CN114202897A - Helicopter warning confirmation system - Google Patents
Helicopter warning confirmation system Download PDFInfo
- Publication number
- CN114202897A CN114202897A CN202111382458.4A CN202111382458A CN114202897A CN 114202897 A CN114202897 A CN 114202897A CN 202111382458 A CN202111382458 A CN 202111382458A CN 114202897 A CN114202897 A CN 114202897A
- Authority
- CN
- China
- Prior art keywords
- alarm
- warning
- information
- display
- level
- 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.)
- Pending
Links
- 238000012790 confirmation Methods 0.000 title claims abstract description 53
- 238000001514 detection method Methods 0.000 claims description 8
- 238000000034 method Methods 0.000 abstract description 16
- 230000000007 visual effect Effects 0.000 description 7
- 230000000638 stimulation Effects 0.000 description 5
- 230000008859 change Effects 0.000 description 3
- 230000002159 abnormal effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 210000004247 hand Anatomy 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000004132 cross linking Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000036541 health Effects 0.000 description 1
- 238000005286 illumination Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001953 sensory effect Effects 0.000 description 1
- 210000003813 thumb Anatomy 0.000 description 1
- 238000010200 validation analysis Methods 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B21/00—Alarms responsive to a single specified undesired or abnormal condition and not otherwise provided for
- G08B21/18—Status alarms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
- B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B7/00—Signalling systems according to more than one of groups G08B3/00 - G08B6/00; Personal calling systems according to more than one of groups G08B3/00 - G08B6/00
- G08B7/06—Signalling systems according to more than one of groups G08B3/00 - G08B6/00; Personal calling systems according to more than one of groups G08B3/00 - G08B6/00 using electric transmission, e.g. involving audible and visible signalling through the use of sound and light sources
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Alarm Systems (AREA)
Abstract
The invention provides a helicopter warning confirmation system, which comprises: the alarm confirmation button, the alarm display component and the alarm sound component are arranged on the base; the alert display assembly includes: a main warning light, a main attention light and a display; the alarm confirmation button is arranged on a helicopter steering column; the alarm confirmation button is connected with the main warning lamp, the main attention lamp, the display and the alarm sound component and is used for executing at least one of the following actions when being pressed by the driver: and extinguishing the main warning lamp, extinguishing the main attention lamp, turning on or off the alarm information displayed on the display, and stopping the alarm sound component from broadcasting the alarm information. The helicopter alarm confirmation method which is more convenient to operate and complete in function is provided.
Description
Technical Field
The invention belongs to the technical field of aviation, and particularly relates to a helicopter warning confirmation system.
Background
The helicopter alarm provides abnormal working indication and necessary state information of each system of the helicopter to the set in a certain mode so as to support the decision of the set. The alarm confirmation is that the alarm indication is interrupted by the operation of the pilot, and represents the visual or auditory interference caused by the fact that the alarm information is known and the indication signal is ended.
Analyzing the design of the conventional helicopter for warning confirmation, wherein the warning confirmation is realized by pressing a main warning lamp and a main attention lamp on an instrument panel by a pilot to respectively confirm warning level and attention level warning information, and the effect of the confirmation operation is that the main warning lamp and the main attention lamp are turned off.
However, the alarm confirmation method has the following defects: firstly, when the pilot performs the alarm confirming operation, the pilot needs to stop operating the steering column, the body tilts forwards at the same time, and the pilot moves the hand above the instrument board to press the main warning lamp or the main attention lamp, so that the pilot is not convenient to operate and the flight safety is influenced; secondly, only the warning level and the attention level alarm can be confirmed, but the prompt level alarm cannot be confirmed; thirdly, only the main alarm is stopped from flashing when the warning level alarm and the attention level alarm are confirmed, and the auditory stimulation and the visual stimulation on the display cannot be stopped.
Disclosure of Invention
The invention provides a helicopter warning confirmation system, and provides a helicopter warning confirmation method which is more convenient to operate and complete in function.
