Augmented weight sensing for aircraft cargo handling systems

• US 10,589,872 B1
• Filed: 01/29/2019
• Issued: 03/17/2020
• Est. Priority Date: 01/29/2019
• Status: Active Grant

• Current Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Rockwell Collins, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Sundararaj, Laveen Vikram, Patanna, Vikramasimha Reddy
• Primary Examiner(s): Feild, Joseph H
• Assistant Examiner(s): Point, Rufus C
• Application Number:
  US16/261,132
• Time in Patent Office: 413 Days
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: B64D 9/00 Equipment for handling freight; Equipment for facilitating passenger embarkation or the like emergency equipment B64D17/00, B64D19/00, B64D25/00; structures integral with fuselage to facilitate loading, fuselage floors specially adapted for freight, steps mounted on and retractable within aircraft B64C; ground installations B64F
• CPC Class Codes: B64F 1/32 for handling freight
• CPC Class Codes: G01G 19/07 for weighing aircraft
• CPC Class Codes: G01G 19/414 using electronic computing means only
• CPC Class Codes: G01G 19/62 Over or under weighing apparatus
• CPC Class Codes: Y02T 50/80 Energy efficient operational measures, e.g. ground operations or mission management

Abstract

An aircraft cargo handling system with augmented weight sensing capability is disclosed. In embodiments, the aircraft cargo handling system includes a loadmaster control station including a controller with a user interface communicatively coupled to the controller. The user interface is configured to receive user-input weight data for one or more cargo units. The aircraft cargo handling system further includes one or more sensors configured to detect weight data for the cargo units or one or more carriers for the cargo units. The sensors may be coupled to respective transmitters that are configured to transmit the detected weight data to a data gateway device that is communicatively coupled to the controller. The controller is configured to compare the user-input weight data to the detected weight data and generate an alert when the difference between the user-input weight data and the detected weight data is greater than a threshold weight difference.

Claims

1. An aircraft cargo handling system, comprising:

a loadmaster control station including a controller;

a user interface communicatively coupled to the controller and configured to receive user-input weight data for one or more cargo units or one or more carriers for the one or more cargo units;

one or more sensors configured to detect weight data for the one or more cargo units; and

one or more transmitters coupled to the one or more sensors and configured to transmit the detected weight data to a data gateway device communicatively coupled to the controller,

wherein the controller is configured to;

receive the user-input weight data from the user interface;

receive the detected weight data from the data gateway device;

compare the user-input weight data to the detected weight data; and

generate an alert when a difference between the user-input weight data and the detected weight data is greater than a threshold weight difference.

2. The aircraft cargo handling system of claim 1, wherein the one or more sensors include one or more force sensors configured to detect one or more weights associated with the one or more cargo units or the one or more carriers for the one or more cargo units.

3. The aircraft cargo handling system of claim 2, wherein the one or more force sensors are coupled to the one or more cargo units or to the one or more carriers for the one or more cargo units.

4. The aircraft cargo handling system of claim 1, wherein the one or more sensors include one or more torque or throttle sensors configured to detect a change in torque or throttle required to propel an aircraft carrying the one or more cargo units.

5. The aircraft cargo handling system of claim 4, wherein the one or more torque or throttle sensors are coupled to a propulsion system of the aircraft.

6. The aircraft cargo handling system of claim 4, wherein the one or more torque or throttle sensors are coupled to a powertrain of a pushback tractor configured to pull the aircraft.

7. The aircraft cargo handling system of claim 1, wherein the one or more sensors include one or more imaging devices or radio frequency identification (RFID) readers configured to detect one or more identifiers associated with one or more predetermined weights of the one or more cargo units or the one or more carriers for the one or more cargo units.

8. The aircraft cargo handling system of claim 7, wherein the one or more identifiers are coupled to the one or more cargo units or to the one or more carriers for the one or more cargo units.

9. The aircraft cargo handling system of claim 1, wherein the controller is further configured to:

generate a cargo weight verification signal when the difference between the user-input weight data and the detected weight data is less than the threshold weight difference.

10. The aircraft cargo handling system of claim 1, further comprising:

one or more position sensors configured to detect position data for the one or more cargo units or the one or more carriers for the one or more cargo units, wherein the one or more transmitters are coupled to the one or more position sensors and configured to transmit the detected position data to the data gateway device.

11. The aircraft cargo handling system of claim 10, wherein the one or more position sensors are coupled to the one or more cargo units or to the one or more carriers for the one or more cargo units.

12. The aircraft cargo handling system of claim 10, wherein the controller is further configured to:

receive the detected position data from the data gateway device; and

update at least one of the user-input weight data or the detected weight data based on the detected position data for the one or more cargo units or the one or more carriers for the one or more cargo units.

13. A loadmaster control station, comprising:

a controller;

a user interface communicatively coupled to the controller and configured to receive user-input weight data for one or more cargo units or one or more carriers for the one or more cargo units;

a data gateway device communicatively coupled to the controller, the data gateway device configured to receive weight data detected by one or more sensors coupled to the one or more cargo units or to one or more carriers for the one or more cargo units;

wherein the controller is configured to;

receive the user-input weight data from the user interface;

receive the detected weight data from the data gateway device;

compare the user-input weight data to the detected weight data; and

generate an alert when a difference between the user-input weight data and the detected weight data is greater than a threshold weight difference.

14. The loadmaster control station of claim 13, wherein the controller is further configured to:

generate a cargo weight verification signal when the difference between the user-input weight data and the detected weight data is less than the threshold weight difference.

15. The loadmaster control station of claim 13, wherein the data gateway device is further configured to receive position data detected by one or more position sensors coupled to the one or more cargo units or to the one or more carriers for the one or more cargo units.

16. The loadmaster control station of claim 15, wherein the controller is further configured to:

receive the detected position data from the data gateway device; and

update at least one of the user-input weight data or the detected weight data based on the detected position data for the one or more cargo units or the one or more carriers for the one or more cargo units.

17. A method of monitoring aircraft cargo, comprising:

receiving user-input weight data for one or more cargo units via a user interface;

receiving weight data detected by one or more sensors coupled to the one or more cargo units or to one or more carriers for the one or more cargo units;

comparing the user-input weight data to the detected weight data; and

generating an alert when a difference between the user-input weight data and the detected weight data is greater than a threshold weight difference.

18. The method of claim 17, further comprising:

generating a cargo weight verification signal when the difference between the user-input weight data and the detected weight data is less than the threshold weight difference.

19. The method of claim 17, further comprising:

receiving position data detected by one or more position sensors coupled to the one or more cargo units or to the one or more carriers for the one or more cargo units.

20. The method of claim 19, further comprising:

updating at least one of the user-input weight data or the detected weight data based on the detected position data for the one or more cargo units or the one or more carriers for the one or more cargo units.