Communication system from airport gate to cockpit

• US 8,174,396 B1
• Filed: 04/01/2009
• Issued: 05/08/2012
• Est. Priority Date: 04/01/2009
• Status: Active Grant

• Current Assignee: Twist, Inc. (Aeria, Inc.)
• Original Assignee: Twist, Inc. (Aeria, Inc.)
• Inventors: Schrinner, Scott E., Dillon, James, McIntire, David K.
• Primary Examiner(s): Hunnings, Travis
• Application Number:
  US12/416,731
• Time in Patent Office: 1,133 Days
• Field of Search: 340/584, 285/148.15, 285/320, 285/311, 285/312, 285/358, 285/87, 285/325, 285/409, 141/383, 141/384, 141/382, 292/11, 292/46, 292/97, 292/98, 292/113, 292/132, 292/232
• US Class Current: 340/584
• CPC Class Codes: B64F 1/20 Arrangement of optical beacons
• CPC Class Codes: B64F 1/305 Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
• CPC Class Codes: B64F 1/362 Installations for supplying conditioned air to parked aircraft
• CPC Class Codes: Y10T 292/081 Swinging and hooked end

Abstract

An apparatus for visually communicating to a pilot in the cockpit of a parked aircraft the status of a preconditioned air (PCA) unit associated with the gate has an electrically controlled PCA indicator box positioned so that it is visible to the pilot in the cockpit. The PCA indicator box has a first appearance when the preconditioned air unit is not operating and a second appearance when the preconditioned air unit is operating. A method of assisting aircraft operators to reduce fuel costs and emissions of an aircraft parked at a gate includes mounting to the gate an electrical PCA indicator and electrically coupling it to a preconditioned air unit at the gate.

Claims

1. An apparatus for visually communicating to a pilot in the cockpit of an aircraft parked at an airport gate regarding a status of a preconditioned air unit associated with the gate comprising:

an electrically controlled PCA indicator box positioned at the gate so that the message of the PCA indicator box is visible to the pilot in the cockpit;

the PCA indicator box having a first appearance when the preconditioned air unit is not operating; and

the PCA indicator box having a second appearance when the preconditioned air unit is operating.

2. The apparatus of claim 1 wherein the second PCA indicator box appearance communicates to the pilot that the preconditioned air unit is operating and that the pilot is to turn the aircraft'"'"'s auxiliary power unit off.

3. The apparatus of claim 1 wherein the PCA indicator box is not illuminated when the preconditioned air unit is not operating, and is illuminated when the preconditioned air unit is operating.

4. The apparatus of claim 3 wherein the illuminated condition is a flashing illuminated condition.

5. The apparatus of claim 1 further comprising an illuminator for the PCA indicator box, wherein the illuminator'"'"'s electrical power is controlled by the electrical power flow to the preconditioned air unit.

6. The apparatus of claim 1 further comprising a universal mount comprising a first portion for mounting to the gate adjustably coupled to a second portion mounted to the PCA indicator box.

7. The apparatus of claim 1, the electrically controlled PCA indicator box further comprising:

a face substantially facing the pilot having translucent indicia; and

an electric illuminator positioned behind the face to project light through the translucent indicia towards the pilot.

8. The apparatus of claim 7, the electrically controlled PCA indicator box further comprising:

a sun shade to reduce sunlight on the electric illuminator.

9. The apparatus of claim 7 wherein the indicia spell the phrases “

PCA On” and

“

APU OFF”

.

10. The apparatus of claim 7 wherein the indicia spell the phrase “

PCA On”

.

11. The apparatus of claim 7 wherein the indicia spell the phrase “

APU OFF”

.

12. The apparatus of claim 7 wherein the translucent indicia comprise:

a metal plate with the indicia cut-out; and

a translucent sheet between the metal plate and the illuminator.

13. The apparatus of claim 7 wherein the translucent indicia comprise:

a metal plate with the indicia cut-out;

a transparent sheet between the metal plate and the illuminator; and

at least one prismatic lens between the transparent sheet and the illuminator.

14. A method of assisting aircraft operators to reduce fuel costs and emissions of an aircraft parked at a gate comprising:

mounting to the gate in a position that will be in view from a cockpit of the aircraft an electrical PCA indicator having a first appearance when the electrical PCA indicator is not operating, and a second appearance when the electrical PCA indicator is operating;

electrically coupling the electrical PCA indicator to a preconditioned air unit at the gate so that when the preconditioned air unit is not operating the first appearance is visible, and when it is operating the second appearance is visible.

15. The method of claim 14 further comprising:

not illuminating the PCA indicator box when the preconditioned air unit is not operating; and

,

illuminating the PCA indicator box when the preconditioned air unit is operating.

16. The method of claim 14 further comprising:

controlling electrical power to an illuminator for the PCA indicator box by using the electrical power flow to the preconditioned air unit.

17. The method of claim 14 wherein the second appearance indicates with words or symbols that the preconditioned air unit is on.

18. The method of claim 17, the step of indicating comprising:

spelling the phrase “

PCA On”

.

19. The method of claim 17, the step of indicating comprising:

spelling the phrase “

APU OFF”

.

20. The method of claim 17 wherein the second appearance further indicates with words or symbols that the pilot should turn off the aircraft APU.

21. The method of claim 20 further comprising:

spelling the phrases “

PCA On” and

“

APU OFF”

as a part of the second appearance.