CN202175198U - Multifunctional rescue aircraft - Google Patents
Multifunctional rescue aircraft Download PDFInfo
- Publication number
- CN202175198U CN202175198U CN2011202626191U CN201120262619U CN202175198U CN 202175198 U CN202175198 U CN 202175198U CN 2011202626191 U CN2011202626191 U CN 2011202626191U CN 201120262619 U CN201120262619 U CN 201120262619U CN 202175198 U CN202175198 U CN 202175198U
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- aircraft
- flow guide
- aircraft body
- rescue
- multifunctional rescue
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Abstract
A multifunctional rescue aircraft comprises a remote controller, an aircraft body, a lifting device arranged on the aircraft body and used for controlling rising and falling of the aircraft, an engine for driving the lifting device and a remote control receiving device. The multifunctional rescue aircraft is characterized in that the lifting device comprises a flow guide cylinder with an open top, a propeller arranged in the flow guide cylinder and used for vertical lifting of the aircraft and a flow guide grate arranged at the bottom of the flow guide cylinder. Grating pieces of the flow guide grate are respectively in rotating connection with the flow guide cylinder, a micro motor on the aircraft body provides driving force to drive the grating pieces to rotate, and the rotation of the grating pieces is controlled by the remote controller. A hanging hook for hanging a rope is arranged at the bottom of the aircraft body. The multifunctional rescue aircraft has small volume and low construction cost, and obstacles are crossed to deal with danger and rescue lives by utilizing a flying function of the aircraft. Light urgent goods can be delivered, rescuing ropes and the like can be transferred by utilizing a carrying function of the aircraft, and stranded persons and environmental conditions can be observed in real time by utilizing a camera shooting function of the aircraft.
Description
Technical field
The utility model relates to a kind of wrecking equipment, specifically a kind of low-latitude flying rescue accessory equipment based on wireless remote control.
Background technology
In the existing stranded rescue, stranded like floods, fire is stranded, and cliff is stranded, and in the height rescue, usually there be obstacle, hazardous environment or the dangerous situation that can't go beyond in the rescue group because of rescue site, so that feel simply helpless.The rescue group goes to incur loss through delay best rescue opportunity near trapped personnel because of not employing large-scale wrecking equipment at short notice, brings difficulty for the follow-up work of rescue; And some large-scale wrecking equipments like autogyro, because its resource is rare, are difficult to be equipped with in numerous rescue occasions.
The utility model content
The utility model is for fear of the weak point that prior art exists, and provides that a kind of volume is little, cost is low, the multifunctional rescue aircraft of flexible operation, utilizes its flight function to realize leaping over obstacles, handle dangerous, the purpose of rescue life.
The utility model technical solution problem adopts following scheme:
The multifunctional rescue aircraft comprises and establishes remote controller, aircraft body, is arranged on the jacking system that the controlling aircraft on the aircraft body is risen and fallen, and is used to drive the driving engine of jacking system, and remote-receiver; Its constructional feature is: said jacking system comprises the guide shell of open top, the water conservancy diversion grid that is arranged at the screw propeller that is used for the aircraft vertical lift in the guide shell and is arranged on the guide shell bottom; Each grid sheet of said water conservancy diversion grid is rotationally connected with guide shell respectively, and the rotation of grid sheet is provided propulsive effort and controlled its rotation by remote controller by the miniature motor that is arranged on the aircraft body; The bottom of said aircraft body is provided with the stirrup that is used for suspension cord.
The utility model constructional feature also is:
Said jacking system has three groups, the setting that on the aircraft body, is centrosymmetric, and the grid sheet in said adjacent two jacking systems is 60 ° of angles and arranges.
Also be provided with the manipulator that is used for grasping objects and has auto-lock function on the said rescuing device body, said manipulator is provided propulsive effort and is controlled its motion by remote controller by the miniature motor that is arranged on the aircraft body.
