CN107933928A - A kind of unmanned plane article loading device - Google Patents

A kind of unmanned plane article loading device Download PDF

Info

Publication number
CN107933928A
CN107933928A CN201810038079.5A CN201810038079A CN107933928A CN 107933928 A CN107933928 A CN 107933928A CN 201810038079 A CN201810038079 A CN 201810038079A CN 107933928 A CN107933928 A CN 107933928A
Authority
CN
China
Prior art keywords
article
case
unmanned plane
vehicle body
aerial vehicle
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201810038079.5A
Other languages
Chinese (zh)
Inventor
赵雪冬
孙晓伟
金晶
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Anhui Wing Flight Safe Technology Ltd
Original Assignee
Anhui Wing Flight Safe Technology Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Anhui Wing Flight Safe Technology Ltd filed Critical Anhui Wing Flight Safe Technology Ltd
Priority to CN201810038079.5A priority Critical patent/CN107933928A/en
Publication of CN107933928A publication Critical patent/CN107933928A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D9/00Equipment for handling freight; Equipment for facilitating passenger embarkation or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Buffer Packaging (AREA)

Abstract

The invention discloses a kind of unmanned plane article loading device,It is related to unmanned air vehicle technique field,Case is carried including the article installed in unmanned aerial vehicle body lower end,The lower end of the unmanned aerial vehicle body is equipped with wire interface,Wire interface is electrically connected with the power supply in unmanned aerial vehicle body,Article carries the wherein open at one end of case and is hinged with chamber door,The upper surface that article carries case is equipped with concave mounting groove,Micro air pump is installed in mounting groove,The inner wall that article carries case is bonded with high-pressure gasbag,The high-pressure gasbag is connected by air inlet pipe with micro air pump,The outer wall that article carries case is equipped with the exhaust pipe connected with high-pressure gasbag,And exhaust pipe is equipped with solenoid valve,The configuration of the present invention is simple,The positioning that article can be stablized,Unmanned plane is when transporting article,Article will not produce shaking phenomenon,Improve stability during unmanned plane during flying,And article can be effectively protected,Article is prevented to be damaged.