The invention provides a helicopter warning confirmation system, which comprises: the alarm confirmation button, the alarm display component and the alarm sound component are arranged on the base; the alert display assembly includes: a main warning light, a main attention light and a display;
the alarm confirmation button is arranged on a helicopter steering column;
the alarm confirmation button is connected with the main warning lamp, the main attention lamp, the display and the alarm sound component and is used for executing at least one of the following actions when being pressed by the driver:
and extinguishing the main warning lamp, extinguishing the main attention lamp, turning on or off the alarm information displayed on the display, and stopping the alarm sound component from broadcasting the alarm information.
Optionally, the system further includes: the alarm control box and alarm signal sensors of various subsystems of the helicopter; the alert display assembly further comprises: fault signal lamps of various subsystems of the helicopter;
the alarm control box is respectively connected with an alarm signal sensor, a main alarm lamp, a main attention lamp, fault signal lamps of all subsystems of the helicopter, a display and an alarm sound component;
and the alarm control box is used for controlling the alarm display component to display and the alarm sound component to broadcast according to the detection information of the alarm signal sensor of each subsystem of the helicopter.
Optionally, the warning control box is specifically configured to, when it is determined that warning level warning information exists according to detection information provided by warning signal sensors of various subsystems of the helicopter, control the warning sound assembly to broadcast the warning level warning information, control the display to highlight a fault information character corresponding to the warning level warning information, light a fault signal lamp corresponding to the warning level warning information, and flash the main warning lamp.
Optionally, the warning confirmation button is specifically configured to, when warning level warning information is present, and when pressed by the driver,
and extinguishing the main warning lamp, dimming the warning level warning information displayed on the display, and stopping the warning sound component to broadcast the warning level warning information.
Optionally, the warning control box is further configured to, when it is determined that attention level warning information exists according to detection information provided by warning signal sensors of subsystems of the helicopter, control the warning sound assembly to broadcast the attention level warning information, control the display to highlight a fault information character corresponding to the attention level warning information, light a fault signal lamp corresponding to the attention level warning information, and flash the main attention lamp.
Optionally, the warning confirmation button is specifically configured to, when the attention level warning information is present, and when pressed by the driver,
and extinguishing the main attention lamp, dimming the attention level warning information displayed on the display, and stopping the warning sound component to broadcast the attention level warning information.
Optionally, the alarm control box is further configured to, when it is determined that there is prompt level alarm information according to detection information provided by alarm signal sensors of subsystems of the helicopter, control the alarm sound assembly to broadcast the prompt level alarm information, control the display to highlight fault information characters corresponding to the prompt level alarm information, and light fault signal lamps corresponding to the prompt level alarm information.
Optionally, the warning confirmation button is specifically configured to, when there is prompt level warning information and when pressed by the driver,
and (4) broadcasting the prompt level alarm information from bright to dark and stopping the alarm sound component from broadcasting the prompt level alarm information displayed on the display.
The invention provides a helicopter warning confirmation system, which comprises: the alarm confirmation button, the alarm display component and the alarm sound component are arranged on the base; the alert display assembly includes: a main warning light, a main attention light and a display; the alarm confirmation button is arranged on a helicopter steering column; the alarm confirmation button is connected with the main warning lamp, the main attention lamp, the display and the alarm sound component and is used for executing at least one of the following actions when being pressed by the driver: and extinguishing the main warning lamp, extinguishing the main attention lamp, turning on or off the alarm information displayed on the display, and stopping the alarm sound component from broadcasting the alarm information. Through will report an emergency and ask for help or increased vigilance the acknowledgement button and arrange on the steering column, the pilot need not to stop the manipulation to the steering column when reporting an emergency and asking for help or increased vigilance the operation, and has avoided the health to lean forward and move the hand to the instrument board top and press main warning light, has not only ensured the pilot hand not from the manipulation driving of pole, has improved flight safety, and the operation is more convenient moreover. And, press the warning confirmation button on the steering column and can suspend the report of the sounding subassembly of warning, the character font color and ground color of information in the warning window of the display will be darkened at the same time, the main warning light/main attention light will be extinguished, compare with the method of pressing the main warning light in the past, can avoid the unnecessary auditory interference, and has changed the highlighted display state of the character in the display, thus has lightened the vision stimulus to the interference of the pilot effectively.
