Flight deck systems in aircraft typically include graphical display systems that integrate numerous elements of flight critical data—including Global Positioning System (GPS) navigation information, traffic information, lightning information, and terrain. The graphical display system displays this data on a screen of a display monitor and allows the pilot to overlay important navigation data such as the active flight plan route, airways, political boundaries, obstacles and special use airspace, over a color-contoured terrain and water base map. Standard flight instrumentation including attitude, heading, airspeed, altitude and vertical speed may also be displayed on the screen.
The graphical display system includes push buttons and adjustable knobs to allow the pilot to select modes or change the data that is displayed on the screen. Different data or screen views (pages) can be selected for display on the screen. The push buttons and knobs are mapped to different functions dependent on the page being displayed.
The push buttons that are active for a particular page being displayed on the screen can be confusing to the pilot. To reduce potential confusion, each push button is seated within a recess and has an illuminable element adjacent to the push button. The illuminable element is separately controllable and is illuminated only if the push button is active for the displayed page, that is, if the push button is mapped to a selectable function for the displayed page. The illuminable element provides a lighting effect around the periphery of the button. This illumination of the active push button has the effect of drawing attention to the applicable push button and improves the ease of operation of the system.
A display system includes a screen and a plurality of push buttons, an illuminable element is adjacent to each push button to provide a lighting effect around the periphery of the button. The screen displays a page of information (screen view) that includes at least one selectable function mapped to one of the push buttons. Light is transmitted through the illuminable element adjacent to the one push button mapped to the one selectable function, to denote that the push button is active for the displayed page.
The illuminable element may be seated in a recess surrounding the push button. The push button may be in the shape of a rectangle having rounded corners. The page of information may include multiple selectable functions mapped to respective ones of the push buttons. The illuminable element of each of the respective ones of the push buttons becomes illuminated during display of the page. For different pages displayed on the display there are respective different selectable functions mapped to different ones of the push buttons. For each different page, during display of that page the illuminable elements of the ones of the push buttons that have selectable functions mapped thereto are illuminated. The illuminable element may be a light pipe or a pair of light emitting diodes.
The foregoing and other objects, features and advantages of the invention will be apparent from the following more particular description of preferred embodiments of the invention, as illustrated in the accompanying drawings in which like reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of the invention.
A description of preferred embodiments of the invention follows.
Each push button 102 includes a recess surrounding the actuator or controller portion of push button 102 in which an illuminable element 104 is seated. In one embodiment, the illuminable element is a light pipe that is adjacent to the push button and surrounds the push button. A light pipe is a solid transparent plastic rod for transmitting light lengthwise. The light can be provided by a Light Emitting Diode (LED). The illumination of each illuminable element 104 is separately controlled. In alternate embodiments, other lighting techniques well known to those skilled in the art can be used for the illuminable element. For example, the illuminable element can include a pair of light emitting diodes positioned adjacent to the push button such that when both diodes are lit, a lighting effect is provided around the periphery of the push button.
The light is only transmitted by the illuminable element 104, if the push button 102 is active for the page displayed on the screen 108, that is, if the push button 102 is mapped to a selectable function for the page displayed on the screen 108.
In the embodiment shown, each of the push buttons 102 is in the shape of an oval or a rectangle having rounded corners. Printed circuit boards used for mounting push buttons and knobs in a display system are well known to those skilled in the art.
The display routine 202 controls the information displayed (displayed pages/screen view) on the screen 108 and the illumination of the illuminable elements 104 adjacent to push buttons 102 to denote active push buttons for the displayed page. The illumination of the illuminable element 104 adjacent to each push button 102 is controlled by the control circuit 216 for the active push buttons 102. An embodiment of the control circuit 216 will be described later in conjunction with
The checklist page is displayed on the screen 108. The checklist page includes a checklist menu 336. A menu is a list of options from which the user can make a selection in order to perform a desired action. The checklist menu 336 is a list of all the normal procedures checklists for each phase of flight. The first item in the checklist menu 336 is highlighted by a rectangular box 338. The checklist page also includes a label (description of the function) indicating the function that is mapped to each active push button 102a-c and 102f-i. The label is displayed at a position on the display screen that is adjacent to the respective push button 102. For example, push buttons 102a and 102b are mapped to functions that move the outlined box 338 up and down over the items in the menu 336.
Label 320 adjacent to push button 102a is an up arrow symbol that indicates that push button 102a is mapped to the function which moves the outlined box 338 to the item directly above the currently selected item in the list/menu 336. Label 322 adjacent to push button 102b is a down arrow symbol that indicates that push button 102b is mapped to the function which moves the outlined box 338 to the item in the menu 336 directly below the currently highlighted item in the menu 336. Label 324 adjacent to push button 102c includes the text “select” that indicates that push button 102c is mapped to the function that selects the currently highlighted item in the menu 336. Respective illuminable elements 104d, 104e adjacent to push buttons 102d, 102e are not illuminated indicating that the push buttons are not active for the current page (screen view) displayed on the screen 108. Also, there is no label displayed at positions on the screen 108 adjacent to non-active push buttons 102d, 102e.
