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Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

Scientific and Technical Aerospace Reports Volume 39 April 6, 2001

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Contract(s)/Grant(s): F19628-95-C-0002<br />

Report No.(s): AD-A384805; MIT-MS-13783; ESC-TR-99-085; Copyright; Avail: Defense <strong>Technical</strong> Information Center<br />

(DTIC)<br />

In situ laser cleaning is shown to be an effective tool for removal of organic contaminants on CaF2 windows. to study laser<br />

cleaning in a controlled fashion, CaF2 substrates were pre-contaminated with 5 to 10 nm of poly(methyl methracylate),<br />

poly(4-hydroxy styrene), poly(norbomene), <strong>and</strong> poly(beta-pinene) thin films. Irradiation of all the polymer films showed similar<br />

trends. Initially, a high rate of material removal occurs, which depends on the chemistry of the polymer. During this period, the<br />

material also undergoes significant bond rearrangement, forming a more tightly bound highly conjugated network. Removal of<br />

this residual ’graphitized’ film is significantly more difficult, but can be accelerated by the presence of modest levels of oxygen.<br />

For oxygen concentrations between 10 - 1000 ppm, the measured removal rate is approximately 3 hm/(kJ/sq cm)/ppm oxygen.<br />

No effect on removal rate was observed as pulse energy or purge gas flow rate was varied over ranges expected to be used in practical<br />

systems.<br />

Author<br />

Cleaning; Contamination; Irradiation; Lasers; Lithography<br />

37<br />

MECHANICAL ENGINEERING<br />

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<strong>2001</strong>0024110 Department of the Navy, Washington, DC USA<br />

Grommet Having Metal Insert<br />

Roush, Robert A., Inventor; Bartlett, David I., Inventor; Young, William T., Inventor; Sep. 28, 1998; 10p; In English<br />

Patent Info.: Filed 28 Sep. 1998; US-Patent-Appl-SN-9,162,633<br />

Report No.(s): AD-D019427; No Copyright; Avail: Defense <strong>Technical</strong> Information Center (DTIC)<br />

The invention is directed to a grommet including a cylindrical body fabricated from rubber or synthetic rubber material. The<br />

body has a centrally located aperture extending there through <strong>and</strong> at least one radially located aperture with a slit for easily receiving<br />

a cable or the like. The grommet further includes a rigid insert secured to the body in the centrally located aperture. The insert<br />

has female threads formed therein for releasably securing a tool there to remove the grommet from the ballast tank without destroying<br />

the body of the grommet. The insert has a tubular member <strong>and</strong> an outwardly projecting circumferential flange formed on the<br />

tubular member. The body is formed on the tubular member wherein the flange secures the insert axially with respect to the body.<br />

Preferably, the body is fabricated from neoprene <strong>and</strong> is vulcanized to its final form.<br />

DTIC<br />

Reinforcement Rings; Cylindrical Bodies; Apertures; Inserts<br />

<strong>2001</strong>0025814 S<strong>and</strong>ia National Labs., Albuquerque, NM USA<br />

Effects of Injector Conditions on the Flame Lift-Off Length of DI Diesel Sprays<br />

Siebers, D. L.; Higgins, B. S.; Jul. 01, 2000; 27p; In English<br />

Report No.(s): DE00-758328; SAND2000-8249; No Copyright; Avail: Department of Energy Information Bridge<br />

The effects of injection pressure <strong>and</strong> orifice diameter on the lift-off length of a direct-injection (DI) diesel spray (defined as<br />

the farthest upstream location of high temperature combustion) were investigated using a natural light emission imaging technique.<br />

The lift-off length experiments were conducted in a constant-volume combustion vessel under quiescent, heavy-duty DI<br />

diesel engine conditions using a Phillips research grade No.2 diesel fuel. The results show that natural light emission at 310 nm<br />

provides an excellent marker of the lift-off length. At this location, natural light emission at 310 nm is dominated by OH chemiluminescence<br />

generated by high-temperature combustion chemistry. Lift-off lengths determined from images of natural light emission<br />

at 310 nm show that as either injection pressure (i.e., injection velocity) or orifice diameter increase, the lift-off length<br />

increases. The observed lift-off length increase was linearly dependent on injection velocity, the same dependency as previously<br />

noted for gas jets. The lift-off length increase with increasing orifice diameter, however, is different than the independence of liftoff<br />

length on orifice diameter noted for gas jets An important overall observation was made by considering the lift-off length data<br />

in conjunction with data from recent investigations of liquid-phase fuel penetration <strong>and</strong> spray development. The combined data<br />

suggests that a systematic evolution of the relationship <strong>and</strong> interaction between various processes in a DI diesel spray has been<br />

occurring over time, as injection pressures have been increased <strong>and</strong> orifice diameters reduced as part of efforts to meet emissions<br />

151

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