CN201604798U - Remote-control rescue aircraft - Google Patents
Remote-control rescue aircraft Download PDFInfo
- Publication number
- CN201604798U CN201604798U CN2010201251555U CN201020125155U CN201604798U CN 201604798 U CN201604798 U CN 201604798U CN 2010201251555 U CN2010201251555 U CN 2010201251555U CN 201020125155 U CN201020125155 U CN 201020125155U CN 201604798 U CN201604798 U CN 201604798U
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- rescue
- aircraft
- remote
- rope
- bearing box
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- Buildings Adapted To Withstand Abnormal External Influences (AREA)
Abstract
The utility model relates to a remote-control rescue aircraft, comprising an aircraft body, a motor, a propeller and a remote controller, wherein a remote control receiver is arranged above the motor in the aircraft body; a rope is arranged below the aircraft body; a bearing box is arranged below the rope; two sides of the bearing box are provided with sliding doors; the top of the bearing box is a transparent cover, the lower edge at the external side thereof is provided with a pulley sheathed with the rope, and the bottom thereof is provided with a universal wheel; an operator sends out command signals by a remote control emitter to operate the aircraft to takeoff vertically; and when the aircraft arrives a rescue site, the operator carries out the rescue work. The remote-control rescue aircraft has simple and contact structure, and labor-saving and convenient work; and the rescue efficiency improves continuously with the proficiency of the operation; therefore, the remote-control rescue aircraft is suitable for the triphibian rescue work of water, land and air, and is suitable for disaster regions with the emergency rescue such as fire hazard, flood disaster, earthquake, bane disaster and the like.
Description
Technical field
The utility model relates to a kind of emergency rescue device, specifically, relates to a kind of remote control rescue aircraft that is used for disasters such as fire big flood earthquake calamity poison calamity.
Background technology
At present, at the burst fire, big flood, earthquake calamity, in face of the great disasters such as poison calamity, the mankind possess certain rescue ability of combating a natural disaster, but, drop into timeliness, still there is deficiency in aspects such as safety and stability, be subjected to the restriction of geographical location circumstances condition easily, can not be rapidly in time drop into steadily comprehensively and combat a natural disaster rescue work, and the safe poor-performing of safety, cause that to combat a natural disaster salvage work's effect not ideal enough, particularly obstructed at access to information in short road from far-off regions, rescue group's salvage gear can not put in place fast, especially in the search and rescue target, implementing the rescue work aspect is limited to, affect best rescue opportunity adversely, current main transportation salvage gear is vehicle and the vehicle-mounted lifesaving ship etc. of charging, and very easily is subjected to the traffic condition restriction of water route, land route, large aircraft is difficult in the hazardous environment operation of mountain valley, narrow basin, and in abominable weather environment critical moment, the crew is difficult to the accurate wrecked masses that sue and labour among in deep distress, and it is panic to comprise that city neighborhood commodity roof is escaped the resident of difficulty of fire poison calamity floods, the perhaps common people that struggle to call for help in the flood wave, for the moment be difficult to the flee danger condition, therefore, along with starting construction emergency management and rescue system, need the remote control rescue aircraft of urgent execution rescue that to be in time rapidly, and extensively carry out penetration and promotion and use.
The utility model content
The purpose of this utility model is in order to overcome the deficiencies in the prior art, a kind of light and flexible to be provided, and is easy and simple to handle, time saving and energy saving, easily efficient, as long as one man operation can be finished the function of efficient rescue quick and precisely, realize the remote control rescue aircraft of the safe purpose of highly effective and safe.
In order to achieve the above object, the utility model has adopted following technical scheme:
A kind of remote control rescue aircraft, comprise fuselage (1), driving engine (2) and screw propeller (3) and remote controller (8), rope (5) is installed below the fuselage (1), bearing box (6) is installed below the rope (5), and bearing box (6) both sides are equipped with sliding door (7), and the case top is translucent cover (9), outside bottom is equipped with sets of cords pulley (10), and the bottom is equipped with cardan wheel (11).
Receiver of remote-control sytem (4) is installed in driving engine (2) top, receive the instruction of remote controller (8), remote controller (8) is provided with controls the height landing of taking off, the speed speed, about turn to this several buttons, aircraft flight adopts fuel oil as power, and rope bearing box translucent cover is the dust-proof and earthquake-proof material of fire-proof and water-proof.
The utility model rescue work is in time safe and reliable rapidly, the target of suing and labouring is accurately safe, rescue scope object is extensive, rescue respond well to the people that meet with disasters such as fire big flood earthquake calamity poison calamity, the environmental area comformability is strong, flies height speed steering operation freely, and the accurate safety of the object of suing and labouring is safe, the emergency management and rescue of dwelling of suitable land, water and air three are fit to the emergency relief operation of disasters such as fire big flood poison calamity earthquake calamity.
