Avionics system having access through hinged display and control panel

• US 5,786,995 A
• Filed: 11/14/1996
• Issued: 07/28/1998
• Est. Priority Date: 11/14/1996
• Status: Expired due to Fees

• Current Assignee: Teledyne Industries Incorporated (Teledyne Technologies Incorporated)
• Original Assignee: Teledyne Industries Incorporated (Teledyne Technologies Incorporated)
• Inventors: Coleman, Larry Wayne
• Primary Examiner(s): Elmore, Reba I.
• Assistant Examiner(s): Lewis, Monica
• Application Number:
  US08/748,767
• Time in Patent Office: 621 Days
• Field of Search: 364/188, 361/681, 340/971, 313/478, 348/144, 434/55
• US Class Current: 700/83
• CPC Class Codes: B64D 11/00 Passenger or crew accommodation; Flight-deck installations not otherwise provided for
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C

Abstract

An avionics unit is configured to be mounted in an aircraft cockpit for recording and displaying aircraft information. Front panel space is conserved on the avionics unit. The avionics unit includes a housing having an interior. At least one connector is located within the housing. The connector is configured to receive at least one removable storage cartridge. The avionics unit also includes an active front panel assembly having at least one display and at least one control. The active front panel assembly is swingably mounted to the housing, permitting the active front panel assembly to be selectively opened, to expose the housing interior for removal of the storage cartridge, and selectively closed, to enclose the storage cartridge within the housing interior.

Claims

1. An avionics unit in which front panel space is conserved, said avionics unit configured to be mounted in an aircraft cockpit for recording and displaying aircraft information, said avionics unit comprising:

a housing, said housing having an interior;

a stacked assembly of at least two circuit cards located within said housing;

at least one receptacle mounted on at least one of said two circuit cards, said at least one receptacle configured to receive at least one removable storage cartridge;

an active front panel assembly having an inward facing side and an outward facing side, said active front panel assembly including at least one display and at least one control used to set a mode of said avionics unit on said outward facing side, said active front panel assembly swingably mounted to said housing, wherein said active front panel assembly is configured to be selectively opened, thereby exposing said housing interior for removal of said at least one removable storage cartridge, said active front panel assembly configured to be selectively closed, thereby enclosing said at least one removable storage cartridge within said interior; and

a circuit board mounted on the inward facing side of said active panel, wherein said control is connected to said circuit board.

2. An avionics unit as defined in claim 1, wherein said front panel assembly includes at least one fastener having a buckle shaped grip, said at least one fastener configured to releasably secure said front panel assembly in a closed position.

3. An avionics unit as defined in claim 1, wherein said at least one fastener can be latched without the use of tools and said front panel assembly is coupled to said housing by at least one hinge having a portion disposed in a slot defined by said front panel.

4. An avionics unit as defined in claim 1, further comprising at least one mounting fastener, said at least one mounting fastener configured to mount said avionics unit to at least one cockpit rail.

5. An avionics unit as defined in claim 1, wherein said at least one removable storage cartridge is a PCMCIA cartridge.

6. An avionics unit as defined in claim 1, wherein said at least one display is a dot matrix LED display having at least one 5×

7 LED array.

7. An avionics unit as defined in claim 1, further comprising at least one optical filter, said at least one optical filter disposed over at least a portion of said at least one display to enhance display contrast.

8. An avionics unit as defined in claim 7, wherein said at least one optical filter includes electromagnetic shielding.

9. An avionics unit as defined in claim 1, further comprising an EMI gasket disposed on said inward side of said front access door so that said EMI gasket is in contact with said housing when said active front panel assembly is in the closed position.

10. A housing for an electronic system, said housing comprising:

an enclosure having an interior;

at least one circuit board mounted in said housing, said circuit board supported by at least one stand-off;

at least one receptacle located within said enclosure, said at least one receptacle connected to said at least one circuit board and configured to receive at least one removable electronic module; and

an active panel, including at least one operator-accessible switch used to set an operating mode of said electronic system, said active panel movably mounted to said housing, wherein said active panel is configured to be selectively opened, thereby exposing said interior for removal of said at least one removable electronic module, and wherein said active panel is configured to be selectively closed, thereby covering said enclosure interior and said at least one electronic module, said operator-accessible switch being accessible when said active panel is closed.

11. A housing as defined in claim 10, wherein said removable electronic module is a data storage cartridge.

12. An housing as defined in claim 11, wherein said electronic module is a PCMCIA device.

13. A housing as defined in claim 10, wherein said active panel includes at least one display.

14. A housing as defined in claim 13, wherein said display is an LED display including at least one array having at least 35 pixels capable of displaying at least a portion of the ASCII character set.

15. A housing as defined in claim 13, wherein said display is an CRT used to display status information.

16. A housing as defined in claim 13, wherein said display is an LCD display.

17. A housing as defined in claim 13, further comprising a polarized lens, said lens disposed over said at least one display.

18. A housing as defined in claim 10, wherein said active panel includes at least one vernier switch.

19. An aircraft status monitoring system, said aircraft status monitoring system configured to retain data when power is removed, said aircraft status monitoring system comprising:

a housing having an interior;

a circuit board located in said interior;

at least one socket located within said housing and mounted to said circuit board, said at least one socket configured to receive at least one removable non-volatile memory cartridge;

an access door, said access door movably mounted to said housing, wherein said access door is movable from an open position, thereby exposing said interior for removal of said at least one removable non-volatile memory, to a closed position, wherein said interior and said at least one non-volatile memory cartridge is covered;

an illuminated switch positioned on said access door; and

at least one pixel display, said pixel display attached to said access door.

20. A housing for a first electronic system, said housing comprising:

an enclosure having an interior;

at least one port connector located within said enclosure, said at least one port connector configured to receive at least one removable cable connectable to a second electronic system for retrieving data stored within said first electronic system; and

an active panel having either a display or a switch or both said display and said switch, said active panel movably mounted to said housing, wherein said active panel is configured to be selectively opened, thereby exposing said interior providing access to said port connector for connection to said removable cable, and wherein said active panel is configured to be selectively closed, thereby covering said enclosure interior and said port connector.