CN209506022U - The accurate automatic life-saving apparatus of height launched for unmanned plane - Google Patents

The accurate automatic life-saving apparatus of height launched for unmanned plane Download PDF

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Publication number
CN209506022U
CN209506022U CN201920141727.XU CN201920141727U CN209506022U CN 209506022 U CN209506022 U CN 209506022U CN 201920141727 U CN201920141727 U CN 201920141727U CN 209506022 U CN209506022 U CN 209506022U
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China
Prior art keywords
shell
steering
cabin
valve
unmanned plane
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Active
Application number
CN201920141727.XU
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Chinese (zh)
Inventor
祁正岩
李树森
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 Xinglong Steel Structure Co.,Ltd.
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Qianmei Aviation Technology Xingtai Co Ltd
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Application filed by Qianmei Aviation Technology Xingtai Co Ltd filed Critical Qianmei Aviation Technology Xingtai Co Ltd
Priority to CN201920141727.XU priority Critical patent/CN209506022U/en
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Publication of CN209506022U publication Critical patent/CN209506022U/en
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Abstract

Precisely automatic life-saving apparatus is related to lifesaving appliance field to the height launched for unmanned plane.When mainly to solve current sea rescue, launch what lifesaving appliance was designed by the problem that situations such as weather is influenced to cause placement position not accurate by unmanned plane.It includes shell, there is infrared tracing sensor in photoelectricity cabin;There are two steering engines in steering gear flat, and the rocker arm outer end of two steering engines is connected with both direction rudder respectively;Dioxide bottle is installed in function cabin, solenoid valve is installed on the gas outlet of dioxide bottle, the outlet of solenoid valve is connected with tracheae, and the other end of tracheae is connected with the air inlet for folding lifebuoy, folds and is equipped with valve on the shell above lifebuoy;Battery, controller, motor are installed in piggyback pod, has propeller on motor power output shaft, has protective cover outside propeller.Advantage is can be automatically moved into indicator of trapped personnel at one's side after dispensing, improves lifesaving effect.

Description

The accurate automatic life-saving apparatus of height launched for unmanned plane
Technical field:
The utility model relates to lifesaving appliance fields, fill more particularly to a kind of automatic lifesaving launched for unmanned plane It sets.
Background technique:
At present when sea rescue, lifesaving appliance can be launched by unmanned plane.This mode is influenced to cause by situations such as weather Placement position is not accurate, and lifesaving appliance cannot reach near indicator of trapped personnel.
Summary of the invention:
The technical problem to be solved by the utility model is to provide it is a kind of can reach automatically indicator of trapped personnel at one's side for nothing The accurate automatic life-saving apparatus of height of man-machine dispensing.
Above-mentioned purpose is achieved in that it includes shell, be divided into from front to back in shell photoelectricity cabin, steering gear flat, Function cabin, piggyback pod are equipped with infrared tracing sensor in photoelectricity cabin;There are two steering engines, shell also to set outside for installation in steering gear flat There are two rudder, the rocker arm of two steering engines is stretched out from shell, the rocker arm outer end of two steering engines respectively with both direction rudder phase Connection;Dioxide bottle is installed in function cabin, solenoid valve is installed on the gas outlet of dioxide bottle, solenoid valve goes out Mouth is connected with tracheae, and the other end of tracheae is connected with the air inlet for folding lifebuoy, folds and pacify on the shell above lifebuoy Equipped with valve;Battery, controller, motor are installed, the power output shaft of motor is stretched out from housing rear end, is located at shell in piggyback pod Propeller is installed on the motor power output shaft outside body, is equipped with protective cover outside propeller, the front end of protective cover is fixed on On shell.Shell is made by engineering plastics.
Include in controller infrared signal processing module, two steering engine controllers, solenoid relay valve, electric machine controller, Processor, power module;Wherein power module is connect with battery by conducting wire, power module and infrared signal processing module, two A steering engine controller, solenoid relay valve, electric machine controller, processor are all connected by conducting wire respectively;Processor and infrared letter Number processing module, two steering engine controllers, solenoid relay valve, electric machine controllers all pass through conducting wire respectively and connect;Infrared signal Processing module is connect with infrared tracing sensor by electric wire, and two steering engines are connected with two steering engine controllers by electric wire respectively It connects, solenoid valve is connect with solenoid relay valve by electric wire, and motor is connect with electric machine controller by electric wire.
The utility model has the advantages that: after being launched using unmanned plane, infrared tracing sensor tracks the infrared letter of indicator of trapped personnel Number, signal is transmitted to infrared signal processing module, information characteristics are transmitted to processor by infrared signal processing module, and processor passes through Corresponding signal is transmitted to steering engine controller and electric machine controller by operation, and the motor control present apparatus moves forward or back, steering engine control The direction of the present apparatus, it is close to indicator of trapped personnel.Reach indicator of trapped personnel at one's side when, processor issue signal control solenoid valve open to Lifebuoy inflation is folded, lifebuoy is folded and opens valve pop-up.The present apparatus can be automatically moved into indicator of trapped personnel at one's side after dispensing, It is used for indicator of trapped personnel.Lifesaving effect can be greatly improved using the present apparatus.
Detailed description of the invention:
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the structural schematic diagram of controller in the utility model.
Specific embodiment:
Referring to Fig.1, it includes shell 1, is divided into photoelectricity cabin 2 in shell from front to back, steering gear flat 3, function cabin 4, moves Power cabin 5 is equipped with infrared tracing sensor 6 in photoelectricity cabin;There are two steering engines 7, shell to be additionally provided with two outside for installation in steering gear flat The rocker arm of rudder 8, two steering engines is stretched out from shell, and the rocker arm outer end of two steering engines is connected with both direction rudder respectively; Dioxide bottle 9 is installed in function cabin, solenoid valve 10, the outlet of solenoid valve are installed on the gas outlet of dioxide bottle It is connected with tracheae 11, the other end of tracheae is connected with the air inlet for folding lifebuoy 12, folds on the shell above lifebuoy Valve 13 is installed;Battery 14, controller 15, motor 16 be installed, the power output shaft of motor is from housing rear end in piggyback pod It stretches out, propeller 16 is installed on the motor power output shaft of hull outside, protective cover 17, protection are equipped with outside propeller The front end of cover is fixed on shell.Shell is made by engineering plastics.
It include infrared signal processing module 18, two steering engine controllers 19, solenoid relay valve in controller referring to Fig. 2 20, electric machine controller 21, processor 22, power module 23;Wherein power module is connect with battery by conducting wire, power module with Infrared signal processing module, two steering engine controllers, solenoid relay valve, electric machine controller, processors all pass through conducting wire respectively Connection;Processor all leads to respectively with infrared signal processing module, two steering engine controllers, solenoid relay valve, electric machine controllers Cross conducting wire connection;Infrared signal processing module is connect with infrared tracing sensor by electric wire, two steering engines respectively with two rudders Machine controller is connected by electric wire, and solenoid valve is connect with solenoid relay valve by electric wire, and motor and electric machine controller pass through electricity Line connection.

