Granted Patent B2

US 10,005,562 · App. 14/642,032 · Granted Jun 26, 2018

Inventor: Jeremy Joseph Kneuper (Hesston, KS)

Assignee: Textron Innovations Inc.

B64D43/00G01C23/00G06F3/0488G09G5/14G06F2203/04804G09G2340/10G09G2340/12G09G2380/12

Abstract

Claims (36)

1. An instrument panel system for an aircraft, comprising:

a touch-screen information panel display configured to interface with aircraft systems through a computing system; and

a standby instrument hard mounted in a cockpit of the aircraft, the standby instrument being behind, and facing a backside of a portion of the information panel display;

wherein:

the standby instrument is powered separately from the information panel display and regularly provides updated information;

the standby instrument is at least partially hidden from view when the information panel display is in a powered state;

the standby instrument being viewable when the portion of the information panel display is cleared; and

the standby instrument being viewable through the portion when the information panel display is in an unpowered state.

2. The system of claim 1 , wherein the information panel display is one of transparent and translucent in the unpowered state.

3. The system of claim 1 , wherein the information panel display is an OLED display.

4. The system of claim 1 , wherein the standby instrument comprises a display, and wherein the standby instrument display is configured to illuminate through the information panel display when the information panel display is in the unpowered state.

5. The system of claim 1 , wherein the information panel display is cleared as a result of one of:

i. a loss of electrical power to the information panel display; and

ii. a positive selection to disengage at least a portion of the information panel display.

6. The system of claim 1 , wherein the touch-screen display panel is at least one of a suspended particle display, a LCD display, and a projection display.

7. The system of claim 1 , wherein the portion of the information panel display is one of transparent and translucent when cleared.

8. A method comprising the steps of:

providing a display panel in a vehicle such that in a first state the panel is active, and in a second state, the panel is more transparent than when in the first state;

securing a standby instrument in the vehicle, the standby instrument being hard mounted behind the panel and facing a backside of the panel;

powering the instrument independently from the display panel for continuously providing updated information;

orienting the instrument such that the instrument can be observed through the display panel, and information learned from the instrument, when the panel is in the second state and is more transparent; and

activating the second state by a positive selection made on the panel to clear at least a portion of the display.

9. The method of claim 8 , wherein the vehicle is an aircraft and wherein the panel enables interfacing with at least one mechanical or one electrical system in the aircraft.

10. The method of claim 9 , further comprising the steps of:

locating the panel in an aircraft cockpit; and

causing the panel to laterally extend such that the panel spans a substantial portion of the width of the cockpit.

11. The method of claim 8 , wherein the second state is created by an interruption in the power supply to the display.

12. The method of claim 8 wherein the vehicle is an aircraft, and the standby instrument displays the aircraft's attitude, altitude, and airspeed.

13. An aircraft system comprising:

an interactive display panel constructed of an organic semiconductor which is sandwiched between two electrodes, the display panel having transparency when power is lost; and

a standby instrument providing a first continually updated aircraft reading, the standby instrument being secured in the aircraft cockpit separate from the interactive display panel, the standby instrument having an independent source of electrical power and a first reading being located behind a first portion of the display panel, wherein the standby instrument is oriented such that when power to the display panel is lost or a selection is made to clear a portion of the display panel, the first reading is readable through the display panel.

14. The system of claim 13 , wherein the standby instrument is centrally located behind the display panel.

15. The system of claim 13 , wherein the standby instrument is an instrument from which at least one of the aircraft's attitude, altitude, and airspeed is displayed.

16. The system of claim 13 , wherein the display panel is a touch screen and is arranged through a computer system to interface with a plurality of aircraft systems such that the display panel substantially takes the place of a plurality of controls utilized to interact with said plurality of aircraft systems.

17. The system of claim 13 , wherein the standby instrument provides at least one additional continually updated reading, the at least one additional reading being located behind a second portion of the display panel such that when power to the display panel is lost, the additional reading is readable through the second portion of the display panel.

18. The system of claim 13 , wherein the standby instrument is located behind the display panel substantially to one side of the display panel.

Assignments (3)

Continuity (21)

Cited By (1)

US 1,065,351