Control panel for use in controlling a large area display

• US 9,505,487 B2
• Filed: 03/15/2013
• Issued: 11/29/2016
• Est. Priority Date: 03/15/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Miener, Steven John
• Primary Examiner(s): Watko, Julie Anne
• Application Number:
  US13/839,505
• Publication Number:
  US 20140266979A1
• Time in Patent Office: 1,355 Days
• US Class Current: 1/1
• CPC Class Codes: B64C 13/04 actuated personally
• CPC Class Codes: B64D 31/04 actuated personally
• CPC Class Codes: B64D 43/00 Arrangements or adaptations of instruments arrangements of cameras B64D47/08; aeronautical measuring instruments per se G01C
• CPC Class Codes: G02B 2027/0161 characterised by the relative positioning of the constitutive elements
• CPC Class Codes: G02B 27/01 Head-up displays
• CPC Class Codes: G02B 27/0149 characterised by mechanical features G02B27/0176 takes precedence

Abstract

In one aspect, an aircraft instrumentation system for a cockpit instrument panel of an aircraft is provided. The system includes a first display operable to display at least one of flight mission data or aircraft systems monitoring data, and a second display operable to control a plurality of display options of the first display. The first display and the second display are positioned outside an ejection envelope of the aircraft.

Claims

1. An aircraft instrumentation system for a cockpit instrument panel of an aircraft that includes an ejection seat positioned within a cockpit of the aircraft, said system comprising:

a first display operable to display at least one of flight mission data or aircraft systems monitoring data to a pilot; and

a second display operable to control a plurality of display options of said first display, wherein said first display and said second display are positioned outside an ejection envelope for the ejection seat for the pilot, wherein said second display is within reach of the pilot of the aircraft locked in a torso harness of the ejection seat, and said first display is positioned forward of said second display such that said first display is outside the reach of the pilot locked in the torso harness when the pilot is shorter than a predetermined physical height, wherein both said first display and said second display are touch screen displays, wherein a pilot shorter than said predetermined physical height enters a first set of commands and a second set of commands on the touch screen of only the second display, wherein a pilot taller than said predetermined physical height has the option of entering both said first set of commands and said second set of commands only on the touch screen of the second display while locked in the torso harness, or of entering said first set of commands on the touch screen of said first display and said second set of commands on the touch screen of said second display while locked in the torso harness.

2. The aircraft instrumentation system of claim 1, wherein said second display is positioned such that the pilot can maintain a view ahead of the aircraft while viewing said second display.

3. The aircraft instrumentation system of claim 1, wherein said system further comprises a head up display (HUD), said second display positioned below said HUD and above said first display.

4. The aircraft instrumentation system of claim 1, wherein said ejection envelope is defined at least partially by a forward ejection clearance plane, said second display positioned forward of said forward ejection clearance plane.

5. The aircraft instrumentation system of claim 1, wherein said second display is smaller than said first display.

6. The aircraft instrumentation system of claim 1, wherein the second display provides a portion of the information displayed on the first display.

7. An aircraft comprising:

a cockpit including a cockpit instrument panel;

an ejection seat for a pilot positioned within said cockpit, said ejection seat including an ejection envelope; and

an aircraft instrumentation system coupled to said instrument panel, said aircraft instrumentation system comprising;

a first display operable to display at least one of flight mission data or aircraft systems monitoring data to the pilot; and

a second display operable to control a plurality of display options of said first display, wherein said first display and said second display are positioned outside the ejection envelope, wherein said second display is within reach of the pilot of the aircraft locked in a torso harness of the ejection seat, and said first display is positioned forward of said second display such that said first display is outside the reach of the first pilot locked in the torso harness when the pilot is shorter than a predetermined physical height, wherein both said first display and said second display are touch screen displays, wherein a pilot shorter than said predetermined physical height enters a first set of commands and a second set of commands on the touch screen of only the second display, wherein a pilot taller than said predetermined physical height has the option of entering both said first set of commands and said second set of commands only on the touch screen of the second display while locked in the torso harness, or of entering said first set of commands on the touch screen of said first display and said second set of commands on the touch screen of said second display while locked in the torso harness.

8. The aircraft of claim 7, wherein said second display is positioned such that the pilot can maintain a view ahead of said aircraft while viewing said second display.

9. The aircraft of claim 7, wherein said aircraft instrumentation system further comprises a head up display (HUD), said second display positioned below said HUD and above said first display.

10. The aircraft of claim 7, wherein said ejection envelope is at least partially defined by a forward ejection clearance plane, said second display is positioned forward of said forward ejection clearance plane.

11. The aircraft of claim 7, wherein said second display is smaller than said first display.

12. A method of assembling an aircraft instrumentation system for a cockpit instrument panel of an aircraft that includes an ejection seat positioned within a cockpit of the aircraft, said method comprising:

providing a first display operable to display at least one of flight mission data or aircraft systems monitoring data to a pilot;

providing a second display operable to control a plurality of display options of the first display; and

positioning the first display and the second display outside an ejection envelope for the ejection seat for the pilot, wherein the second display is positioned further aft than the first display such that the second display is within reach of the pilot of the aircraft locked in a torso harness, and such that the first display is outside the reach of the pilot locked in the torso harness when the pilot is shorter than a predetermined physical height, wherein both said first display and said second display are touch screen displays, wherein a pilot shorter than said predetermined physical height enters a first set of commands and a second set of commands on the touch screen of only the second display, wherein a pilot taller than said predetermined physical height has the option of entering both said first set of commands and said second set of commands only on the touch screen of the second display while locked in the torso harness, or of entering said first set of commands on the touch screen of said first display and said second set of commands on the touch screen of said second display while locked in the torso harness.

13. The method of claim 12, further comprising positioning the second display such that the pilot can maintain a view ahead of the aircraft while viewing the second display.

14. The method of claim 12, further comprising providing a heads-up-display (HUD).

15. The method of claim 14, further comprising positioning the second display below the HUD and above the first display.

16. The method of claim 12, further comprising positioning the second display forward of a forward ejection clearance plane of the ejection envelope.

17. The method of claim 12, wherein providing a second display comprises providing a second display smaller than the first display.