CN205959352U - System for a slide expandes for preventing due to carelessness - Google Patents

System for a slide expandes for preventing due to carelessness Download PDF

Info

Publication number
CN205959352U
CN205959352U CN201620912557.7U CN201620912557U CN205959352U CN 205959352 U CN205959352 U CN 205959352U CN 201620912557 U CN201620912557 U CN 201620912557U CN 205959352 U CN205959352 U CN 205959352U
Authority
CN
China
Prior art keywords
sensor
signal
hatch
speaker
carelessness
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
CN201620912557.7U
Other languages
Chinese (zh)
Inventor
高秋
胡敏
文青松
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.)
Chengdu Teda Teda Aviation Technology Co Ltd
Original Assignee
Chengdu Teda Teda Aviation 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 Chengdu Teda Teda Aviation Technology Co Ltd filed Critical Chengdu Teda Teda Aviation Technology Co Ltd
Priority to CN201620912557.7U priority Critical patent/CN205959352U/en
Application granted granted Critical
Publication of CN205959352U publication Critical patent/CN205959352U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Emergency Alarm Devices (AREA)

Abstract

The utility model provides a system for a slide expandes for preventing due to carelessness, the hatch door handle sensor that the emergency exit handle then triggered the producing signals is close to including being used for detecting the hand in this system, an emergency exit state sensor for detecting safety plug pin is extracted then triggers the producing signals, a signal processing unit for judging egress door handle sensor or emergency exit state sensor are triggered then sends alarm signal, a power for receiving speaker that alarm signal then sent the warning provides the electric energy with being used for for the system, hatch door handle sensor, emergency exit state sensor, speaker and power all are connected with signal processing unit. On the aircraft of this system of installing, under non - emergency, when the safety plug pin of emergency hatch is extracted or have the hand to be close to the emergency exit handle of ampere capsule, can in time send out the police dispatch newspaper, play warning effect.