Claims (2)

1. for the accurate automatic life-saving apparatus of height that unmanned plane is launched, including shell (1), it is characterized in that: in shell from front to back It is divided into photoelectricity cabin (2), steering gear flat (3), function cabin (4), piggyback pod (5), infrared tracing sensor is installed in photoelectricity cabin (6);Installation is additionally provided with both direction rudder (8) there are two steering engine (7) outside shell in steering gear flat, and the rocker arms of two steering engines is from shell The rocker arm outer end of middle stretching, two steering engines is connected with both direction rudder respectively;Dioxide bottle is installed in function cabin (9), it is equipped on the gas outlet of dioxide bottle solenoid valve (10), the outlet of solenoid valve is connected with tracheae (11), tracheae The other end is connected with the air inlet for folding lifebuoy (12), folds and is equipped with valve (13) on the shell above lifebuoy;It is dynamic Battery (14), controller (15), motor (16) are installed, the power output shaft of motor stretches out from housing rear end, is located in power cabin It is equipped on the motor power output shaft of hull outside propeller (17), is equipped with protective cover (18) outside propeller, protective cover Front end is fixed on shell.
2. the height accurate automatic life-saving apparatus described in accordance with the claim 1 launched for unmanned plane, it is characterized in that: in controller Including infrared signal processing module (24), two steering engine controllers (19), solenoid relay valve (20), electric machine controller (21), Processor (22), power module (23);Wherein power module is connect with battery by conducting wire, and power module and infrared signal are handled Module, two steering engine controllers, solenoid relay valve, electric machine controller, processors are all connected by conducting wire respectively;Processor with Infrared signal processing module, two steering engine controllers, solenoid relay valve, electric machine controllers are all connected by conducting wire respectively;It is red External signal processing module is connect with infrared tracing sensor by electric wire, and two steering engines pass through electricity with two steering engine controllers respectively Line connection, solenoid valve are connect with solenoid relay valve by electric wire, and motor is connect with electric machine controller by electric wire.
CN201920141727.XU 2019-01-28 2019-01-28 The accurate automatic life-saving apparatus of height launched for unmanned plane Active CN209506022U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920141727.XU CN209506022U (en) 2019-01-28 2019-01-28 The accurate automatic life-saving apparatus of height launched for unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920141727.XU CN209506022U (en) 2019-01-28 2019-01-28 The accurate automatic life-saving apparatus of height launched for unmanned plane

Publications (1)

Publication Number Publication Date
CN209506022U true CN209506022U (en) 2019-10-18

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920141727.XU Active CN209506022U (en) 2019-01-28 2019-01-28 The accurate automatic life-saving apparatus of height launched for unmanned plane

Country Status (1)

Country Link
CN (1) CN209506022U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111899476A (en) * 2020-07-17 2020-11-06 江苏曌丰智能安防有限公司 Geological disaster early warning sensor for self-organized network self-built coordinates by utilizing rocket spreading

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111899476A (en) * 2020-07-17 2020-11-06 江苏曌丰智能安防有限公司 Geological disaster early warning sensor for self-organized network self-built coordinates by utilizing rocket spreading

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Effective date of registration: 20210825

Address after: 231323 west side of Qiantai Road, Hengshan Town, Huoshan County, Lu'an City, Anhui Province

Patentee after: Anhui Xinglong Steel Structure Co.,Ltd.

Address before: 054000 room 602, building 7, science and Technology Park (Xingtai) of Hebei University of technology, No. 1889, Zhongxing East Street, Qiaodong District, Xingtai City, Hebei Province

Patentee before: QIANMEI AVIATION TECHNOLOGY XINGTAI Co.,Ltd.