Follow this link to go to the text only version of nasa.gov
NASA - National Aeronautics and Space Administration
Follow this link to skip to the main content
+ Text Only Site
+ Contact STI Help Desk
+ Search the NTRS Database
WHAT IS STI? GET HELP REGISTER SITE SEARCH FEEDBACK FAQ


+ Spinoff Home

Spinoff
history of spinoff
request a spinoff
be in spinoff
spinoff database
spinoff Frequently Asked Questions
contact us



SPINOFF 1996

of Spinoff technology fading together
Public Safety

Next Page Gray button with arrow pointing right

Previous Page
Spinoff Contents
Spinoff Homepage


Stress Measurement System

As part of NASA's Aircraft Structural Integrity program (see page 68), Langley Research Center teamed with Stress Photonics Inc., Madison, Wisconsin to develop an infrared-based stress measurement system for use in nondestructive evaluation of materials and structures. Stress Photonics has commercialized the technology and incorporated it into the DeltaTherm 1000 (DeltaTherm 1000 is a trademark of Stress Photonics Inc.) system.

of a man operating the Delta 1000 stress measurement system with its infrared camera
The DeltaTherm 1000 stress measurement system combines digital signal processing technology with an infrared camera.

Both the NASA system, intended for inspection of aircraft structures to detect cracks and disbonds, and the commercial unit make use of the fact that all materials change temperature when compressed or expanded. In solid materials, this effect is known as thermoelasticity. Thermelectric Stress Analysis (TSA) employs special infrared detectors and signal processing equipment to image temperature changes that correspond to the dynamic stresses in a structure; modern TSA systems can measure temperature changes as small as one-thousandth of a degree Centigrade.

Stress Photonics' DeltaTherm 1000 is an infrared differential thermography system for TSA and thermal nondestructive evaluation. The system is used to verify mathematical models of a design, demonstrate the effects of loadings on the design, measure stress concentrations and stress intensity factors in load-bearing components, and survey a structure for potential problem sites. It combines digital signal processing technology with a special infrared camera to provide instantaneous thermal images and live TSA (differential) images. Data collected from the infrared camera is processed at 434 frames a second; processed images are sent to a computer and/or to a video monitor for immediate display.

Infrared image of a chain hook, and the temperature changes that correspond to dynamic stress in a structure.  The stressed areas appear yellow against the blue chain
Used in nondestructive evaluation of materials and structures, the system images temperature changes that correspond to dynamic stresses in a structure.

 


 

 

 

 

 

 

 








Next Page Gray button with arrow pointing right

Previous Page
Spinoff Contents
Spinoff Homepage




USA dot Gov: The U.S. Government's Official Web Portal
+ Sitemap
+ E-GOV Act Regulations
+ Visit the NASA Portal
+ Disclaimers, Copyright Notice, and Terms and Conditions of Use
+ Freedom of Information Act
+ Budgets, Strategic Plans and Accountability Reports
+ The President's Management Agenda
+ NASA Privacy Statement, Disclaimer, and Accessibility
Certification

+ Inspector General Hotline
+ Equal Employment Opportunity Data Posted Pursuant to the
No Fear Act

+ Information-Dissemination Priorities and Inventories
NASA - National Aeronautics and Space Administration
Editor: NASA Center for AeroSpace Information (CASI)
NASA Official: Lynn Heimerl
Last Update: July 10, 2007
+ Contact STI