Description

The system launched for slide caused by carelessness for the prevention
Technical field
This utility model is related to warning system field, especially relate to a kind of prevention slide of leading to of anthropic factor and misplace be System.
Background technology
Aircraft emergency hatch is to withdraw use for passenger ground escape on machine in the case of accident, only in case of emergency Just should open.Almost the safety door of every kind of airline carriers of passengers is equipped with corresponding slide assembly, once this door is unlocked, accordingly Slide system will discharge.And must repack after slide release and be installed in place, aircraft is just calculated and is in seaworthiness shape State.And the group bag after slide release is not that Mei Jia airline can complete it is necessary to deliver to the aircraft repairing qualification Parts for maintenance mechanism, this has not only delayed the quality time of other passengers, and airline more to be allowed pays tens thousand of units or even tens of Ten thousand yuan of sky high cost.Moreover, on indivedual types, the safety door of such " Jin Gui " can be opened in hundred meters of low latitudes, such as flies During landing stage of relative risk dash forward and opened, the pneumatic integrity of aircraft will be had a strong impact on, interference rudder face manipulates, or even leads Electromotor Foreign body aspiration is caused to lose power.Nowadays increasing passenger selects to go by air to go on a journey, but " safety door " thing taking place frequently Part, Que Ling airline and civil aviaton insider are anxious and fearful.On November 13rd, 1, CA4307 (Chengdu fly to Guangzhou) When arriving at Guangzhou Bai Yun International airport, the emergent slide of front door is released, and causes delayed flight and heavy economic lossess.
At present, aircraft emergency hatch all controls the opening and closing of hatch door using the pattern of handle behind the door and safety pin, and it is simultaneously Can not effectively prevent passenger, ground staff, crew because various factors (lack of knowledge, time pressure, attention lax, Fatigue etc.) mistakenly open emergency hatch, and then inflation staircase is put down, thus causing the thing that aircraft can not normally take off Therefore.All the time, the accident launched due to neglecting the slide that leads to emerges in an endless stream, seriously Flights Delayed cause a large amount of economy Loss, each airline does not also find the solution of problems at present.
Utility model content
This utility model is based on emergency hatch control mode of today, by installing additional thereon for prevention caused by carelessness The system launched of slide, reach to warn and under non-fortuitous event, attempt to open the purpose of emergency hatch.
Utility model purpose of the present utility model is achieved through the following technical solutions:
The slide that a kind of prevention anthropic factor leads to misplaces system, and this system is included for handss has been detected near safety door Handle then triggers and produces the hatch door grip sensor of signal, is pulled out, for safety pin is detected, the peace that then triggering produces signal Air cock state sensor, it is used for judging that hatch door grip sensor or safe door condition sensor are triggered, send alarm signal Signal processing unit, then send the speaker of warning and for providing a system to the electricity of electric energy for receiving alarm signal Source, described hatch door grip sensor, safe door condition sensor, speaker and power supply are all connected with signal processing unit.
As further technical scheme, described hatch door grip sensor is capacitance sensor or infrared heat sensor.
As further technical scheme, described safe door condition sensor is the reed switch of electro permanent magnetic, when safety is inserted When pin is in normal position, this switch connection does not produce signal;When safety pin is pulled out, this switches off generation signal.
As further technical scheme, described speaker is made up of exciter panel and excitation frame, and this speaker is installed on , there is sound into cabin by the vibration of speaker and safety door in emergency hatch surface.
As further technical scheme, described power supply is battery, and this battery and signal processing unit are arranged on same shell In vivo.
As further technical scheme, described housing is provided with the dual-colored LED display lamp being connected with signal processing unit, This dual-colored LED display lamp is when battery electric quantity is higher than 40% and hatch door grip sensor and the equal fault-free of safe door condition sensor Shown in green, it is less than 40% in battery electric quantity or hatch door grip sensor breaks down or event in safe door condition sensor Shown in red during barrier.
As further technical scheme, between described battery and signal processor, it is serially connected with electric fuse and wave filter.
As further technical scheme, described hatch door grip sensor is arranged at the inner side of emergency hatch trim panel.
Compared with prior art, this utility model has advantages below:
1st, on the aircraft being provided with the system, under nonemergency, be pulled out when the safety pin of emergency hatch or There are handss near when pacifying the safety door handle of sea cabin, alarm can be sent in time, play alarming effect.
2nd, this system adopts dual sensor, has both monitored safety door handle, also monitoring safety pin so that safe class very High.
3rd, this system is independently-powered, independently installed, independent maintenance, independent control system, and operating temperature is -15 DEG C -+55 DEG C, all flight environment of vehicle that can meet aircraft require.
4th, this system weight is light, small volume, and often fan safety door all can install this system, therefore each safe door alarm Whether non-interference, it is easy to crew and case of emergency is processed.
5th, the electromagnetic interference that the shell energy screened circuit plate of signal processing unit produces, and battery possesses short circuit and automatically disconnects Function, improves the safety of system, stability, reliability.
Brief description
Fig. 1 is electrical block diagram of the present utility model;