Description

A kind of unmanned plane article loading device
Technical field
The present invention relates to unmanned air vehicle technique field, and in particular to a kind of unmanned plane article loading device.
Background technology:
In recent years, Material Transportation is carried out to disaster area using unmanned plane or the transport of rescue aid is carried out to scene of fire Situation is more and more, is extensively favored because unmanned plane possesses good flexibility by all trades and professions, although in the market have it is very much Unmanned plane article loading device, but most of these devices have many defects, the structure that some stay in device is complex, The stability of unmanned plane during flying is influenced in the case of in quality, and article easily rocks during carrying, causes unmanned plane to exist Security when flight reduces, and difficulty is added for goods transportation.
The Chinese patent of Application No. 2017202317814 discloses a kind of goods and materials carrying platform of unmanned plane, including peace Goods and materials carrying platform loaded on unmanned fuselage lower end, the goods and materials carrying platform include a fixing bracket, inside fixing bracket One telescope motor is installed, fixing bracket bottom has an extension, is set with a luggage carrier in the extension, on luggage carrier End has a reducing gear, and the bottom of luggage carrier is provided with the lanyard of more than one, and lanyard bottom has hook, and hook is risen to the bait Relief goods are placed with, relief goods upset is placed on the reducing gear with luggage carrier upper end.
The technical solution of above-mentioned patent is during goods and materials are transported, since goods and materials are to be placed on load by linking up with hook Below rack, so unmanned plane, during belongings fly, if subjected to if the influence of air-flow, goods and materials produce rolling It is dynamic, it can so cause the flight stability of unmanned plane to reduce, there is security risk.
The content of the invention
It is caused by the prior art above-mentioned to solve it is an object of the invention to provide a kind of unmanned plane article loading device Multinomial defect.
A kind of unmanned plane article loading device, including the article carrying case installed in unmanned aerial vehicle body lower end, the article The both sides for carrying case are equipped with positioning plate, and the positioning plate is fastenedly connected by the lower end of retaining mechanism and unmanned aerial vehicle body, described The lower end of unmanned aerial vehicle body is equipped with wire interface, and wire interface is electrically connected with the power supply in unmanned aerial vehicle body, and the article is taken Load case is a hollow babinet, and article carries the wherein open at one end of case and is hinged with chamber door, and the upper surface that article carries case is set There is concave mounting groove, micro air pump is installed in the mounting groove, the micro air pump is connected by conducting wire with wire interface, The inner wall that the article carries case is bonded with high-pressure gasbag, and the high-pressure gasbag is connected by air inlet pipe with micro air pump, and into Cooling gas check valve is installed, the outer wall that the article carries case is equipped with the exhaust pipe connected with high-pressure gasbag, and arranges on tracheae Tracheae is equipped with solenoid valve, and the outer wall that the article carries case is equipped with controller, and described controller one end is by conducting wire with leading Line interface connects, and the other end is electrically connected with micro air pump and solenoid valve respectively by conducting wire.
Preferably, the retaining mechanism includes positioning bolt, compression spring and nut, and the positioning plate is equipped with up/down perforation Location hole, positioning bolt are integrated part with unmanned aerial vehicle body, and compression spring sleeve is on positioning bolt, and positioning bolt passes through location hole, And pass through nut check, the upper surface close contact of compression spring one end and positioning plate, and the lower face of the other end and unmanned aerial vehicle body It is in close contact.
Preferably, the positioning plate is equipped with four, and is evenly distributed on article and carries on the side wall of case, and positioning plate and thing Product carry case and are integrated part.
Preferably, the wire interface includes interface one and interface two, interface one and interface two with unmanned aerial vehicle body Power supply be electrically connected, solenoid valve is connected with micro air pump by conducting wire with interface one, and controller one end is by conducting wire with connecing The connection of mouth two and the other end pass through conducting wire and micro air pump and solenoid valve is electrically connected.
The advantage of the invention is that:By being arranged compression spring on positioning bolt, improve article and carry case and unmanned plane machine The stability of body installation, compression spring are in compressive state, and such nut will not produce loosening easily, by being carried in article in case High-pressure gasbag is set on wall, when needing carrying article to be transported, article is placed items within and carries in case, start miniature gas Pump pressurizes high-pressure gasbag, can expand and heave after high-pressure gasbag pressurization, such high-pressure gasbag can be close with the outer wall of article Extrusion, so as to be positioned to article, for unmanned plane during being transported to article, article will not produce showing of rocking As, stability and security that unmanned plane is run are improved, meanwhile, touched when unmanned plane produces during forced landing with ground In the case of hitting, high-pressure gasbag can be effectively protected article, place article and be damaged.
