Aircraft passenger luggage bin load weight and balance system

Patent metadata

Field	Value
Publication number	US-11047728-B2
Application number	US-201815864036-A
Country	US
Kind code	B2
Filing date	Jan 8, 2018
Priority date	Jan 8, 2018
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

A load weight and balance system has first sensors for providing a first output signal proportional to an available internal volume of an associated passenger luggage storage bin. Second sensors provide a second output signal proportional a weight of any luggage in the associated passenger luggage storage bin. Display devices provide a visual indication whether or not each passenger luggage storage bin is filled to capacity. A main display provides a visual indication of the storage status of all of the passenger luggage storage bins. A processor receives the signals from the first sensors and the second sensors, calculates whether or not each of the passenger luggage storage bins is filled to capacity and whether or not each of the passenger luggage storage bins is within a predetermined weight value, and determines whether or not the weight distribution of the passenger luggage storage bins in the aircraft is balanced.

First claim

What is claimed is:

1. A load weight and balance system for passenger luggage storage bins in an aircraft, comprising:
at least one first sensor coupled to each of the passenger luggage storage bins in the aircraft for providing a first output signal proportional to an available internal volume of an associated passenger luggage storage bin;
at least one second sensor coupled to each of the passenger luggage storage bins in the aircraft for providing a second output signal proportional a weight of any luggage in the associated passenger luggage storage bin;
a display device for each of the passenger luggage storage bins for providing a visual indication whether or not the associated passenger luggage storage bin is filled to capacity;
a main display for providing a visual indication of a storage status of all of the passenger luggage storage bins; and
a processor coupled to receive the first output signals from each of the at least one first sensors and which is configured to:
calculate, based upon the first output signals from the at least one first sensors, whether or not each of the associated passenger luggage storage bins is filled to capacity;
provide an output signal to each of the display devices causing the display device to indicate whether or not the associated passenger luggage storage bin is filled to capacity;
receive the second output signals from each of the at least one second sensors;
calculate, based upon the second output signals from the at least one second sensors, whether or not each of the associated passenger luggage storage bins is within a predetermined weight value;
provide a signal to the main display causing the main display to indicate whether or not each of the passenger luggage storage bins is within the predetermined weight value;
calculate a balance state of the aircraft based on distribution of passenger luggage storage bin weights across the aircraft;
determine a first redistribution of contents of at least some of the passenger luggage storage bins in the aircraft to improve the balance state responsive to the processor determining that the distribution of the passenger luggage storage bin weights is not balanced, and wherein determining the first redistribution includes identifying that moving a first item from a first passenger luggage storage bin to a second passenger luggage storage bin improves the balance state; and
display instructions at the main display, wherein the instructions include an instruction to move the first item from the first passenger luggage storage bin to the second passenger luggage storage bin.

2. The load weight and balance system of claim 1 , wherein each of the at least one second sensor comprises a load sensor and wherein the output signal from each of the at least one second sensor is proportional to a weight of items within the associated passenger luggage storage bin.

3. The load weight and balance system of claim 1 , wherein each of the at least one first sensor comprises a range sensor and wherein the output signal from each of the at least one first sensor is proportional to an amount of empty space available within the associated passenger luggage storage bin.

4. The load weight and balance system of claim 1 , wherein the processor is configured to provide a signal to the main display causing the main display to indicate whether or not each of the passenger luggage storage bins is filled to capacity.

5. The load weight and balance system of claim 1 , wherein the processor is configured to calculate the distribution of all of the passenger luggage storage bin weights.

6. The load weight and balance system of claim 1 , wherein the at least one second sensor comprises a piezoelectric pressure sensor.

7. The load weight and balance system of claim 1 , wherein the instructions include a second instruction to move a second item from a third passenger luggage storage bin to a fourth passenger luggage storage bin.

8. The load weight and balance system of claim 1 , wherein the main display is a crew display.

9. The load weight and balance system of claim 8 , wherein the visual indication of the storage status of all of the passenger luggage storage bins comprises a map identifying each of the passenger luggage storage bins, and wherein each visual representations of the passenger luggage storage bins on the map are shaded based on a corresponding storage status.

10. The load weight and balance system of claim 1 , wherein the main display is a passenger display.

11. A load weight and balance system for passenger luggage storage bins in an aircraft, comprising:
at least one sensor coupled to each of the passenger luggage storage bins in the aircraft for providing an output signal proportional a weight of any luggage in an associated passenger luggage storage bin;
a main display for providing a visual indication of a storage status of all of the passenger luggage storage bins; and
a processor coupled to receive the output signals from each of the at least one sensors and which is configured to:
calculate, based upon the output signals from the at least one sensors, whether or not each of the associated passenger luggage storage bins is within a predetermined weight value;
provide a signal to the main display to cause the main display to indicate whether or not each of the passenger luggage storage bins is within the predetermined weight value;
calculate a balance state of the aircraft based on distribution of passenger luggage storage bin weights across the aircraft;
determine a first redistribution of contents of at least some of the passenger luggage storage bins in the aircraft to improve the balance state responsive to the processor determining that the distribution of the passenger luggage storage bin weights is not balanced, and wherein determining the first redistribution includes identifying that moving a first item from a first passenger luggage storage bin to a second passenger luggage storage bin improves the balance state; and
display instructions at the main display, wherein the instructions include an instruction to move the first item from the first passenger luggage storage bin to the second passenger luggage storage bin.

12. The load weight and balance system of claim 11 , wherein each of the at least one sensor is a load cell.

13. The load weight and balance system of claim 11 , wherein the processor is configured to calculate the distribution of the passenger luggage storage bin weights across the aircraft.

14. The load weight and balance system of claim 13 , wherein the instructions include a second instruction to move a second item from a third passenger luggage storage bin to a fourth passenger luggage storage bin.

15. The load weight and balance system of claim 14 , wherein the main display is a crew display.

16. The load weight and balance system of claim 15 , wherein the first instruction comprises merging the contents of the first passenger luggage storage bin with the contents of the second passenger luggage storage bin or moving a portion of the contents of the first passenger luggage storage bin to the second passenger luggage storage bin, wherein the first passenger luggage storage bin is in a different column, row, or both as the second passenger luggage storage bin.

17. The load weight and balance system of claim 11 , wherein the at least one sensor comprises a piezoelectric pressure sensor.

18. The load weight and balance system of claim 11 , wherein the main display is a passenger display.

19. A method for balancing a load w

Assignees

• Boeing Co

Inventors

• Zajac Michal
• Kajak Pawel

Classifications

• B64D11/003 Primary

  Stowage devices for passengers' personal luggage · CPC title

• B64C17/02

  by gravity or inertia-actuated apparatus · CPC title

• B64D43/00

  Arrangements or adaptations of instruments · CPC title

• G01G19/414

  using electronic computing means only · CPC title

• G01G19/417

  with provision for checking computing part of balance · CPC title