SYSTEM AND METHOD FOR DAMAGE TRACKING AND MONITORING DURING GROUND HANDLING OF AIRCRAFT

• US 20160200449A1
• Filed: 01/12/2016
• Published: 07/14/2016
• Est. Priority Date: 01/12/2015
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE), Airbus SAS (Airbus SE)
• Original Assignee: Airbus Operations GmbH (Airbus SE), Airbus SAS (Airbus SE)
• Inventors: FU, Tim, ALONSO-TABARES, Diego
• Granted Patent: US 9,676,493 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: B64D 2045/0085 Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
• CPC Class Codes: B64D 45/00 Aircraft indicators or protectors not otherwise provided for camouflage F41H3/00
• CPC Class Codes: G01S 2013/916 Airport surface monitoring [ASDE]
• CPC Class Codes: G06Q 10/08 Logistics, e.g. warehousing, loading or distribution; Inventory or stock management
• CPC Class Codes: G06Q 40/00 Finance; Insurance; Tax strategies; Processing of corporate or income taxes
• CPC Class Codes: G07C 5/008 communicating information to a remotely located station transmission systems for measured values G08C
• CPC Class Codes: G07C 5/085 using electronic data carriers
• CPC Class Codes: G08G 5/00 Traffic control systems for aircraft , e.g. air-traffic control [ATC]

Abstract

A system for damage tracking and monitoring during ground handling of aircraft includes a ground service communication network configured to transmit communication data between ground support equipment, GSE, and aircraft; a database configured to store configuration data and status data of GSE and aircraft; and a computer-based system configured to communicate with the ground service communication network and the database. The computer-based system is configured to update the configuration data and the status data of GSE and aircraft stored in the database on basis of communication data received from the ground service communication network. The computer-based system is further configured to estimate a damage source among the GSE for a damage inflicted on the aircraft by one of the GSE by correlating damage characteristics of the damage with the configuration data and the status data from the database.

Claims

1. A system for damage tracking and monitoring during ground handling of aircraft, comprising:

a ground service communication network configured to transmit communication data between ground support equipment (GSE) and aircraft;

a database configured to store configuration data and status data of GSE and aircraft; and

a computer-based system configured to communicate with the ground service communication network and the database;

wherein the computer-based system is configured to update the configuration data and the status data of GSE and aircraft stored in the database on basis of communication data received from the ground service communication network; and

wherein the computer-based system is configured to estimate a damage source among the GSE for a damage inflicted on the aircraft by one of the GSE by correlating damage characteristics of the damage with the configuration data and the status data from the database.

2. The system according to claim 1, further comprising:

a damage detection system configured to detect damage inflicted on aircraft and to provide damage characteristics of the detected damage,

wherein the computer-based system is further configured to communicate with the damage detection system and to estimate a damage source among the GSE for a damage detected by the damage detection system by correlating damage characteristics of the detected damage provided by the damage detection system with the configuration data and the status data from the database.

3. The system according to claim 1, wherein the damage detection system is aircraft based and/or ground based.

4. The system according to claim 1, wherein the damage detection system is configured to detect impacts on aircraft.

5. The system according to claim 4, wherein the damage detection system comprises a plurality of acceleration sensors placed on aircraft for detecting impacts.

6. The system according to claim 4, wherein the damage detection system is configured to evaluate impact damage on structural components formed from composite material.

7. The system according to claim 6, wherein the damage detection system comprises a plurality of piezoelectric transducers placed on the composite structures for evaluating impact damage on the composite structures by actuating and sensing elastic wave propagation in the composite structures.

8. The system according to claim 1, wherein the configuration data includes type and/or mass and/or shape and/or allowed paths of GSE and/or aircraft.

9. The system according to claim 1, wherein the status data includes speed and/or position and/or orientation and/or condition and/or ground attitude of GSE and/or aircraft.

10. The system according to claim 1, wherein the damage characteristics include time and/or location and/or type and/or size and/or affected area on the aircraft and/or potential of the damage.

11. A method for damage tracking and monitoring during ground handling of an aircraft, comprising:

transmitting and receiving communication data via a ground service communication network between ground support equipment (GSE) aircraft and a computer-based system;

storing and updating configuration data and status data of GSE and aircraft on a database with the computer-based system on basis of the communication data received from the ground service communication network; and

estimating a damage source among the GSE with the computer-based system for a damage inflicted on the aircraft by one of the GSE by correlating damage characteristics of the damage with the configuration data and the status data from the database.

12. The method according to claim 11, further comprising:

detecting damage inflicted on aircraft with a damage detection system and providing damage characteristics of the detected damage,

wherein transmitting and receiving communication data via the ground service communication network includes transmitting and receiving communication data from and to the damage detection system, and

wherein estimating the damage source among the GSE with the computer-based system includes estimating the damage source among the GSE for a damage detected by the damage detection system by correlating damage characteristics of the detected damage provided by the damage detection system with the configuration data and the status data from the database.

13. The method according to claim 12, wherein detecting damage inflicted on aircraft with the damage detection system includes estimating an approximate damage area on the aircraft and/or calculating a damage potential of the damage.

14. The method according to claim 11, further comprising:

assessing an impact of the damage on aircraft operations and requesting an inspection of the aircraft if necessary.

15. The method according to claim 11, further comprising:

analyzing the configuration data and the status data of GSE and aircraft and sending an alert warning if the configuration data and/or status data of GSE and/or aircraft are not conforming to pre-defined presets.

16. A system for damage tracking and monitoring during ground handling of aircraft, comprising:

a ground service communication network configured to transmit communication data between ground support equipment (GSE) and aircraft;

a database configured to store configuration data and status data of GSE and aircraft; and

a computer-based system configured to communicate with the ground service communication network and the database;

wherein the computer-based system is configured to update the configuration data and the status data of GSE and aircraft stored in the database on basis of communication data received from the ground service communication network;

wherein the computer-based system is configured to estimate a damage source among the GSE for a damage inflicted on the aircraft by one of the GSE by correlating damage characteristics of the damage with the configuration data and the status data from the database; and

a damage detection system configured to detect damage inflicted on aircraft and to provide damage characteristics of the detected damage,

wherein the computer-based system is further configured to communicate with the damage detection system and to estimate a damage source among the GSE for a damage detected by the damage detection system by correlating damage characteristics of the detected damage provided by the damage detection system with the configuration data and the status data from the database.

17. The system according to claim 16,

wherein the damage detection system is aircraft based and/or ground based;

and

wherein the damage detection system is configured to detect impacts on aircraft.

18. The system according to claim 17,

wherein the damage detection system comprises a plurality of acceleration sensors placed on aircraft for detecting impacts;

and

wherein the damage detection system is configured to evaluate impact damage on structural components formed from composite material.

19. The system according to claim 18,

wherein the damage detection system comprises a plurality of piezoelectric transducers placed on the composite structures for evaluating impact damage on the composite structures by actuating and sensing elastic wave propagation in the composite structures;

and

wherein the configuration data includes type and/or mass and/or shape and/or allowed paths of GSE and/or aircraft.

20. The system according to claim 19,

wherein the configuration data includes type and/or mass and/or shape and/or allowed paths of GSE and/or aircraft;

wherein the status data includes speed and/or position and/or orientation and/or condition and/or ground attitude of GSE and/or aircraft; and

wherein the damage characteristics include time and/or location and/or type and/or size and/or affected area on the aircraft and/or potential of the damage.