The active push buttons 102f-102i on the left side of the screen 108 allow the pilot to select other checklists to be displayed on the screen 108. A label 326, 328, 330, 332 indicating the respective checklist that is mapped to each push button 102f-102i is displayed at a screen position adjacent to each push button 102. In the embodiment shown, all of the active push buttons remain active with the respective illuminable element 104 adjacent to each active push button to provide a lighting effect around the periphery of the push button while the checklist page is displayed on the screen 108.
Thus, push button action can be dynamically denoted by whether the illuminable element 104 adjacent to the push button 102 is illuminated. This draws attention to the push buttons that are active dependent on the state of the system and/or the page displayed on the screen 108 and thus improves the ease of operation of the system 100. Additional benefit is obtained by reducing clutter and overall ambient brightness in the cockpit of the aircraft by not illuminating the illuminable element adjacent to non-active push buttons 102.
The left knob 334 below the screen 108 controls the page that is displayed on the display screen. The left knob 334 provides access to the map page. In the embodiment shown, only two pages are available, the checklist page and the map page. However, in other embodiments, there may be more than two selectable pages.
As shown, each active push button 102a-102c, 102f-102h and 102j has an associated label 400, 402, 404, 408, 410, 412 and 414 describing the function that is mapped to the push button (actuator). The labels displayed on the screen 108 and the active push buttons are different for each page displayed. As described in conjunction with the checklist page shown in
Referring to the map page shown in
Likewise, the base map function key (push button) 102c corresponds to the “base map” label 404 displayed in the current screen view 108. The base map function key (push button) 102c selects from multiple levels of map detail, starting with contoured terrain and water base map and political boundaries. Pressing (pushing) the button 102c removes contoured terrain, while leaving water and political boundary references. Pressing (pushing) the button 102c again views the flight plan.
Push buttons 102f-102h control overlay and modes of available sensors. The traffic button 102f associated with the displayed label “traffic” 408 cycles through traffic sensor modes displaying intruders. The lightning button 102g associated with label “lightning” 410 cycles through lighting sensor modes. The clear strikes button 102h associated with label “clear strikes” 412 removes lightning symbols to allow for the refresh of lightning data. Push button 102j associated with the label “emergency checklist” 414 allows the emergency checklist to be displayed with one-button access from the map page.
At step 500, the page selected by the left knob 334 (
At step 502, the illuminable element 104 adjacent to each active push button 102 associated with the function labels displayed on the screen 108 is illuminated by the illumination control circuit to provide a lighting effect around the periphery of the push button, indicating that the push button 102 is active for the displayed page.
At step 504, the display routine 202 (
At step 506, the display routine 202 updates the page to be displayed by retrieving information from the database 216 and updating the data to be displayed on the screen 108. The display routine 202 also selects the push buttons 102 to be illuminated based on the active push buttons for the newly selected page. Processing continues with step 500 to display the newly selected page.
The LED controller circuit 600 receives commands from the processor 210 (
The LED group dimming interface 608 allows use of a secondary Pulse Width modulated signal to enhance the resolution of night time dimming. This allows sub one nit luminosity levels. The secondary pulse width modulated signal labeled “dimming control” 614 provides a greater resolution of the dimming range than that provided by the LED controller circuit 600 and LED driver 602. In the LED group dimming circuit, the secondary Pulse Width Modulated signal is applied to a MOSFET gate, whose drain and source are in series with the combined LED_RTN signal allowing software control of the dimming through the processor 210.
The LED drivers 602 and LED controller circuit 600 shown in
The output signal 712 from the LED controller device 704 is coupled to the gate of FET 606 to control whether LEDs 700, 702 are lit dependent on control signals received on the control interface 610 from the processor 210 over. While the FET 606 is ON, the pair of LEDs 700, 702 are lit and the illuminable element 104 is illuminated.
In one embodiment, the LEDs 700, 702 are manufactured by Toyoda Gosei, for example, part number E1S03-AC1A7-02 RANK P. However, any LED with an approximate 20 mA cathode current draw can be used.
The illumination of an illuminable element 104 to provide a lighting effect around the periphery of the push button 102 can also be used to indicate the position of a focus point (cursor) on the display for use in display systems for helicopters. An illuminable element is illuminated dependent on the proximity of the cursor on the display to the illuminable element.
An embodiment of the invention has been described for a display system for use in the cockpit of an aircraft. However, the invention is not limited to aircraft display systems. The invention can be used in any display system having selectable functions mapped to push buttons.
This application claims the benefit of U.S. Provisional Application No. 60/566,781, filed on Apr. 30, 2004. The entire teachings of the above application are incorporated herein by reference.
Number | Date | Country | |
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60566781 | Apr 2004 | US |