IP Library Granted Patent US 8,683,869
Granted Patent B2
US 8,683,869 · App. 12/536,438 · Granted Apr 1, 2014

Monitoring fastener preload

Inventors: Peter E. Herley (Renton, WA); Bruce W. Blayden (Everett, WA); Thomas J. Lowe (Kent, WA)
Assignee: The Boeing Company
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,683,869
App. No.
12/536,438
Granted
Apr 1, 2014
Kind
B2
Abstract

The health of a structural joint clamped by fasteners is monitored by directly measuring the preload of the fasteners. The preload is measured by a transducer on the fastener and electronically transmitted to a monitoring station where the preload values may be analyzed to assess the health of the joint.

Claims (58)

1. A method of monitoring the preload of fasteners installed on a vehicle, comprising:

measuring the value of fastener preload of each of the fasteners;

electronically transmitting the measured preload values from each of the fasteners to a monitoring station;

using a programmed computer to monitor the measured preload values at the monitoring station; and

assessing the health of the vehicle based on comparing the measured preload values with reference values.

2. The method of claim 1 , wherein transmitting the measured preload is performed wirelessly.

3. The method of claim 1 , further comprising:

reading an identifier at each of the fasteners that uniquely identifies the fastener; and

transmitting the unique identifier from each of the fasteners to the monitoring station.

4. The method of claim 1 , wherein using the programmed computer to monitor the measured preload values includes:

using the programmed computer to analyze the measured preload values, and

displaying each of the measured preload values.

5. A method of monitoring the preload of fasteners installed on an airplane, comprising:

reading an identifier on the fastener that uniquely identifies the fastener;

associating each identifier with a corresponding preload value;

measuring the values of preload on each of the fasteners;

using a transducer on each of the fasteners to sense the preload of the fastener;

reading the value of the sensed preload from the transducer;

generating an electronic data file containing the measured values of preload; and

using the electronic data file to display the measured values of preload.

6. The method of claim 5 , further comprising:

electronically transmitting the measured preload values from on-board the airplane to the monitoring station, and

wherein displaying the measured preload values is performed at the monitoring station.

7. The method of claim 5 , further comprising:

using a programmed computer at the monitoring station to compare the measured values of preload with a set of reference values.

8. The method of claim 5 , further comprising:

displaying a representation of the location on the airplane of a fastener whose preload value has been measured.

9. A method of monitoring the health of a vehicle, comprising:

electronically measuring the preload of each of a plurality of fasteners on the vehicle; and,

using the measured preloads to assess the health of the vehicle, wherein using the measured preloads includes comparing the measured preloads with a set of reference values related to the health of the vehicle.

10. The method of claim 9 , wherein the measuring includes using a transducer on the fastener to sense the preload on the fastener.

11. A fastener installation and preload measurement method, comprising:

specifying a set of fasteners to be installed on a structure;

providing the set of fasteners;

providing a set of preload measurement transducers;

affixing the transducers to the fasteners;

generating a set of unique identifiers respectively linking the fasteners to the transducers;

installing the fasteners on the structure; and

using the transducers affixed to the fasteners to measure the preloads on the fasteners installed on the structure.

12. The system of claim 11 , wherein generating the unique identifiers includes assigning unique serial numbers respectively to the transducers.

13. The system of claim 12 , further comprising:

generating a plan for installing the fasteners on the structure, and

wherein the fasteners are installed according to the plan using the serial numbers assigned to the transducers.

14. The system of claim 11 , further comprising:

using a computer to collect the measured values of preload; and

using a computer and the unique identifiers to display the measured values of preload of the fasteners.

15. Apparatus for monitoring the preload on fasteners installed on a structure, comprising:

a transducer on each of the fasteners for sensing the preload on the fastener and generating a signal related to the sensed preload;

an identifier on each of the transducers that uniquely identifies the transducer;

a monitoring station for monitoring the signals generated by the transducers, including a computer for analyzing the sensed preloads; and

means for transmitting the signals from each of the transducers to the monitoring station, the transmitting means is operable for transmitting each of the identifiers to the monitoring station.

16. The apparatus of claim 15 , wherein the transmitting means includes a wireless transmitter for wirelessly transmitting the signals from the transducers to the monitoring station.

17. The apparatus of claim 15 , further comprising:

a reader coupled with the transmitting means for reading the signals generated by the transducer.

18. The method of claim 9 , the electronically measuring further comprising placing a reader over each of the plurality of fasteners on the structure to engage the transducer on the fastener with a probe of the reader.

19. The method of claim 9 further comprising accessing maintenance and repair records to assess the health of the structure.

20. The method of claim 7 further comprising comparing the measured values of preload with a tolerance range for the preload.

21. The method of claim 1 further comprising using the programmed computer to continuously monitor the measured preload values at the monitoring station.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 5, 2009
From: HERLEY, PETER E.; BLAYDEN, BRUCE W.; LOWE, THOMAS J.
To: BOEING COMPANY, THE
Reel/Frame 023058/0707 →
Continuity (2)
Provisional Application 61190986 · Sep 4, 2008
Related Publication 20100050778A1 · Mar 4, 2010