Said rescuing device also is provided with camera head, and said camera head comprises video frequency pick-up head and the ground video display unit (VDU) that is arranged on the rescuing device body, and the vision signal that said video frequency pick-up head is gathered is given the ground video display unit (VDU) through transmission of wireless signals.Compared with present technology, the utility model beneficial effect is embodied in:
1, the utility model volume is little, cost is low, utilizes the flight function leaping over obstacles of aircraft, handles danger, rescues life; Utilize it to carry function and deliver light urgent article, transmit relief rope etc., utilize its camera function to come Real Time Observation indicator of trapped personnel and ambient conditions; In case of emergency can sacrifice aircraft, implement final relief through the extracting and the auto-lock function of manipulator.
2, the utility model is carried necessary medical diet etc. through flight, prolongs by tolerance time oppressive, the people that goes through dangers; Its camera head provides clear and real ambient conditions to the rescue group, for rescue decision-making, rescue mode provide the information support, thereby improve comprehensive rescue ability.
Description of drawings
Fig. 1 is the utility model front view.
Fig. 2 is the utility model upward view.
Fig. 3 is the utility model stereoscopic-state figure.
Label among the figure: 1 aircraft body, 2 guide shells, 3 screw propellers, 4 grid sheets, 5 stirrups, 6 manipulators, 7 video frequency pick-up heads, 8 land feet.
The utility model is further specified through the specific embodiment below in conjunction with accompanying drawing.
The specific embodiment
Referring to Fig. 1 to Fig. 3; The multifunctional rescue aircraft comprises that ground remote control device, band land the aircraft body 1 of feet 8, and 1 is provided with the jacking system that controlling aircraft is risen and fallen respectively on the aircraft body; Be used to drive the driving engine of jacking system, and remote-receiver; Wherein, Jacking system comprise open top guide shell 2, be arranged at screw propeller that is used for vertical lift 3 in the guide shell 2 and the water conservancy diversion grid that is arranged on guide shell 2 bottoms; Each grid sheet 4 of water conservancy diversion grid is rotationally connected with guide shell respectively, and the rotation of grid sheet provides propulsive effort by the miniature motor that is arranged on the aircraft body 1 and by its rotation of ground remote control device control; Be provided with the stirrup 5 that is used for suspension cord in the bottom of aircraft body 1.
Aircraft jacking system in the present embodiment has three groups, is separately positioned on settings that be centrosymmetric around the outside of aircraft body, and the grid sheet in adjacent two jacking systems is 60 ° of angles arrangements.Carry-on driving engine, miniature motor, remote-receiver and and parts such as power supply be fixedly installed on the medium position of aircraft body 1 respectively.
Also be provided with manipulator 6 and camera head on the aircraft of present embodiment, manipulator 6 is used for grasping objects and has auto-lock function, and manipulator 6 is provided propulsive effort and controlled its motion by the ground remote control device by the miniature motor that is arranged on the aircraft body; Camera head comprises the video frequency pick-up head 7 and ground video display unit (VDU) that is arranged on the rescuing device body, and the vision signal that video frequency pick-up head 7 is gathered is given the ground video display unit (VDU) through transmission of wireless signals.
In the practical implementation, the flight of aircraft is through three screw propellers, three grids, realizes vertical lift-off and aerial moving all around with propeller speed, the grid angle of various combination.Aircraft is controlled whole flight course by the ground remote control device.
Pass through the practicality of this aircraft of simulation environment casehistory below.
The cliff on the stranded opposite of example 1, one people, the rescue group can't directly pass by; And had near oppressive can stationary rope fixture; Hang up an end of light-high-strength cord on the aircraft stirrup, the other end is controlled by the rescue group, lets aircraft fly over indicator of trapped personnel at one's side through operating remote controller; Receive the oppressive lightweight cord that takes off, aircraft flies back; The rescue group ties up to sufficient intensity hawser one end on the lightweight cord, receives oppressive receipts cord, and final hawser arrives stranded people at one's side, and thick refreshing two ends are fixed, and so conveniently sets up the rope bridge, and the rescue group implements rescue through the rope bridge, and indicator of trapped personnel is taken back.If can't set up the rope bridge, also can transport necessary food and drink and medicine earlier, guarantee the rescue of indicator of trapped personnel wait autogyro.