Fig. 2 is system block diagram of the present utility model;
Fig. 3 is the structural representation of control module;
Fig. 4 is DC-DC circuit figure;
Fig. 5 is the circuit diagram of signal processing unit;
Fig. 6 is sensor signal receiving circuit figure;
Fig. 7 is loudspeaker driving circuit figure;
Fig. 8 is interface circuit figure.
Specific embodiment
With specific embodiment, this utility model is described in detail below in conjunction with the accompanying drawings.
Embodiment
This utility model system is based primarily upon emergency hatch control mode of today, by install additional thereon for prevention by The system that slide caused by carelessness launches, reaches and warns the purpose attempting to open emergency hatch under non-fortuitous event.
This utility model system principle is:Hatch door handle sensing when handss are near safety door handle, near handle Device (sensors of capacitance sensor or infrared heat sensor or other similar functions) produces signal and is delivered to signal processing Unit;When safety pin is pulled out, safe door condition sensor produces signal and is delivered to signal processing unit.Signal processing Unit detect any of the above-described sensor be triggered after produced signal value, and calculate this signal value, if this signal value is with advance Storage or the signal value setting are consistent, then judge that this sensor is triggered, output signal drive the speaker simultaneously, and speaker shakes Move and give a warning sound thus reminding crew.
The structure of the system is as shown in figure 1, mainly include then triggering generation for handss has been detected near safety door handle The hatch door grip sensor of signal, it is pulled out, for safety pin is detected, the safe door state sensing that then triggering produces signal Device, for judging that hatch door grip sensor or safe door condition sensor are triggered, send the signal processing list of alarm signal Unit, for receive alarm signal then send warning speaker and for provide a system to the power supply of electric energy, DC-DC circuit, Dual-colored LED display lamp.
Wherein, as shown in Figure 2 and Figure 3, power supply adopts battery, this battery and signal processing unit (being arranged on circuit board) It is arranged in same housing and collectively constitute control module.I.e. controller module is made up of housing, battery, circuit board.Speaker by Exciter panel and excitation frame composition.Control module pass through cable respectively with hatch door grip sensor, safe door condition sensor and Speaker connects.This controller module can accept hatch door grip sensor and the signal of safe door condition sensor transmission, and will It passes to speaker, to send alarm thus reminding crew member after integrating.
Housing can accommodate battery and circuit board, simultaneously the conspicuous position on housing, installs double-colored LED light.When When battery electric quantity is higher than 40% and all the sensors (hatch door grip sensor and safe door condition sensor) fault-free, LED For green.When battery electric quantity, less than 40% or hatch door grip sensor breaks down or safe door condition sensor breaks down When, LED is redness.
Battery specifications are 2.8V-2.85Ah, the short-circuit protection with electric fuse, at least 16 months life-span.
The core cell of signal processor is the single-chip microcomputer of low-power consumption, and the advantage of single-chip microcomputer is signal transmission time is millisecond Level, non-stop run in 24 hours, energy consumption is ultralow;Therefore the time that sensor is triggered between speaker vibrations sounding is less than 0.5 Second, in machine, staff can prevent in time after hearing chimes of doom and attempt to open emergency hatch due under non-fortuitous event Behavior, thus avoid flight delay and economic loss.
Hatch door grip sensor adopts capacitance sensor or infrared heat sensor, is installed on the interior of emergency hatch trim panel Side.When handss are near safety door handle, hatch door grip sensor produces signal and is transferred to control module.
Safe door condition sensor is the reed switch of electro permanent magnetic, and it is arranged at the safety pin of safety door.Work as safety When latch is in normal position, this switch connection, safe door condition sensor does not produce signal;When safety pin is pulled out, This switches off, and safe door condition sensor produces signal and passes to control module.
Exciter panel and exciter frame constitute the speaker reported to the police, and this speaker is installed on emergency hatch surface, utilize There is sound with the vibration of safety door into cabin in speaker.
Fig. 4~Fig. 8 is particular circuit configurations figure, and wherein Fig. 4 is DC-DC circuit, and the system accesses pcb board by set of cells Upper socket J2, electric energy enters DC-DC chip U4 after electric fuse F2 and wave filter F1, and U4 stably exports 3.3V voltage and provides To system unit.Q1 is battery reverse connecting protection device.
Fig. 5 is signal processing unit, and core adopts single-chip microcomputer as central processing unit, embeds and can write logic control Software.The major responsibility of signal processing unit is that the state monitoring two external sensors is sent out deciding whether drive the speaker Sound, and point out plant maintenance personnel by controlling indicator light colors after monitoring battery capacity.
Fig. 6 is the circuit for connecting two sensors, by the signal transmission of two sensors to signal processing unit.
Fig. 7 is loudspeaker driving circuit, the alarm signal being sent according to signal processing unit, and drive the speaker is reported to the police.
Following protection can be accomplished by the system:Reduce the inconvenience bothered and bring to passenger;Improve aircraft Security performance;Save the huge maintenance cost caused by slide surprisingly launches;Effectively lift the reliability of flight dispatching.
The foregoing is only preferred embodiment of the present utility model, not in order to limit this utility model it should refer to Go out, all any modification, equivalent and improvement made within spirit of the present utility model and principle etc., all should comprise Within protection domain of the present utility model.