Drawings
FIG. 1 is a diagram of an alarm validation and alarm system logic cross-over;
fig. 2 is a schematic view of an installation position of an alarm confirm button.
Detailed Description
The helicopter warning confirmation system provided by the invention is explained below with reference to the accompanying drawings.
Referring to fig. 1-2, the present invention realizes the alarm confirmation by a method of setting an alarm confirmation function on a steering column. According to the method, the warning confirmation button is additionally arranged on the steering column, so that a pilot can press the warning confirmation button under the condition that hands are not separated from the steering column, and the confirmation of all warning information of a warning level, a caution level and a prompt level is realized. The warning confirmation button is disposed at the top of the handle of the steering column near the side of the driver and is off-center so that the driver can easily touch and press the thumb when holding the steering column. On one hand, the method ensures that the pilot operates without taking hands off the lever, improves the flight safety and is more convenient and faster to operate; on the other hand, the confirmation of the prompt level alarm information is supplemented, and the alarm confirmation function is more complete; in addition, the confirmation effect of the auditory alarm and the character visual alarm displayed on the display is supplemented, and the interference of unnecessary auditory and visual stimulation to the pilot is effectively avoided.
The helicopter warning system provided by the invention comprises: the alarm system comprises an alarm confirmation button, an alarm display component (comprising a main alarm lamp, a main attention lamp, each fault signal lamp and a display), an alarm sound component, an alarm control box, each system alarm signal sensor component and the like.
The working process of the helicopter warning system comprises the following steps: when some systems of the helicopter enter an abnormal working state or change in state which needs to be known by a pilot when the helicopter is on the ground or in flight, an alarm signal sensor of the system transmits a signal to an alarm control box, and then the alarm control box transmits a corresponding display instruction to an alarm display component and an alarm sound component, so that the display and broadcast of the alarm of each system of the whole helicopter are realized.
When the pilot is informed of the warning information, the visual and auditory sensory stimuli of the warning can be suspended by pressing a warning confirmation button on the steering column.
The alarm control box realizes the illumination of the alarm lamp through the ground/on signal, and the alarm confirmation button also realizes the extinguishment of the alarm lamp through the ground/on signal.
The logical cross-linking of the alarm confirmation and alarm system is shown in FIG. 1.
For example, the installation position of the alarm confirm button is shown in fig. 2.
Illustratively, when a certain fault occurs: firstly, a warning sound component reports fault information, secondly, fault information characters appear in a warning window of a display and are highlighted in color, thirdly, a corresponding fault signal lamp is lighted up, and fourthly, if the fault is at a warning level, a main warning lamp flickers simultaneously; if the fault is in the attention level, the main attention lamp flashes at the same time.
After the pilot knows the warning information, the warning can be confirmed by pressing a warning confirmation button on the steering column. At this time, for the warning level warning information: the method comprises the following steps of firstly, stopping broadcasting fault information by an alarm sound component, secondly, dimming the font color and the bottom color of information characters in an alarm window of a display, and thirdly, turning off a main alarm lamp. For attention level alarm information: the method comprises the following steps of firstly, stopping broadcasting fault information by an alarm sound component, secondly, dimming the font color and the bottom color of information characters in a display alarm window, and thirdly, turning off a main attention lamp. For prompt level alarm information: firstly, the warning sound component stops broadcasting fault information, and secondly, the font color and the bottom color of the information characters in the warning window of the display become dark.
The helicopter alarm confirmation system provided by the invention comprises:
1. compared with the traditional method for pressing the main warning lamp, the method for confirming the warning can be realized by the button on the steering column, the situation that the pilot leaves the steering column to interrupt the operation driving can be avoided, the pilot does not need to lean forward to press the main warning lamp above the instrument board, the operation is more convenient, the pilot can press the main warning lamp without leaving the steering column while the pilot operates in a flying mode, and the flying safety is improved.
2. When the warning level warning information is confirmed, the warning confirmation button on the driving rod is pressed to stop the broadcasting of the warning sound component, the font color and the ground color of the information characters in the warning window of the display can be darkened, and the main warning lamp can be extinguished. Compared with the traditional method of pressing the main warning lamp, the method can avoid unnecessary auditory interference and change the highlight display state of characters in the display, thereby effectively reducing the interference of visual stimulation to pilots.
