Eletronic Flight Instrument

• US 20090295600A1
• Filed: 06/02/2008
• Published: 12/03/2009
• Est. Priority Date: 06/02/2008
• Status: Abandoned Application

• Current Assignee: David Robert Stubben, Todd Keller Sprague
• Original Assignee: David Robert Stubben, Todd Keller Sprague
• Inventors: Sprague, Todd Keller, Stubben, David Robert
• Application Number:
  US12/131,817
• Publication Number:
  US 20090295600A1
• Time in Patent Office: Days
• US Class Current: 340/945
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G01D 2207/10 Displays which are primarily used in aircraft or display aircraft-specific information
• CPC Class Codes: G01D 7/02 Indicating value of two or more variables simultaneously
• CPC Class Codes: G01P 1/07 Indicating devices, e.g. for remote indication indicating working conditions of vehicles G07C5/00

Abstract

A flight instrument, having an electronic display, is configured to fit within a standard instrument mount and within an array of standard instrument mounts. The instrument has the ability to emulate any standard or other instrument. This instrument can share its installed optional sensors with other instances of itself that do not include the optional sensors by way of network interfaces. The instrument can contain emulation for all standard instruments and have a menu to select which to display.

Claims

1. An electronic flight instrument configured to fit in a standard instrument mount and an array of standard instruments including:

an electronic display;

a processor for controlling the electronic display, a network interface or interfaces for communicating with other instruments or sensors; and

an optional sensor system.

2. The electronic flight instrument of claim 1 wherein the standard instrument mount is for 2.25″

instruments.

3. The electronic flight instrument of claim 1 wherein the standard instrument mount is for 3.125″

instruments.

4. The electronic flight instrument of claim 1 wherein the electronic display is a Liquid Crystal Display.

5. The electronic flight instrument of claim 1 wherein the network interface includes at least one serial interface.

6. The electronic flight instrument of claim 1 wherein the network interface includes at least one Ethernet interface.

7. The electronic flight instrument of claim 1 wherein the Sensor System includes a Global Positioning System sensor.

8. The electronic flight instrument of claim 1 wherein the Sensor System includes a three axis accelerometer.

9. The electronic flight instrument of claim 1 wherein the Sensor System includes a rate gyro on each of the yaw, pitch and roll axes.

10. The electronic flight instrument of claim 1 wherein the Sensor System includes pressure sensors for airspeed and altitude sensing.

11. The electronic flight instrument of claim 1 wherein the Sensor System includes a Magnetometer for heading sensing.

12. An electronic flight instrument configured to fit in a standard instrument mount including:

an electronic display;

a processor for controlling the electronic display;

a sensor system; and

a selection method for selecting the operation of the instrument to allow emulation of any one of the “

basic six”

instruments or other instruments.

13. The electronic flight instrument of claim 12 wherein the standard instrument mount is for 2.25″

instruments.

14. The electronic flight instrument of claim 12 wherein the standard instrument mount is for 3.125″

instruments.

15. The electronic flight instrument of claim 12 wherein the electronic display is a Liquid Crystal Display.

16. The electronic flight instrument of claim 12 wherein the Sensor System includes a Global Positioning System sensor.

17. The electronic flight instrument of claim 12 wherein the Sensor System includes a three axis accelerometer.

18. The electronic flight instrument of claim 12 wherein the Sensor System includes a rate gyro on each of the yaw, pitch and roll axes.

19. The electronic flight instrument of claim 12 wherein the Sensor System includes pressure sensors for airspeed and altitude sensing.

20. The electronic flight instrument of claim 12 wherein the Sensor System includes a Magnetometer for heading sensing.

21. The electronic flight instrument of claim 12 wherein the selection method includes a menu display.

22. The electronic flight instrument of claim 12 wherein the selection method includes operation of user switches to step through the emulated instruments.