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Aircraft survey system and method for determining information about an aircraft

A survey system, aircraft technology, applied in the field of aircraft inspection, can solve the problems of human transcription errors, unreliability, etc.

Active Publication Date: 2022-02-08
THE BOEING CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These physical configuration acquisitions performed manually can lead to human transcription errors (such as when distraction occurs during the inspection process)
Other solutions may involve manual survey records kept during construction (possibly lengthy processing)
Additionally, these records may have been maintained by multiple suppliers and may otherwise be unreliable
In the absence of accurate up-to-date configurations, those using manufactured or as-maintained configurations will further face the challenge of performing maintenance and obtaining accurate spare parts inventory

Method used

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  • Aircraft survey system and method for determining information about an aircraft
  • Aircraft survey system and method for determining information about an aircraft
  • Aircraft survey system and method for determining information about an aircraft

Examples

Experimental program
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example 1

[0028] This example describes an exemplary aircraft survey system (see figure 1 ).

[0029] figure 1 is a schematic diagram of an aircraft survey system generally indicated at 100 . Aircraft survey system 100 may include unmanned aerial vehicle (UAV) 102 and base station 104 . UAV 102 may communicate wirelessly with a base station. Aircraft survey system 100 may be configured to inspect or survey aircraft 106 . The UAV may fly along a survey route 108 approaching the aircraft.

[0030] UAV 102 may include one or more sensors 109 (such as visible light cameras, proximity detectors, radio frequency identification (RFID) readers, or other suitable sensors). When activated, the UAV can use one of the sensors (such as a camera or a proximity detector) to detect the closest aircraft to the base station. The UAV may be configured to record one or more images of the aircraft and to transmit a signal representing the images to a base station. The base station may be configured t...

example 2

[0037] This example describes another exemplary aircraft survey system (see figure 2 ). figure 2 is a block diagram of an aircraft survey system generally indicated at 200 . The aircraft survey system 100 described above may be an implementation of the aircraft survey system 200 . Aircraft survey system 200 may be configured to determine information about aircraft 202 . Aircraft survey system 200 may include unmanned aerial vehicle (UAV) 204 and base station 206 .

[0038] Aircraft 202 may include information 208 such as model type identification data 210 associated with the aircraft model type and / or registration number 212 . Information 208 may be displayed visually as, for example, aircraft identification markings on the tail of the aircraft, on the wings of the aircraft, or on a portion of the fuselage of the aircraft. Information 208 may alternatively be encoded into a radio frequency identification (RFID) tag provided on board the aircraft.

[0039] Aircraft 202 m...

example 3

[0063] This example describes an exemplary set of operations performed in determining information about an aircraft (see image 3 ). image 3 is a view of operations indicated generally at 300 that may be performed in a method of determining information about an aircraft. Some or all of operations 300 may be performed by a base station of an aircraft survey system, such as base station 104 of aircraft survey system 100 or base station 206 of aircraft survey system 200 . Some or all of operations 300 may be performed by an unmanned aerial vehicle (UAV) of an aircraft survey system, such as UAV 102 or UAV 204 . Some or all of operations 300 may be performed in circuitry of a first processor of a base station, where the first processor may execute a first set of computer readable program instructions. Some or all of operations 300 may be performed in circuitry of a second processor of the UAV, where the second processor may execute a second set of computer-readable program inst...

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Abstract

Aircraft survey systems and methods for determining information about an aircraft. The method of determining information about the aircraft (202) may include receiving, at the base station (206), an RFID tag location map (244) for the aircraft (202) and sending the RFID tag location map (244) for the aircraft (202) to a Unmanned Aerial Vehicle (UAV) (204). The method may include generating a navigation signal based at least in part on the received RFID tag location map (244), the navigation signal suitable for controlling the UAV (204) to approach an RFID tag (202) supported on the aircraft (202) at the RFID tag location. 213), the RFID tag (213) has aircraft-related identification data. The method may include receiving, by the base station, read-related data (266) from the UAV (204). Read-related data (266) may include aircraft-related identification data when the RFID tag (213) is in the RFID tag location. The method may include determining, at the base station (206), information about the aircraft (202) from the received read-related data (266).

Description

technical field [0001] The present invention relates generally to aircraft inspections. More specifically, the disclosed embodiments relate to systems and methods for obtaining information about aircraft from onboard radio frequency identification (RFID) tags. Background technique [0002] Aircraft configurations may change during manufacture for a number of reasons. The design of an aircraft can change as the aircraft continues down the assembly line. These design changes may be the result of engineering design changes, the availability of new building kits, changing customer demands, federally mediated modifications, security upgrades, or other factors. Accordingly, the "as-built" configuration of a finished aircraft can be difficult to determine, a difficulty that increases with the complexity of the aircraft. Additionally, the manufactured configuration may not match the intended design specification or any of possibly multiple versions of the expected configuration. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06K17/00
CPCB64C39/02B64D43/00G06K7/10366G06K17/00B64U2101/00G06K17/0029G06Q10/20G06Q50/30B64F5/60B64C39/024G05D1/0094B64U10/13B64U2101/30B64U2201/10B64F5/00G05D1/00G06F7/00G06K7/00G05D1/0011G07C5/00
Inventor J·W·格拉特费尔特
Owner THE BOEING CO