Claims (8)

1. the system that a kind of slide for prevention caused by carelessness launches is it is characterised in that this system is included for detecting There are handss then to trigger near safety door handle produce the hatch door grip sensor of signal, be used for safety pin is detected and be pulled out, touch Send out and produce the safe door condition sensor of signal, be used for judging that hatch door grip sensor or safe door condition sensor are triggered Then send the signal processing unit of alarm signal, then send the speaker of warning and for system for receiving alarm signal There is provided electric energy power supply, described hatch door grip sensor, safe door condition sensor, speaker and power supply all with signal processing list Unit connects.
2. a kind of system of slide expansion for prevention caused by carelessness according to claim 1 is it is characterised in that institute Stating hatch door grip sensor is capacitance sensor or infrared heat sensor.
3. a kind of system of slide expansion for prevention caused by carelessness according to claim 1 is it is characterised in that institute State the reed switch that safe door condition sensor is electro permanent magnetic, when safety pin is in normal position, this switch connection does not produce Raw signal;When safety pin is pulled out, this switches off generation signal.
4. a kind of system of slide expansion for prevention caused by carelessness according to claim 1 is it is characterised in that institute State speaker to be made up of exciter panel and excitation frame, this speaker is installed on emergency hatch surface, by speaker and safety door Vibration there is sound into cabin.
5. a kind of system of slide expansion for prevention caused by carelessness according to claim 1 is it is characterised in that institute Stating power supply is battery, and this battery and signal processing unit are arranged in same housing.
6. a kind of system of slide expansion for prevention caused by carelessness according to claim 5 is it is characterised in that institute State housing and be provided with the dual-colored LED display lamp being connected with signal processing unit, this dual-colored LED display lamp in battery electric quantity is higher than 40% and shown in green when hatch door grip sensor and the equal fault-free of safe door condition sensor, it is less than 40% in battery electric quantity Or hatch door grip sensor breaks down or shown in red when safe door condition sensor breaks down.
7. a kind of system of slide expansion for prevention caused by carelessness according to claim 5 is it is characterised in that institute State and between battery and signal processor, be serially connected with electric fuse and wave filter.
8. a kind of system of slide expansion for prevention caused by carelessness according to claim 1 is it is characterised in that institute The hatch door grip sensor stated is arranged at the inner side of emergency hatch trim panel.
CN201620912557.7U 2016-08-19 2016-08-19 System for a slide expandes for preventing due to carelessness Expired - Fee Related CN205959352U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620912557.7U CN205959352U (en) 2016-08-19 2016-08-19 System for a slide expandes for preventing due to carelessness

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620912557.7U CN205959352U (en) 2016-08-19 2016-08-19 System for a slide expandes for preventing due to carelessness

Publications (1)

Publication Number Publication Date
CN205959352U true CN205959352U (en) 2017-02-15

Family

ID=57977915

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620912557.7U Expired - Fee Related CN205959352U (en) 2016-08-19 2016-08-19 System for a slide expandes for preventing due to carelessness

Country Status (1)

Country Link
CN (1) CN205959352U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106205032A (en) * 2016-08-19 2016-12-07 成都成发泰达航空科技有限公司 A kind of slide preventing anthropic factor to cause misplaces system
CN115092404A (en) * 2022-06-29 2022-09-23 广州飞机维修工程有限公司 Aircraft safety pin case with alarm function

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106205032A (en) * 2016-08-19 2016-12-07 成都成发泰达航空科技有限公司 A kind of slide preventing anthropic factor to cause misplaces system
CN115092404A (en) * 2022-06-29 2022-09-23 广州飞机维修工程有限公司 Aircraft safety pin case with alarm function

Similar Documents

Publication Publication Date Title
US11685290B2 (en) Construction and operation of electric or hybrid aircraft
JP4932725B2 (en) Aircraft with cabin differential pressure warning system
US9386638B2 (en) Autonomous emergency light unit for an aircraft and emergency lighting system comprising such light unit
CN103693202B (en) A kind of recovery system of helicopter
CN205959352U (en) System for a slide expandes for preventing due to carelessness
EP2878530B1 (en) Warning circuitry and warning device for an aircraft
CN105346395B (en) A kind of electric automobile power-off system and the electric automobile with power-off system
CN206355470U (en) The automatic fire extinguisher of battery case
CN106205032A (en) A kind of slide preventing anthropic factor to cause misplaces system
CN200977865Y (en) Tyre exploding monitor
CA2622647C (en) Improvements in aircraft doors
CN109794016A (en) A kind of electric bus battery intelligent monitoring fire extinguishing system
CN103448655A (en) System for automatically opening automobile skylight under wading condition and control method thereof
CN204348016U (en) A kind of train pyrotechnics warning device
CN104290733B (en) A kind of escape method for vehicle fire and the vehicle using this method
CN206367453U (en) Car electrically activates formula disaster escape system
CN205527135U (en) Elevator rocks fault detection and alarm system
CN206346111U (en) A kind of bridge inspection car electric control system
CN109606715A (en) A kind of voice warning system and its implementation for aircraft
CN202897710U (en) Alarm system for abnormal opening of elevator landing door
CN109301924B (en) Air-drop signal activation system based on single battery and working method thereof
CN206372406U (en) A kind of automobile-used automatic glass blasting system
CN210626581U (en) Aircraft cabin door latch testing arrangement
CN214422039U (en) Elevator power failure emergency rescue device
CN213768939U (en) Rescue airship

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170215

Termination date: 20180819