Detecting Airborne Mercury by Use of Polymer/Carbon Films
NASA’s Jet Propulsion Laboratory, Pasadena, California
Sunday, November 01 2009
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These films can be operated and regenerated at mild temperatures.
Films made of certain polymer/carbon
composites have been found to be
potentially useful as sensing films for
detecting airborne elemental mercury
at concentrations on the order of tens
of parts per billion or more. That is to
say, when the polymer/carbon composite
films are exposed to air containing
mercury vapor, their electrical
resistances decrease
by measurable amounts.
Because airborne mercury
is a health hazard, it is
desirable to detect it with
great sensitivity, especially
in enclosed environments
in which there is a risk of a
mercury leak from lamps
or other equipment.
Figure 1. These Polymers were selected as components of mercury- detecting polymer/carbon sensor films based on quantummechanical computations of energies of binding between mercury atoms and polymer chemical functionalities, like these, containing amine functional group.
The present effort to
develop polymer-based mercury-
vapor sensors complements
the work reported in
NASA Tech Briefs “Detecting
Airborne Mercury by Use of
Palladium Chloride” (NPO-
44955), Vol. 33, No. 7 (July
2009), page 48 and “De -
tecting Airborne Mer cury by
Use of Gold Nanowires”
(npo-44787), Vol. 33, No. 7 (July 2009),
page 49. Like those previously reported
efforts, the present effort is motivated
partly by a need to enable operation
and/or regeneration of sensors under relatively
mild conditions — more specifically,
at temperatures closer to room temperature
than to the elevated temperatures
(>100°C ) needed for regeneration of sensors
based on noble-metal films.
Figure 2. Small Changes in Electrical Resistances of four polymer/carbon composite films to airborne mercury vapor were observed at concentrations as low as tens of parts per billion.
The present polymer/carbon films
are made from two polymers, denoted
EYN1 and EYN2 (see Figure 1), both of
which are derivatives of poly-4-vinyl pyridine
with amine functional groups.
Composites of these polymers with 10 to
15 weight percent of carbon were prepared
and solution-deposited onto the
JPL ElectronicNose sensor substrates for
testing. Preliminary test results showed
that the resulting sensor films gave measurable
indications of airborne mercury
at concentrations on the order of tens of
parts per billion (ppb) or more. The
operating temperature range for the
sensing films was 28 to 40°C and that the
sensor films regenerated spontaneously,
without heating above operating
temperature (see Figure 2).
This work was done by Abhijit
Shevade, Margaret Ryan, Margie
Homer, Adam Kisor, April Jewell, Shiao-
Pin Yen, Kenneth Manatt, Mario
Blanco, and William Goddard of
Caltech for NASA’s Jet Propulsion
Laboratory.
In accordance with Public Law 96-517,
the contractor has elected to retain title to
this invention. Inquiries concerning rights
for its commercial use should be addressed
to:
Innovative Technology Assets Management
JPL
Mail Stop 202-233
4800 Oak Grove Drive
Pasadena, CA 91109-8099
E-mail:
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Refer to NPO-45003, volume and
number of this NASA Tech Briefs issue,
and the page number.
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