Example 2: someone claims and jumps out of the building on high-rise mansion platform, and threaten the rescue group must not near; The rescue group can disperse its attention, discharges the aircraft that has the light-high-strength cord from other directions, lives its arm or shank with the manipulator back-up tong; Sacrifice aircraft, implement rescue.
Claims (4)
1. multifunctional rescue aircraft comprises and establishes remote controller, aircraft body, is arranged on the jacking system that the controlling aircraft on the aircraft body is risen and fallen, and is used to drive the driving engine of jacking system, and remote-receiver; It is characterized in that: said jacking system comprises the guide shell of open top, the water conservancy diversion grid that is arranged at the screw propeller that is used for the aircraft vertical lift in the guide shell and is arranged on the guide shell bottom; Each grid sheet of said water conservancy diversion grid is rotationally connected with guide shell respectively, and the rotation of grid sheet is provided propulsive effort and controlled its rotation by remote controller by the miniature motor that is arranged on the aircraft body; The bottom of said aircraft body is provided with the stirrup that is used for suspension cord.
2. multifunctional rescue aircraft according to claim 1 is characterized in that, said jacking system has three groups, the setting that on the aircraft body, is centrosymmetric, and the grid sheet in said adjacent two jacking systems is 60 ° of angles and arranges.
3. multifunctional rescue aircraft according to claim 1; It is characterized in that; Also be provided with the manipulator that is used for grasping objects and has auto-lock function on the said rescuing device body, said manipulator is provided propulsive effort and is controlled its motion by remote controller by the miniature motor that is arranged on the aircraft body.
4. multifunctional rescue aircraft according to claim 1; It is characterized in that; Said rescuing device also is provided with camera head; Said camera head comprises video frequency pick-up head and the ground video display unit (VDU) that is arranged on the rescuing device body, and the vision signal that said video frequency pick-up head is gathered is given the ground video display unit (VDU) through transmission of wireless signals.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202626191U CN202175198U (en) | 2011-07-21 | 2011-07-21 | Multifunctional rescue aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202626191U CN202175198U (en) | 2011-07-21 | 2011-07-21 | Multifunctional rescue aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202175198U true CN202175198U (en) | 2012-03-28 |
Family
ID=45865097
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011202626191U Expired - Fee Related CN202175198U (en) | 2011-07-21 | 2011-07-21 | Multifunctional rescue aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN202175198U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102689313A (en) * | 2012-06-11 | 2012-09-26 | 长安大学 | High-altitude dangerous environment article clearing system and clearing method based on flying robot |
| CN106005394A (en) * | 2016-07-22 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | Rescue aircraft |
| CN106043683A (en) * | 2016-04-27 | 2016-10-26 | 深圳市拓灵者科技有限公司 | An aircraft and an outer device thereof |
| CN106064378A (en) * | 2016-06-07 | 2016-11-02 | 南方科技大学 | Control method and device for unmanned aerial vehicle mechanical arm |
| CN108673550A (en) * | 2016-03-21 | 2018-10-19 | 珠海市磐石电子科技有限公司 | A kind of robot device |
-
2011
- 2011-07-21 CN CN2011202626191U patent/CN202175198U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102689313A (en) * | 2012-06-11 | 2012-09-26 | 长安大学 | High-altitude dangerous environment article clearing system and clearing method based on flying robot |
| CN108673550A (en) * | 2016-03-21 | 2018-10-19 | 珠海市磐石电子科技有限公司 | A kind of robot device |
| CN106043683A (en) * | 2016-04-27 | 2016-10-26 | 深圳市拓灵者科技有限公司 | An aircraft and an outer device thereof |
| CN106064378A (en) * | 2016-06-07 | 2016-11-02 | 南方科技大学 | Control method and device for unmanned aerial vehicle mechanical arm |
| CN106005394A (en) * | 2016-07-22 | 2016-10-12 | 中国航空工业集团公司西安飞机设计研究所 | Rescue aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120328 Termination date: 20120721 |