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NASA Scientific and Technical Aerospace Reports

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Gas sensor devices are provided having an atomically flat silicon carbide top surface that, in turn, provides for a uniform,<br />

<strong>and</strong> reproducible surface thereof.<br />

Official Gazette of the U.S. Patent <strong>and</strong> Trademark Office<br />

Fabrication; Gas Detectors; Semiconductors (Materials); Silicon Carbides<br />

20040120992 <strong>NASA</strong> Glenn Research Center, Clevel<strong>and</strong>, OH, USA<br />

Auto-Adjustable Tool for Self-Reacting <strong>and</strong> Conventional Friction Stir Welding<br />

Carter, Robert W., Inventor; April 30, 2002; 6 pp.; In English; Original contains black <strong>and</strong> white illustrations<br />

Patent Info.: Filed 2 May 2003; US-Patent-6,758,382; US-Patent-Appl-SN-431655; <strong>NASA</strong>-Case-LEW-16056-3<br />

Report No.(s): SHINe; No Copyright; Avail: CASI; A02, Hardcopy<br />

A friction stir welding dcvice that is configured to perform convention friction stir welding as well as self-reacting friction<br />

stir welding is described. A pin passes hrough an upper shoulder <strong>and</strong> can selectively attach 10 <strong>and</strong> detach from a lower<br />

shoulder in a preferred embodiment. A controller maintains thc discrete position of, <strong>and</strong>/or force applied by, the upper <strong>and</strong><br />

lower shoulders during self-reacting friction stir welding, or maintains the pin at a desired depth <strong>and</strong>/or applied force during<br />

conventional friction stir welding.<br />

Author<br />

Friction Stir Welding; Diagrams<br />

20040120999 <strong>NASA</strong> Dryden Flight Research Center, Edwards, CA, USA<br />

Force-Measuring Clamp<br />

Nunnelee, Mark, Inventor; July 06, 2004; 10 pp.; In English; Original contains black <strong>and</strong> white illustrations<br />

Patent Info.: Filed 20 Feb. 2002; US-Patent-6,758,098; US-Patent-Appl-SN-084747; <strong>NASA</strong>-Case-DRC-099037; No<br />

Copyright; Avail: CASI; A02, Hardcopy<br />

A precision clamp that accurately measures force over a wide range of conditions is described. Using a full bridge or other<br />

strain gage configuration. the elastic deformation of the clamp is measured or detected by the strain gages. Thc strain gages<br />

transmit a signal that corresponds to the degree of stress upon the clamp. Thc strain gage signal is converted to a numeric<br />

display. Calibration is achieved by ero <strong>and</strong> span potentiometers which enable accurate measurements by the force-measuring<br />

clamp.<br />

Author<br />

Strain Gages; Clamps<br />

38<br />

QUALITY ASSURANCE AND RELIABILITY<br />

Includes approaches to, <strong>and</strong> methods for reliability analysis <strong>and</strong> control, quality control, inspection, maintainability, <strong>and</strong> st<strong>and</strong>ardization.<br />

20040111273 Building <strong>and</strong> Construction Research TNO, Delft, Netherl<strong>and</strong>s<br />

Evaluation of Availability <strong>and</strong> Reliability Data of the Main Propulsion Diesel Engines of the M-Frigates <strong>and</strong> the<br />

Amphibious Transport Ship of the Royal Netherl<strong>and</strong>s Navy<br />

Korse, T. H.; March 08, 2004; 42 pp.; In English<br />

Contract(s)/Grant(s): A02/KM/181; TNO Proj. 006.28217<br />

Report No.(s): TD-2004-0107; Rept-2004-CMC-R011; Copyright; Avail: Other Sources<br />

The databases of the M-frigates <strong>and</strong> the amphibious transport ship Rotterdam of the Royal Netherl<strong>and</strong>s Navy give<br />

valuable information about the availability <strong>and</strong> reliability of the diesel engines <strong>and</strong> the sensitivity for failure of the individual<br />

functional groups. The average availability of the diesel engines of the Rotterdam is higher than the average availability of<br />

the diesel engines of the M-frigates. The average search time <strong>and</strong> repair time per failure is considerably less than the average<br />

waiting time per failure. This is caused by the incidentally <strong>and</strong> exceptionally long waiting time of an ordered component. Most<br />

failures occur in the functional groups for fuel systems <strong>and</strong> electronic components including sensors. In case of the M-frigates,<br />

the number of failures per frigate <strong>and</strong> per year shows a local maximum at about 5 to 7 years after delivery of the respective<br />

frigate.<br />

Author<br />

Diesel Engines; Ships; Reliability; Service Life; Failure Analysis<br />

132

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