CN207029554U - A kind of simple unmanned plane disaster relief delivery device - Google Patents

A kind of simple unmanned plane disaster relief delivery device Download PDF

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Publication number
CN207029554U
CN207029554U CN201720655529.6U CN201720655529U CN207029554U CN 207029554 U CN207029554 U CN 207029554U CN 201720655529 U CN201720655529 U CN 201720655529U CN 207029554 U CN207029554 U CN 207029554U
Authority
CN
China
Prior art keywords
unmanned plane
electromagnet
delivery device
disaster relief
utility
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.)
Expired - Fee Related
Application number
CN201720655529.6U
Other languages
Chinese (zh)
Inventor
何腾飞
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.)
Shenzhen Flying Technology Co Ltd
Original Assignee
Shenzhen Flying Technology Co 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 Shenzhen Flying Technology Co Ltd filed Critical Shenzhen Flying Technology Co Ltd
Priority to CN201720655529.6U priority Critical patent/CN207029554U/en
Application granted granted Critical
Publication of CN207029554U publication Critical patent/CN207029554U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of simple unmanned plane disaster relief delivery device; belong to unmanned plane apparatus field; including drawing umbrella, storage tank and electromagnet; the drawing umbrella is connected with parachute, and the parachute is connected by coupling bar with protection shell, and the protection shell is wrapped in outside the storage tank; the electromagnet is connected with instruction socket; the electromagnet is connected with suction tray, and the storage tank bottom is provided with counter weight base, and cushion pad is provided with below the counter weight base.Beneficial effect is:The utility model can be electromagnetic force by electrical power conversion, absorption is dropped on unmanned plane by telecommand, has the advantages of simple to operate, cost is cheap, there is counterbalancing effect and pooling feature simultaneously, the utility model can be avoided to topple and damage after landing.

Description

A kind of simple unmanned plane disaster relief delivery device
Technical field
The utility model belongs to unmanned plane apparatus field, and in particular to a kind of simple unmanned plane disaster relief delivery device.
Background technology
Unmanned plane is the abbreviation of unmanned remote controlled aircraft, and contrasting manned machine has that cost is low, manipulation is simple, load-carrying Amount is big, requires the advantages of low to weather, landform, therefore more and more extensive answer is suffered from fields such as the disaster relief, meteorology, military affairs With.When there is the condition of a disaster generation, the people of the disaster relief very first time can not enter disaster area, so just needing to launch the disaster relief by unmanned plane Goods and materials, it is therefore desirable to a kind of device that unmanned plane can be easy to launch disaster relief supplies.
Utility model content
The purpose of this utility model is that to solve the above problems and provides a kind of simple unmanned plane disaster relief and launch dress Put.
The utility model is achieved through the following technical solutions above-mentioned purpose:
A kind of simple unmanned plane disaster relief delivery device, including umbrella, storage tank and electromagnet are drawn, the drawing umbrella and parachute phase Connection, the parachute are connected by coupling bar with protection shell, and the protection shell is wrapped in outside the storage tank, institute State electromagnet with instruction socket to be connected, the electromagnet is connected with suction tray, and the storage tank bottom is provided with counterweight bottom Seat, the counter weight base lower section are provided with cushion pad.
In said structure, the utility model is connected with the control system of unmanned plane by the instruction socket, by institute State electromagnet and produce electromagnetic field, and adsorbed the utility model on unmanned plane hanger by the suction tray, when needing to launch During goods and materials, staff sends telecommand, and the instruction socket disconnects electrical connection, and electromagnetic field caused by the electromagnet disappears Lose, the absorption affinity of the suction tray disappears, and the utility model drops from unmanned plane hanger, and opens the drawing umbrella simultaneously, leads to Cross the drawing umbrella and pull open the parachute, complete this air-drop.
In order to further improve performance of the present utility model, the drawing umbrella is connected with the parachute by rope, The parachute is fixedly connected with the coupling bar.
In order to further improve performance of the present utility model, the coupling bar is welded on one with the protection shell Rise, the protection shell and the electromagnet nested encryptions.
In order to further improve performance of the present utility model, the instruction socket electrically connects with the electromagnet, institute Electromagnet is stated to electrically connect with the suction tray.
In order to further improve performance of the present utility model, the electromagnet, the quantity of the suction tray are respectively Two, it is symmetrically mounted on the utility model both sides.
In order to further improve performance of the present utility model, the protection shell is fixed with the counter weight base to be connected Connect, the counter weight base is fixedly connected with the cushion pad.
In order to further improve performance of the present utility model, the material of the counter weight base can be irony, described Cushion pad is highly elastic material.
Beneficial effect is:The utility model can be electromagnetic force by electrical power conversion, adsorb on unmanned plane, by distant Control instruction is dropped, and has the advantages of simple to operate, cost is cheap, while has counterbalancing effect and pooling feature, can be kept away Topple and damage after exempting from the utility model landing.
Brief description of the drawings
Fig. 1 is a kind of front view of simple unmanned plane disaster relief delivery device described in the utility model.
Description of reference numerals is as follows:
1st, umbrella is drawn;2nd, parachute;3rd, coupling bar;4th, storage tank;5th, socket is instructed;6th, electromagnet;7th, suction tray;8th, protect Protect shell;9th, counter weight base;10th, cushion pad.
Embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings:
As shown in figure 1, a kind of simple unmanned plane disaster relief delivery device, including umbrella 1, storage tank 4 and electromagnet 6 are drawn, draw umbrella 1 It is connected with parachute 2, parachute 2 is connected by coupling bar 3 with protection shell 8, and protection shell 8 is wrapped in outside storage tank 4 Portion, electromagnet 6 are connected with instruction socket 5, and electromagnet 6 is connected with suction tray 7, and the bottom of storage tank 4 is provided with counter weight base 9, the lower section of counter weight base 9 is provided with cushion pad 10.
In said structure, by instructing socket 5 that the utility model is connected with the control system of unmanned plane, by electromagnet 6 produce electromagnetic field, and are adsorbed the utility model on unmanned plane hanger by suction tray 7, when needing to launch goods and materials, work Personnel send telecommand, and instruction socket 5 disconnects electrical connection, and electromagnetic field caused by electromagnet 6 disappears, the absorption affinity of suction tray 7 Disappear, the utility model drops from unmanned plane hanger, and opens simultaneously and draw umbrella 1, by drawing umbrella 1 to pull open parachute 2, completes this Secondary air-drop.
In order to further improve performance of the present utility model, umbrella 1 is drawn to be connected with parachute 2 by rope, parachute 2 Be fixedly connected with coupling bar 3,2 can be released a parachute by drawing umbrella 1, the situation for avoiding parachute 2 from not opening, coupling bar 3 with Protection shell 8 welds together, and parachute 2 can be fixed on by coupling bar 3 on protection shell 8, provided for the utility model Aerostatic buoyancy, protection shell 8 and the nested encryptions of electromagnet 6, protection shell 8 can be that electromagnet 6 provides structural support, and instruction is inserted Mouth 5 electrically connects with electromagnet 6, and instruction socket 5 can receive the instruction from unmanned plane, controls the on off operating mode of electromagnet 6, electricity Magnet 6 electrically connects with suction tray 7, and electromagnet 6, the quantity of suction tray 7 are respectively two, are symmetrically mounted on the utility model two Electrical power conversion can be electromagnetic field by side, electromagnet 6, be adsorbed by suction tray 7 on unmanned plane hanger, and keep balancing, side Just drop, protection shell 8 is fixedly connected with counter weight base 9, and counter weight base 9 can provide the work of pose adjustment for the utility model With, avoid air-drop after topple over, counter weight base 9 is fixedly connected with cushion pad 10, and cushion pad 10 can provide for the utility model Ground buffers, and avoids interior items from damaging, the material of counter weight base 9 can be irony, and cost is relatively low, and cushion pad 10 is high resiliency material Material, can improve buffering effect.
General principle, principal character and advantage of the present utility model has been shown and described above.The technical staff of the industry It should be appreciated that the utility model is not restricted to the described embodiments, the simply explanation described in above-described embodiment and specification is originally The principle of utility model, on the premise of the spirit and scope of the utility model is not departed from, the utility model also has various change And improvement, these changes and improvements are both fallen within claimed the scope of the utility model.The utility model requires protection scope Defined by appended claims and its effect thing.