The configuration of the present invention is simple, the positioning that can be stablized to article, unmanned plane is when transporting article, article Shaking phenomenon will not be produced, improves stability during unmanned plane during flying, and article can be effectively protected, prevents thing Product are damaged.
Brief description of the drawings
Fig. 1 is the structure diagram of the present invention.
Fig. 2 is the top view that article carries case.
The connection diagram of Fig. 3 devices in order to control.
Wherein:1-unmanned aerial vehicle body, 2- positioning bolts, 3- compression springs, 4- nuts, 5- positioning plates, 6- articles carry case, 7- High-pressure gasbag, 8- interfaces one, 9- interfaces two, 10- micro air pumps, 11- air inlet pipe, 12- cooling gas check valves, 13- controllers, 14- Solenoid valve, 15- exhaust pipes, 16- power supplys.
Embodiment
To make the technical means, the creative features, the aims and the efficiencies achieved by the present invention easy to understand, with reference to Embodiment, the present invention is further explained.
As shown in Figure 1 to Figure 3, a kind of unmanned plane article loading device, including the article installed in 1 lower end of unmanned aerial vehicle body Case 6 is carried, the both sides that the article carries case 6 are equipped with positioning plate 5, and the positioning plate 5 passes through retaining mechanism and unmanned aerial vehicle body 1 Lower end be fastenedly connected, the lower end of the unmanned aerial vehicle body 1 is equipped with wire interface, wire interface and the electricity in unmanned aerial vehicle body 1 Source 16 is electrically connected, and it is a hollow babinet that the article, which carries case 6, and article carries the wherein open at one end of case 6 and is hinged with Chamber door (is not drawn into) in figure, and the upper surface that article carries case 6 is equipped with concave mounting groove, and miniature gas is provided with the mounting groove Pump 10, the micro air pump 10 is connected by conducting wire with wire interface, and the inner wall that the article carries case 6 is bonded with high-pressure gasbag 7, the high-pressure gasbag 7 is connected by air inlet pipe 11 with micro air pump 10, and cooling gas check valve 12 is provided with air inlet pipe 11, institute The outer wall for stating article carrying case 6 is equipped with the exhaust pipe 15 connected with high-pressure gasbag 7, and exhaust pipe 15 is equipped with solenoid valve 14, The outer wall that the article carries case 6 is equipped with controller 13, and described 13 one end of controller is connected by conducting wire with wire interface, and The other end is electrically connected with micro air pump 10 and solenoid valve 14 respectively by conducting wire.
In the present embodiment, the retaining mechanism includes positioning bolt 2, compression spring 3 and nut 4, and the positioning plate 5 is equipped with The location hole of up/down perforation, positioning bolt 2 are integrated part with unmanned aerial vehicle body 1, and compression spring 3 is sleeved on positioning bolt 2, and position spiral shell Bolt 2 passes through location hole, and is locked by nut 4, and 3 one end of compression spring and the upper surface of positioning plate 5 are in close contact, and the other end and nothing The lower face of man-machine fuselage 1 is in close contact.
In the present embodiment, the positioning plate 5 is equipped with four, and is evenly distributed on article and carries on the side wall of case 6, and fixed Position plate 5 carries case 6 with article and is integrated part.
In the present embodiment, the wire interface includes interface 1 and interface 29, interface 1 and interface 29 with nothing Power supply 16 in man-machine fuselage 1 is electrically connected, and solenoid valve 14 is connected with micro air pump 10 by conducting wire with interface 1, control 13 one end of device is connected by conducting wire with interface 29 and the other end is electrically connected by conducting wire and micro air pump 10 and solenoid valve 14 Connecing, controller 13 is used for the operating mode for controlling micro air pump 10 and solenoid valve 14, so that high-pressure gasbag 7 is pressurizeed and depressurized, Easy to be positioned and unloaded to article.
By being arranged compression spring 3 on positioning bolt 2, improve article and carry the stabilization that case 6 is installed with unmanned aerial vehicle body 1 Property, compression spring 3 is in compressive state, and such nut 4 will not produce loosening easily, is set on the inner wall by carrying case 6 in article High-pressure gasbag 7, when needing carrying article to be transported, places items within article and carries in case 6, it is right to start micro air pump 10 High-pressure gasbag 7 pressurizes, and high-pressure gasbag 7 can be expanded after pressurizeing and heaved, and such high-pressure gasbag 7 can closely be squeezed with the outer wall of article Go out, so as to be positioned to article, for unmanned plane during being transported to article, article will not produce the phenomenon rocked, The stability and security of unmanned plane operation are improved, meanwhile, when unmanned plane produces collision during forced landing with ground In the case of, high-pressure gasbag 7 can be effectively protected article, place article and be damaged.
The configuration of the present invention is simple, the positioning that can be stablized to article, unmanned plane is when transporting article, article Shaking phenomenon will not be produced, improves stability during unmanned plane during flying, and article can be effectively protected, prevents thing Product are damaged.
As known by the technical knowledge, the present invention can pass through the embodiment party of other essence without departing from its spirit or essential feature Case is realized.Therefore, embodiment disclosed above, all things considered, is all merely illustrative, not the only.Institute Have within the scope of the present invention or be included in the invention in the change being equal in the scope of the present invention.

