Structural analysis using measurement of fastener parameters

• US 8,521,448 B1
• Filed: 10/21/2009
• Issued: 08/27/2013
• Est. Priority Date: 10/21/2009
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Ung, Kevin Y., Ayyagari, Arun, Battles, Craig F., Farricker, James T., Tillotson, Brian
• Primary Examiner(s): Raymond, Edward
• Application Number:
  US12/582,885
• Time in Patent Office: 1,406 Days
• Field of Search: 702/42, 702182-185
• US Class Current: 702/42
• CPC Class Codes: B64F 5/60 Testing or inspecting aircraft components or systems
• CPC Class Codes: F16B 2200/95 with markings, colours, indicators or the like
• CPC Class Codes: F16B 31/02 for indicating the attainment of a particular tensile load or limiting tensile load apparatus for, or method of, determining value of torque or twisting moment for tightening a nut or other member similarly stressed G01L5/24

Abstract

A computer implemented method is provided for analyzing the health of a structure by measuring the value of preload on each of a plurality of fasteners installed on the structure and correlating the measured values of preload with a set of specifications. A report is generated for each of the fasteners representing the results of the correlations. Groups of the fastener reports are used to infer the health of the structure.

Claims

1. A method of analyzing a structure, comprising:

storing in a plurality of radio frequency identification (RFID) tags a value of at least one parameter indicating a status of each of a plurality of fasteners installed on a structure;

measuring with a handheld reader the value of the at least one parameter stored in the plurality of RFID tags indicating the status of each of the plurality of fasteners installed on the structure;

correlating the measured values;

analyzing the structure based on the results of the correlation; and

generating an analytical report for each of the fasteners based on the results of the correlation, wherein at least one of the correlating and analyzing is performed using a programmed computer.

2. The method of claim 1, wherein the correlating includes:

correlating the measured values to predefined characteristics of the environment in which the fastener is installed and historical operational data for the structure.

3. The method of claim 2, wherein the predefined characteristics and historical operational data include at least one of:

installed fastener location,

allowable maximum load on the fastener,

magnitude of torque used to install the fastener,

ambient temperature range,

the maximum stress and strain to which the fastener has been previously subjected,

the material from which the fastener is constructed, and

the material from which the structure is constructed.

4. The method of claim 1, wherein the parameter is one of:

preload on the fastener,

torque,

ambient temperature surrounding the fastener,

stress or strain, and

an identifier that uniquely identifies the fastener.

5. The method of claim 1, wherein analyzing the structure includes using a computer to infer information representing the health of the structure based on the results of the correlations.

6. The method of claim 5, further comprising:

generating an analytical report for each of the fasteners based on the results of the correlation, and

wherein using the computer to infer the health of the structure is based on the analytical reports.

9. The method of claim 1 further comprising displaying a structural map, the structural map showing a location of each of the plurality of fasteners on the structure.

7. A computer implemented method of analyzing the health of a structure, comprising:

measuring the value of preload on each of a plurality of fasteners installed on the structure;

correlating the measured values of preload with a set of database information relating to the structure;

generating a report for each of the fasteners representing the results of the correlations;

inferring the health of the structure based on a group of the fastener reports;

applying a voltage pulse to each of the plurality of fasteners; and

measuring a time of flight of an ultrasonic wave reflected back from an end of each of the plurality of fasteners.

8. The method of claim 7, wherein the measured values of preload are correlated to at least one of:

the location of the fasteners on the structure,

the tools that were used to install the fastener,

the identity of the manufacturer who manufactured the fasteners,

the temperature of the fasteners,

the magnitude of initial torques used to install the fasteners,

preload tolerances representing allowable maximum and minimums allowable values of preload,

the material from which the structure is made, and

the material from which the fasteners are made.

10. The method of claim 7, further comprising:

wirelessly reading the measured preload values from each of the fasteners.

11. The method of claim 7, wherein inferring the health of the structure is performed by analyzing the correlated values of measured preload for at least two groups of the fasteners.

12. The method of claim 7, further comprising:

measuring the value of at least one parameter related to each of the fasteners other than preload; and

correlating the measured values of the at least one parameter with a set of database information relating to the structure.

13. The method of claim 7, wherein correlating the measured values, generating a report for each of the fasteners and inferring the health of the structure are performed at a ground based station off-board an aircraft.

14. The method of claim 7 further comprising:

measuring the value of preload on each of a second plurality of fasteners installed on a second structure, wherein structure is a first airplane and the second structure is a second airplane identical to the first airplane;

correlating the measured values of preload of the plurality of fasteners with the measured values of preload of the second plurality of fasteners.

15. The method of claim 7 further comprising:

measuring the value of preload on each of a second plurality of fasteners, the second plurality of fasteners being a second group of fasteners installed on a first portion of the structure, wherein the plurality of fasteners are a first group of fasteners separate from the second group of fasteners, the first group of fasteners also being installed on the first portion of the structure;

correlating the measured value of preload of the first group of fasteners with the measured value of preload of the second group of fasteners.

16. A system for analyzing an aircraft structure having a plurality of fasteners installed thereon, comprising:

a first plurality of sensors respectively on a first plurality of fasteners on a first section of the aircraft structure and each operable for measuring the value of at least one parameter related to the associated fastener;

a second plurality of sensors respectively on a second plurality of fasteners on a second section of the aircraft structure and each operable for measuring the value of at least one parameter related to the associated fastener;

a database containing information related to characteristics of the structure;

at least one correlation and analysis module for correlating the measured values from the first plurality of sensors and from the second plurality of sensors, for correlating the measured values of the parameter with at least one of the characteristics contained in the database, and for generating a report reflecting the results of the correlation;

an information inferencing engine for inferring structural information based on the report and for generating a structural analysis report reflecting the inferred structural information; and

a fastener tracking database used by the correlation and analysis module to correlate the measured values, the fastener tracking database including a set of data representing unique characteristics of each of the fasteners.

17. The system of claim 16, where the correlation and analysis module includes a software program.

18. The system of claim 16, wherein the inferencing engine includes a software program.

19. The system of claim 16, further comprising:

a programmed computer coupled with the database for controlling the operation of the correlation and analysis module and the inferencing engine.

20. The system of claim 16, further comprising:

a radio frequency transmitter on each of the fasteners for storing and transmitting the measured values, and

at least one reader on-board the aircraft for interrogating the transmitters and for receiving the measured values from the transmitters.