Description of drawings
Fig. 1 is a lateral plan of the present utility model;
Fig. 2 is a upward view of the present utility model;
The specific embodiment
Below in conjunction with drawings and Examples the utility model is described in further detail: as depicted in figs. 1 and 2, the utility model is by fuselage 1, driving engine 2 and screw propeller 3 and remote controller 8 are formed, receiver of remote-control sytem 4 is installed in driving engine 2 tops, by receiving the operation signal of remote controller 8, operating aircraft landing dogled, and rope 5 is installed below fuselage 1, bearing box 6 is installed below the rope 5, sliding door 7 is installed in bearing box 6 both sides, the case top is translucent cover 9, the following installation sleeve rope pulley 10 in the outside, and cardan wheel 11 is installed in the bottom.
Aircraft flight adopts fuel oil as power, rope bearing box translucent cover is the dust-proof and earthquake-proof material of fire-proof and water-proof, check before the operating personal operation that each working part performance of debugging is intact, take off vertically by controller 8 commander's aircrafts, after arriving required rescue work place, remote controller 8 sends instruction, bearing box is accurately dropped to the rescue object at one's side, allow the personnel of receiving aid enter the transfer of closing the door in the bearing box immediately, the terrestrial water Orly draws, and the roof space is suspended, hightail the dangerous condition of disaster, telecontrolled aircraft realizes the rescue work purpose around the touring flight rescue of disaster scope, finishes rescue task.
Adopted such scheme, remote control rescue aircraft tight Minato simple in structure, the laborsaving convenience of operation, the rescue work efficiency improves constantly along with the skilled operation degree, is fit to wide popularization and application fire big flood earthquake calamity poison calamity or the like emergency management and rescue operation.
Claims (3)
1. remote control rescue aircraft, comprise fuselage (1), driving engine (2) and screw propeller (3) and remote controller (8), it is characterized in that: rope (5) is installed below the fuselage (1), bearing box (6) is installed below the rope (5), bearing box (6) both sides are equipped with sliding door (7), case top is translucent cover (9), sets of cords pulley (10) is installed below the outside, and the bottom is equipped with cardan wheel (11).
2. remote control rescue aircraft according to claim 1, it is characterized in that: receiver of remote-control sytem (4) is installed in driving engine (2) top, receives the instruction of remote controller (8), and remote controller (8) is provided with the height landing of taking off of control autogyro, the speed speed, about turn to this several buttons.
3. remote control rescue aircraft according to claim 1 is characterized in that: aircraft flight adopts fuel oil as power, and rope bearing box translucent cover is the dust-proof and earthquake-proof material of fire-proof and water-proof.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201251555U CN201604798U (en) | 2010-03-02 | 2010-03-02 | Remote-control rescue aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2010201251555U CN201604798U (en) | 2010-03-02 | 2010-03-02 | Remote-control rescue aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201604798U true CN201604798U (en) | 2010-10-13 |
Family
ID=42949506
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2010201251555U Expired - Fee Related CN201604798U (en) | 2010-03-02 | 2010-03-02 | Remote-control rescue aircraft |
Country Status (1)
Country | Link |
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CN (1) | CN201604798U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105405336A (en) * | 2015-12-30 | 2016-03-16 | 大连海事大学 | Helicopter rescue simulated training system |
CN105658519A (en) * | 2013-08-26 | 2016-06-08 | 谷歌公司 | Mechanisms for lowering payload to ground from uav |
-
2010
- 2010-03-02 CN CN2010201251555U patent/CN201604798U/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105658519A (en) * | 2013-08-26 | 2016-06-08 | 谷歌公司 | Mechanisms for lowering payload to ground from uav |
US9783297B2 (en) | 2013-08-26 | 2017-10-10 | X Development Llc | Mechanisms for lowering a payload to the ground from a UAV |
US9957046B2 (en) | 2013-08-26 | 2018-05-01 | X Development Llc | Mechanisms for lowering a payload to the ground from a UAV |
US10106257B2 (en) | 2013-08-26 | 2018-10-23 | X Development Llc | Mechanisms for lowering a payload to the ground from a UAV |
CN105405336A (en) * | 2015-12-30 | 2016-03-16 | 大连海事大学 | Helicopter rescue simulated training system |
WO2017114445A1 (en) * | 2015-12-30 | 2017-07-06 | 大连海事大学 | Simulation system for helicopter rescue training |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
DD01 | Delivery of document by public notice |
Addressee: Xie Lunguo Document name: Notification to Pay the Fees |
|
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101013 Termination date: 20120302 |