Claims (4)

1. a kind of unmanned plane article loading device, it is characterised in that including the article carrying installed in unmanned aerial vehicle body (1) lower end Case (6), the both sides that the article carries case (6) are equipped with positioning plate (5), and the positioning plate (5) passes through retaining mechanism and unmanned plane The lower end of fuselage (1) is fastenedly connected, and the lower end of the unmanned aerial vehicle body (1) is equipped with wire interface, wire interface and unmanned plane machine Power supply (16) in body (1) is electrically connected, and it is a hollow babinet that the article, which carries case (6), and article carries case (6) wherein Open at one end and chamber door is hinged with, the upper surface that article carries case (6) is equipped with concave mounting groove, is provided with the mounting groove Micro air pump (10), the micro air pump (10) are connected by conducting wire with wire interface, and the inner wall that the article carries case (6) glues High-pressure gasbag (7) is had, the high-pressure gasbag (7) is connected by air inlet pipe (11) with micro air pump (10), and air inlet pipe (11) On cooling gas check valve (12) is installed, the outer wall that the article carries case (6) is equipped with the exhaust pipe connected with high-pressure gasbag (7) (15), and exhaust pipe (15) is equipped with solenoid valve (14), and the outer wall that the article carries case (6) is equipped with controller (13), institute Controller (13) one end is stated to be connected with wire interface by conducting wire, and the other end by conducting wire respectively with micro air pump (10) and Solenoid valve (14) is electrically connected.
A kind of 2. unmanned plane article loading device according to claim 1, it is characterised in that:The retaining mechanism includes fixed Position bolt (2), compression spring (3) and nut (4), the positioning plate (5) are equipped with the location hole of up/down perforation, positioning bolt (2) and Unmanned aerial vehicle body (1) is integrated part, and compression spring (3) is sleeved on positioning bolt (2), and positioning bolt (2) passes through location hole, and is passed through Nut (4) is locked, and compression spring (3) one end and the upper surface of positioning plate (5) are in close contact, and the other end and unmanned aerial vehicle body (1) Lower face is in close contact.
A kind of 3. unmanned plane article loading device according to claim 1, it is characterised in that:The positioning plate (5) is equipped with Four, and be evenly distributed on article and carry on the side wall of case (6), and positioning plate (5) carries case (6) with article and is integrated part.
A kind of 4. unmanned plane article loading device according to claim 1, it is characterised in that:The wire interface includes connecing One (8) of mouth and interface two (9), interface one (8) are electrically connected with interface two (9) with the power supply (16) in unmanned aerial vehicle body (1), Solenoid valve (14) is connected with micro air pump (10) by conducting wire with interface one (8), and controller (13) one end is by conducting wire with connecing The connection of two (9) of mouth and the other end pass through conducting wire and micro air pump (10) and solenoid valve (14) is electrically connected.
CN201810038079.5A 2018-01-16 2018-01-16 A kind of unmanned plane article loading device Pending CN107933928A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810038079.5A CN107933928A (en) 2018-01-16 2018-01-16 A kind of unmanned plane article loading device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810038079.5A CN107933928A (en) 2018-01-16 2018-01-16 A kind of unmanned plane article loading device

Publications (1)

Publication Number Publication Date
CN107933928A true CN107933928A (en) 2018-04-20

Family

ID=61937604

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810038079.5A Pending CN107933928A (en) 2018-01-16 2018-01-16 A kind of unmanned plane article loading device

Country Status (1)

Country Link
CN (1) CN107933928A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108388265A (en) * 2018-04-09 2018-08-10 广东思派康电子科技有限公司 A kind of four-axle aircraft and the goods transportation system based on the four-axle aircraft
CN109941450A (en) * 2019-03-26 2019-06-28 深圳市律远汇智科技有限公司 A kind of multi-functional unmanned flight's device
CN109969357A (en) * 2019-01-15 2019-07-05 深圳市安思科电子科技有限公司 A kind of rescue robot of mobility strong
CN111532432A (en) * 2020-05-07 2020-08-14 徐州徐薯食品研究院有限公司 Plant protection unmanned aerial vehicle is with preventing shaking medical kit
CN112124790A (en) * 2020-09-21 2020-12-25 姜高敏 Be applied to logistics distribution unmanned aerial vehicle's lightweight container

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105857615A (en) * 2016-05-16 2016-08-17 苏州金建达智能科技有限公司 Unmanned aerial vehicle with object transportation function of robot
CN106428568A (en) * 2016-11-08 2017-02-22 郑州郑航通用航空工业科技有限公司 Multifunctional double-layer plant protection box for electrodynamic unmanned aerial vehicle for plant protection and unmanned aerial vehicle
CN206384133U (en) * 2017-01-22 2017-08-08 衡阳云雁航空科技有限公司 Many rotor remote control distributor unmanned plane casings of charged pool case
CN107215466A (en) * 2017-05-12 2017-09-29 常州银鹰航空科技有限公司 A kind of plant protection unmanned plane is anti-to swing box body device and plant protection unmanned plane
CN206590129U (en) * 2017-03-29 2017-10-27 四川职业技术学院 A kind of logistics UAV system container
CN207389564U (en) * 2018-01-16 2018-05-22 安徽翼讯飞行安全技术有限公司 A kind of unmanned plane article loading device