3. When the attention level warning information is confirmed, the warning confirmation button on the driving rod is pressed to stop the broadcasting of the warning sound component, meanwhile, the font color and the ground color of the information characters in the warning window of the display can become dark, and the main attention lamp can be turned off. Compared with the traditional method of pressing the main attention lamp, the method can avoid unnecessary auditory interference and change the highlight display state of characters in the display, thereby effectively reducing the interference of visual stimulation to pilots.
4. When the prompt level warning information is confirmed, the warning confirmation button on the steering column is pressed to stop the broadcasting of the warning sound component, and the font color and the ground color of the information characters in the warning window of the display become dark. Compared with the design that prompt level alarm information cannot be confirmed in the past, the alarm confirming function is more complete.
Claims (8)
1. A helicopter warning confirmation system, comprising: the alarm confirmation button, the alarm display component and the alarm sound component are arranged on the base; the alert display assembly includes: a main warning light, a main attention light and a display;
the alarm confirmation button is arranged on a helicopter steering column;
the alarm confirmation button is connected with the main warning lamp, the main attention lamp, the display and the alarm sound component and is used for executing at least one of the following actions when being pressed by the driver:
and extinguishing the main warning lamp, extinguishing the main attention lamp, turning on or off the alarm information displayed on the display, and stopping the alarm sound component from broadcasting the alarm information.
2. The system of claim 1, further comprising: the alarm control box and alarm signal sensors of various subsystems of the helicopter; the alert display assembly further comprises: fault signal lamps of various subsystems of the helicopter;
the alarm control box is respectively connected with an alarm signal sensor, a main alarm lamp, a main attention lamp, fault signal lamps of all subsystems of the helicopter, a display and an alarm sound component;
and the alarm control box is used for controlling the alarm display component to display and the alarm sound component to broadcast according to the detection information of the alarm signal sensor of each subsystem of the helicopter.
3. The system of claim 2, wherein the alarm control box is specifically configured to, when it is determined that there is alarm-level alarm information according to detection information provided by alarm signal sensors of the subsystems of the helicopter, control the alarm sound assembly to broadcast the alarm-level alarm information, control the display to highlight a fault information character corresponding to the alarm-level alarm information, light a fault signal lamp corresponding to the alarm-level alarm information, and flash the main alarm lamp.
4. The system of claim 3, wherein the alert confirmation button is specifically configured to, when a warning level alert message is present and is pressed by the driver,
and extinguishing the main warning lamp, dimming the warning level warning information displayed on the display, and stopping the warning sound component to broadcast the warning level warning information.
5. The system of claim 2, wherein the alarm control box is further configured to, when it is determined that attention level alarm information exists according to detection information provided by alarm signal sensors of the helicopter subsystems, control the alarm sound assembly to broadcast the attention level alarm information, control the display to highlight a fault information character corresponding to the attention level alarm information, light a fault signal lamp corresponding to the attention level alarm information, and flash a main attention lamp.
6. The system according to claim 5, characterized in that said alarm confirmation button is particularly adapted to, when attention level alarm information is present and pressed by the driver,
and extinguishing the main attention lamp, dimming the attention level warning information displayed on the display, and stopping the warning sound component to broadcast the attention level warning information.
7. The system of claim 2, wherein the alarm control box is further configured to control the alarm speaker assembly to broadcast the alert level alarm information, control the display to highlight a fault information character corresponding to the alert level alarm information, and illuminate a fault signal lamp corresponding to the alert level alarm information when the alert level alarm information is determined to exist based on the detection information provided by the alarm signal sensors of the various subsystems of the helicopter.