Claims (7)

  1. A kind of 1. simple unmanned plane disaster relief delivery device, it is characterised in that:Including drawing umbrella, storage tank and electromagnet, the drawing umbrella It is connected with parachute, the parachute is connected by coupling bar with protection shell, and the protection shell is wrapped in the storage Outside thing case, the electromagnet is connected with instruction socket, and the electromagnet is connected with suction tray, and the storage tank bottom is set Counter weight base is equipped with, cushion pad is installed below the counter weight base.
  2. A kind of 2. simple unmanned plane disaster relief delivery device according to claim 1, it is characterised in that:It is described drawing umbrella with it is described Parachute is connected by rope, and the parachute is fixedly connected with the coupling bar.
  3. A kind of 3. simple unmanned plane disaster relief delivery device according to claim 1, it is characterised in that:The coupling bar and institute State protection shell to weld together, the protection shell and the electromagnet nested encryptions.
  4. A kind of 4. simple unmanned plane disaster relief delivery device according to claim 1, it is characterised in that:It is described instruction socket with The electromagnet electrical connection, the electromagnet electrically connect with the suction tray.
  5. A kind of 5. simple unmanned plane disaster relief delivery device according to claim 1, it is characterised in that:The electromagnet, institute The quantity for stating suction tray is respectively two, is symmetrically mounted on simple unmanned plane disaster relief delivery device both sides.
  6. A kind of 6. simple unmanned plane disaster relief delivery device according to claim 1, it is characterised in that:It is described protection shell with The counter weight base is fixedly connected, and the counter weight base is fixedly connected with the cushion pad.
  7. A kind of 7. simple unmanned plane disaster relief delivery device according to claim 1, it is characterised in that:The counter weight base Material is irony, and the cushion pad is highly elastic material.
CN201720655529.6U 2017-06-07 2017-06-07 A kind of simple unmanned plane disaster relief delivery device Expired - Fee Related CN207029554U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720655529.6U CN207029554U (en) 2017-06-07 2017-06-07 A kind of simple unmanned plane disaster relief delivery device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720655529.6U CN207029554U (en) 2017-06-07 2017-06-07 A kind of simple unmanned plane disaster relief delivery device

Publications (1)

Publication Number Publication Date
CN207029554U true CN207029554U (en) 2018-02-23

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720655529.6U Expired - Fee Related CN207029554U (en) 2017-06-07 2017-06-07 A kind of simple unmanned plane disaster relief delivery device

Country Status (1)

Country Link
CN (1) CN207029554U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108974362A (en) * 2018-07-20 2018-12-11 中国空空导弹研究院 To ammunition locking arrangement and aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108974362A (en) * 2018-07-20 2018-12-11 中国空空导弹研究院 To ammunition locking arrangement and aircraft

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180223

Termination date: 20190607

CF01 Termination of patent right due to non-payment of annual fee