direction shaft (10) is being followed to turn to any one of wind turbine block brush (9) Shi Keyu wind turbines to brush stick (12)Block brush is in contact and can be by the electricity in the wind turbine (8) corresponding with the wind turbine block brush and the unmanned plane main body (1)Source is conducted.
CN201810268369.9A2018-03-292018-03-29It is a kind of can be according to the unmanned plane of both tramp-liner smooth flightsPendingCN108657421A (en)

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Application NumberPriority DateFiling DateTitle
CN201810268369.9ACN108657421A (en)2018-03-292018-03-29It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
CN201810268369.9ACN108657421A (en)2018-03-292018-03-29It is a kind of can be according to the unmanned plane of both tramp-liner smooth flights

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CN108657421Atrue CN108657421A (en)2018-10-16

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN111284687A (en)*2020-04-142020-06-16中国人民解放军32180部队High-wind-resistance coaxial reverse-paddle type mooring unmanned aerial vehicle and flight control method thereof
CN114858970A (en)*2021-12-022022-08-05绍兴腾耀环保科技有限公司 A portable ozone wireless detector

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* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB409993A (en)*1932-09-301934-05-10Marcel Louis GianoliImprovements in stabilising devices for aircraft
CN107031830A (en)*2017-05-122017-08-11西华酷农无人机产业园运营有限公司It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance
CN107207088A (en)*2014-12-042017-09-26埃尔瓦有限公司 Reconfigurable Unmanned Aerial Vehicle System
CN206719532U (en)*2017-04-102017-12-08四川建筑职业技术学院A kind of rearmounted damping undercarriage of fixed-wing unmanned plane
CN207631475U (en)*2018-02-282018-07-20大英县东创农业有限公司It is a kind of can self-adjusting balance plant protection drone

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB409993A (en)*1932-09-301934-05-10Marcel Louis GianoliImprovements in stabilising devices for aircraft
CN107207088A (en)*2014-12-042017-09-26埃尔瓦有限公司 Reconfigurable Unmanned Aerial Vehicle System
CN206719532U (en)*2017-04-102017-12-08四川建筑职业技术学院A kind of rearmounted damping undercarriage of fixed-wing unmanned plane
CN107031830A (en)*2017-05-122017-08-11西华酷农无人机产业园运营有限公司It is a kind of can be according to the unmanned plane of wind direction self-adjusting balance
CN207631475U (en)*2018-02-282018-07-20大英县东创农业有限公司It is a kind of can self-adjusting balance plant protection drone

Cited By (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
CN111284687A (en)*2020-04-142020-06-16中国人民解放军32180部队High-wind-resistance coaxial reverse-paddle type mooring unmanned aerial vehicle and flight control method thereof
CN114858970A (en)*2021-12-022022-08-05绍兴腾耀环保科技有限公司 A portable ozone wireless detector
CN114858970B (en)*2021-12-022024-04-09绍兴腾耀环保科技有限公司Portable ozone wireless detector

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