8. The system of claim 7, wherein the alert confirmation button is specifically configured to, when a prompt level alert message is present and is pressed by the driver,
and (4) broadcasting the prompt level alarm information from bright to dark and stopping the alarm sound component from broadcasting the prompt level alarm information displayed on the display.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111382458.4A CN114202897A (en) | 2021-11-19 | 2021-11-19 | Helicopter warning confirmation system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111382458.4A CN114202897A (en) | 2021-11-19 | 2021-11-19 | Helicopter warning confirmation system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114202897A true CN114202897A (en) | 2022-03-18 |
Family
ID=80648085
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111382458.4A Pending CN114202897A (en) | 2021-11-19 | 2021-11-19 | Helicopter warning confirmation system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN114202897A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2880672Y (en) * | 2006-01-17 | 2007-03-21 | 上海子锦电子科技有限公司 | Electrical controlling system of liquid sky-writing device |
| CN106507763B (en) * | 2007-11-30 | 2013-04-10 | 成都飞机工业（集团）有限责任公司 | Emission system is fast controlled for demonstrating machine glory bullet |
| JP5679497B1 (en) * | 2014-03-17 | 2015-03-04 | 株式会社ビーエムオージャパン | Hazard lamp parallel operation device |
| CN106742001A (en) * | 2016-11-30 | 2017-05-31 | 中国直升机设计研究所 | A kind of airborne alarm control lamp box and the light alarm method with it |
| CN209814299U (en) * | 2018-11-06 | 2019-12-20 | 中国直升机设计研究所 | Helicopter centralized alarm device |
| CN212149321U (en) * | 2020-04-03 | 2020-12-15 | 北京安达维尔航空设备有限公司 | Alarm control box for terrain sensing and alarm system of helicopter |
-
2021
- 2021-11-19 CN CN202111382458.4A patent/CN114202897A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2880672Y (en) * | 2006-01-17 | 2007-03-21 | 上海子锦电子科技有限公司 | Electrical controlling system of liquid sky-writing device |
| CN106507763B (en) * | 2007-11-30 | 2013-04-10 | 成都飞机工业（集团）有限责任公司 | Emission system is fast controlled for demonstrating machine glory bullet |
| JP5679497B1 (en) * | 2014-03-17 | 2015-03-04 | 株式会社ビーエムオージャパン | Hazard lamp parallel operation device |
| CN106742001A (en) * | 2016-11-30 | 2017-05-31 | 中国直升机设计研究所 | A kind of airborne alarm control lamp box and the light alarm method with it |
| CN209814299U (en) * | 2018-11-06 | 2019-12-20 | 中国直升机设计研究所 | Helicopter centralized alarm device |
| CN212149321U (en) * | 2020-04-03 | 2020-12-15 | 北京安达维尔航空设备有限公司 | Alarm control box for terrain sensing and alarm system of helicopter |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US9862304B2 (en) | Vehicle lighting control system | |
| KR101823937B1 (en) | Apparatus for vehicle safety | |
| DE102015116175B4 (en) | System and method to provide visual feedback in an aircraft | |
| JP2008132814A (en) | Interior air state notifying device | |
| CN114202897A (en) | Helicopter warning confirmation system | |
| KR20180136851A (en) | System and method for displaying driver sleepiness | |
| JP6421290B1 (en) | A display method that evokes characters and figures on a car display panel. | |
| KR102518720B1 (en) | Apparatus for operating turn signal lamp of vehicle and control method thereof | |
| JP2012128512A (en) | Control device | |
| KR20130021579A (en) | Control device for automotive vehicles | |
| JP3203807U (en) | Device for preventing mistakes in pedaling for automobiles | |
| US2598056A (en) | Vehicle light indicator | |
| JP4102477B2 (en) | Vehicle alarm sound notification device | |
| CN113002418A (en) | Automobile and information display method | |
| KR20180080922A (en) | Traffic lights that simultaneously display lights and flashes | |
| JP2013047740A (en) | Vehicle driving operation training device and vehicle | |
| TWM608645U (en) | Controller of warning device | |
| GB2116348A (en) | Hazard indicator for a vehicle | |
| JP2008059127A (en) | Airfield lighting monitoring control system | |
| KR200203637Y1 (en) | Auto yield-light system for automobil | |
| KR20200068237A (en) | System for controlling turn signals | |
| JP5062124B2 (en) | Vehicle display device | |
| KR102309235B1 (en) | A transformable high-mounted stop lamp and a system comprising the same | |
| JP2022063952A (en) | Control device, presentation system, and program | |
| KR200340965Y1 (en) | Support light for text display of car |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20220318 |