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105857615A (en) * 2016-05-16 2016-08-17 苏州金建达智能科技有限公司 Unmanned aerial vehicle with object transportation function of robot
CN106428568A (en) * 2016-11-08 2017-02-22 郑州郑航通用航空工业科技有限公司 Multifunctional double-layer plant protection box for electrodynamic unmanned aerial vehicle for plant protection and unmanned aerial vehicle
CN206384133U (en) * 2017-01-22 2017-08-08 衡阳云雁航空科技有限公司 Many rotor remote control distributor unmanned plane casings of charged pool case
CN206590129U (en) * 2017-03-29 2017-10-27 四川职业技术学院 A kind of logistics UAV system container
CN107215466A (en) * 2017-05-12 2017-09-29 常州银鹰航空科技有限公司 A kind of plant protection unmanned plane is anti-to swing box body device and plant protection unmanned plane
CN207389564U (en) * 2018-01-16 2018-05-22 安徽翼讯飞行安全技术有限公司 A kind of unmanned plane article loading device

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108388265A (en) * 2018-04-09 2018-08-10 广东思派康电子科技有限公司 A kind of four-axle aircraft and the goods transportation system based on the four-axle aircraft
CN109969357A (en) * 2019-01-15 2019-07-05 深圳市安思科电子科技有限公司 A kind of rescue robot of mobility strong
CN109969357B (en) * 2019-01-15 2021-10-15 山东边健科技集团有限公司 Rescue robot with strong mobility
CN109941450A (en) * 2019-03-26 2019-06-28 深圳市律远汇智科技有限公司 A kind of multi-functional unmanned flight's device
CN111532432A (en) * 2020-05-07 2020-08-14 徐州徐薯食品研究院有限公司 Plant protection unmanned aerial vehicle is with preventing shaking medical kit
CN112124790A (en) * 2020-09-21 2020-12-25 姜高敏 Be applied to logistics distribution unmanned aerial vehicle's lightweight container
CN112124790B (en) * 2020-09-21 2021-06-18 苏州赛荣建筑装饰工程有限公司 Be applied to logistics distribution unmanned aerial vehicle's lightweight container

Similar Documents

Publication Publication Date Title
CN107933928A (en) A kind of unmanned plane article loading device
CN207389564U (en) A kind of unmanned plane article loading device
CN107380456B (en) Conformable pressure vessel
TWM517715U (en) Multi-axis aircraft capable of carrying life-saving equipment
CN110498136B (en) Air logistics transportation container
US9657856B2 (en) Regulating apparatus for a pressure activated one-way valve
CN205801548U (en) Three Degree Of Freedom simulated weightlessness air floating platform
CA3018303A1 (en) System and method for reinforcing aerostats
SA517390247B1 (en) Coaxial two-layered parachute
CN103600741B (en) Wheeled/air cushion convertible car for spacecraft transfer
CN206417212U (en) Unmanned plane All-in-One mission payload
CN207328843U (en) A kind of good unmanned plane of transportation stability
CN207257991U (en) Land buffer-type transport unmanned plane
CN111259488B (en) Oil transportation and thermal management integrated system for controlling temperature rise of fuel oil of high-speed aircraft
US10287027B2 (en) Expandable flexible fuel tank device and system for externally pressurized fuel systems
CN102704573A (en) Lift-type extension cabin
CN218806724U (en) Unmanned aerial vehicle's buffer
CN107150808A (en) A kind of delivery unmanned plane
CN206691375U (en) The landing platform of utricule type aircraft
CN103928743B (en) The loading of the inflating expanded parabolic antenna of a kind of fin-plate type and expansion controlling organization
CN203211516U (en) Matching apparatus for installation of onboard mission load of ship-based unmanned aerial vehicle (UAV)
CN208559742U (en) Undercarriage and aircraft
CN102530232A (en) Controllable hydrogen flight vehicle
CN111209632A (en) Design method of oil transportation thermal management system for controlling temperature rise of fuel oil of high-speed aircraft
CN209905068U (en) Portable commodity circulation cabin structure of unmanned aerial vehicle

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination