Thermal
Imaging from Thermal Survey Ltd
What
is thermal imaging?
Principles of infra-red radiation.
Equipment types.
Image interpretation.
Survey Techniques.
What
is Thermal Imaging?
Infra-red radiation is electromagnetic
radiation, as are radio waves and visible light. Electromagnetic radiation
ranges from low frequency, long wavelength emissions such as the Rugby
Radio Clock at 60Khz (5000 metres) to X-rays whose frequency may exceed
1020Hz, a wavelength of 3 x 10-12 metres. All these
emissions share the same free space velocity of 2.99 x 108
m/s.

Infra-red radiation is emitted
by every object above absolute zero, (-273°C). The amount to which
an object will emit infra-red radiation is partly governed by the temperature
of the object. This infra-red radiation can be detected using a thermal
imager which can then produce a pictorial representation of the object.
It is important to remember
that the thermal imager produces a picture totally made up of detected
heat with no visible light content whatsoever. Infra-red imaging, by
detecting small radiant temperature differences at high spatial resolutions,
presents an excellent way of monitoring the energy efficiency of buildings,
pipelines, plant & equipment and electrical power distribution.
These are by no means the only uses for thermal imaging equipment however,
such equipment has been used in applications as diverse as airborne
animal counting and mineshaft detection.
Principles
of Infra-red Radiation
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Infra-red radiation is
emitted by every object in the universe, so long as that object is
above absolute zero, (-273°C).
The distribution of radiation
with wavelength, according to the temperature of the body, is shown
in the black body curves below. (A black body being a theoretical perfect
radiator with an emissivity of 1.0)
A very nice demonstration
of Planck
Curves may be found at Electro Optical Industries, Inc.
This distribution of radiant
energy follows Planck's Law as shown in the figure. Max
Planck being a Nobel prize winning physicist of the early 20th Century.
From these curves, we can
clearly see that the frequency at which maximum radiation occurs changes
depending upon the actual temperature of the object. This is of use
when determining the wavelength of infra-red radiation that should be
studied to provide an image of the object.
In practice, the total energy
emitted by the object is of interest. This total emission is the integral
of the curve above and is defined by the Stefan-Boltzman Law:
Although in practice, many
factors influence the detected signal intensity. We can see that there
are two major factors which must be taken into account when considering
thermal imaging of an object.
The absolute temperature
of the object which defines the wavelength at which maximum (but not
all) radiation occurs, in addition to influencing the amount of total
radiation.
The emissivity
of the object which defines how much radiation will be emitted from
the object. The emissivity of an object can also cause other complications
which will be looked at later.
Infra-red lies past the red end of the visible light spectrum and for
imaging purposes can be regarded as the wavelengths covered between
1µm and 20µm. (micron = µm = 1 x 10-6 metres).
Infra-red in the 1µm
region is generally used for non-imaging applications such as short
range remote controls or basic intruder detection systems.
There are several areas across
the infrared wavelength spectrum in which the absorption of radiation
by the atmosphere renders these wavelengths unusable for imaging applications.
This extreme atmospheric absorption is caused mainly by carbon dioxide
and water vapour present in the atmosphere.
This leaves us with two
bands of Infra-red radiation that are transmitted through the atmosphere
well enough to enable imaging to take place. These are the 3 - 5 µm
and 8 - 14µm bands.
By examining black body (Planck)
curves, we can see that a radiator at ambient temperature would radiate
most effectively in the 8 - 14µm band whereas a hotter object
such as a furnace would emit the greater amount of its radiation in
the 3 - 5 µm band. When considering thermal imaging equipment,
the anticipated temperature of the object under examination should be
used to give an indication of the most suitable band to use. It should
however, be remembered that most radiators will be emitting radiation
in both bands so that images may be produced in either band.
Equipment
Types
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In both of the imaging bands
considered, there are two types of detector that may be used to convert
the incoming infra-red thermal radiation to an electrical signal suitable
for processing into a pictorial output; Thermal Detectors and Quantum
Detectors.
Thermal detectors rely on
a change in material characteristic caused by absorption of infra-red
energy. The most common type of thermal detector uses the pyro-electric
effect in which the temperature change of the element causes a change
in the charge present on the device electrodes. These are the types
of detector element used in fire and intruder detection systems. They
have the advantage of not requiring cooling and are also used as part
of PEV imaging systems.
More sophisticated imaging
systems tend to use quantum detectors, these are semiconductor devices
in which incident radiation excites excess carriers, proportional to
the radiation intensity.
The most common semiconductor
used as a quantum detector is Cadmium Mercury Telluride (CMT), this
has the advantage that its composition can be adjusted to give maximum
sensitivity at either 3 - 5 µm or 8 - 14µm.
The signal output of a quantum
detector is so small that it would be swamped by noise generated internally
to the device at room temperatures.
Since noise within a semiconductor
is partly proportional to temperature, quantum detectors must be operated
at low temperatures. CMT detectors should be operated at -80°C when
operating in 3 - 5µm modes and to -193°C when operating in
the 8 - 14µm band.
This cooling requirement
is a significant disadvantage in the use of quantum detectors. However,
their superior electronic performance still makes them the detector
of choice for the bulk of thermal imaging applications.
There are several different
ways of cooling the detector to the required temperature.
Bulk liquid. In
the early days of thermal imaging, liquid nitrogen was poured into
imagers to cool the detector. Although satisfactory, the logistical
and safety implications led to developments into HPPG and thermal
transfer technology.
HPPG. High Pressure
Pure Gas can be used to cool a detector to the required temperatures.
The Joule Thomson effect is the reduction in temperature of a gas
when it rapidly expands from a high to low pressure. The gas is passed
via a pipe coil to an orifice (typically <100µm in diameter),
the gas rapidly expands and undergoes a rapid loss in temperature.
The waste gas passing upwards past the incoming coil cools the incoming
gas further until the cooler has provided a rapid cool down to design
temperature. Suitable gases are Nitrogen, Oxygen, Air and Argon. In
general use, Pure air is the most common gas used due to the relative
simplicity and low cost of producing suitable volumes of gas. Particular
care must be taken regarding the purity of the gas used in a Joule
Thomson cooler. Since the orifice is so small, any particulate contamination
will block the cooler, as will the formation of ice if there is any
water vapour in the gas. Therefore, suitable filtration must be provided
at all stages. A typical thermal imaging facility will clean and dry
the air during the charging of bottles and the air will also be passed
via a filter assembly when being subsequently fed to the detector.
Mechanical cooling
systems are also in use. These have the logistical advantages
of freeing the imager from the requirements of carrying high pressure
gases or liquid nitrogen. They do however, have a number of disadvantages
when compared to a Joule Thomson system such as higher noise level,
electrical interference, longer reaction time, increased power requirements,
additional control circuitry and they have, in the past, gained a
poor reputation for reliability. Modern split cycle Stirling coolers
have overcome (or reduced to acceptable levels) these disadvantages
and are now coming into widespread use in commercially available imagers.
There are a number of different ways in which imagers operate, these
can be roughly classified into PEV, Staring Array and Scanning systems.
A Pyro-Electric Vidicon
(PEV) is a variation of a conventional vidicon camera tube. A plate
of pyroelectric material is placed at the front of a vidicon tube, this
effectively forms a variable capacitance with its characteristics varying
according to the incident infra-red radiation. The plate matrix is scanned
by an electron beam and the resultant impulses amplified and processed
into a video signal. These are uncooled devices and although in service
for basic applications are no substitute for cooled quantum detector
based systems. Since the pyroelectric effect depends upon a change in
incident radiation, they have to be constantly moved to produce an output.
In practice, this is achieved by using a mechanical optical 'chopper'
to interrupt the thermal radiation scene. They have limited spatial
resolution due to thermal spreading (conduction) within the cell matrix
on the front plate of the vidicon.
Staring Arrays, as
the name implies, consist of a matrix of detector elements. These elements
are often manufactured from Cadmium Mercury Telluride or Platinum Sillicide.
The entire scene is focused on this array, each element cell then provides
an output dependent upon the infra-red radiation falling upon it. These
types of imagers have the advantages of not requiring delicate thermionic
devices (such as the vidicon) or sophisticated scanning optics. However,
at the moment, although a number of commercial imagers do use this technology,
there are practical limitations in producing an array with a large enough
number of elements to match the resolution achieved by scanning systems.
This is an area of imaging where significant development is currently
taking place, particularly for midrange commercial applications.
The bulk of high resolution
(military grade) thermal imagers use scanned optical techniques.
They use a cooled CMT detector which is scanned across the image in
a number of formats.
In the simplest form, a single
element could be scanned along each line in the frame (serial scanning).
In practice, this would require impossibly high scan speeds so a series
of elements may be used. These may be scanned as a block, along each
line. This cuts down the scan speed from having just a single detector
but the scan speed and channel bandwidth requirements are still high.
It does however, give a good degree of uniformity. The frame movement
can be provided by frame scanning optics or in the case of linescan
type imagers, by the movement of the imager itself. This type of imager
is often used in aerial applications where the detector element(s) are
scanned along the same line, whilst the forward movement of the aircraft
provides the relative frame movement. These imagers often provide a
digital or photographic output rather than a CCIR video signal. Problems
of non-linearity may be introduced by lateral movement of the aircraft.
Another method is to use
a number of elements scanning in parallel (parallel scanning).
These have one element per line but scan several lines simultaneously,
this can give rise to poor uniformity. However, frame scan speeds are
lower.
A frequently used compromise
is to use a serial/parallel matrix. This provides acceptable uniformity
in conjunction with realisable bandwidths and scanning speeds.
Each of the above methods
has its advantages and disadvantages. They are all in use in modern
thermal imagers.
Another type of CMT based
detector is the SPRITE. This again is a cooled detector which requires
scanning optics. SPRITE (Signal Processing In The
Element) takes the place of several serial elements. The processing
that would have been done external to those elements now takes place
due to semiconductor biasing & doping within the SPRITE element
itself.. This has the advantage of reduced encapsulation lead-outs,
less signal processing circuitry and an improved signal to noise ratio.
Several SPRITEs may be used in a parallel scan to further improve efficiency.
Most of the modern top quality imagers now available, including some
of those used by Thermal Survey Ltd, use SPRITE technology. Multi-element
SPRITE systems may still be regarded as restricted military technology.
When considering the optical
requirements for thermal imagers, it is important to consider the optical
material used. At infra-red imaging wavelengths, glass becomes a complex
radiator and cannot be used to transmit radiation. There are many materials
with suitable infra-red properties but these are often of restricted
use due to physical limitations.
Germanium has become the
most popular material as it is now readily available in large sizes
with good optical characteristics. A wide range of protective coatings
exist and it is in almost universal use for standard imaging applications.
Its only major drawback is that it becomes opaque above 100°C, making
it unsuitable for high speed aerial applications.
Zinc sulphide, zinc selenide,
sapphire and magnesium fluoride are also used in certain applications.
Image
Interpretation
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Most thermal imagers produce
a video output in which white indicates areas of maximum radiated energy
whilst black indicates areas of lower radiation. Most cameras have the
facility to invert this video so that black relates to maximum radiation
and vice versa.
This video output is recorded
onto high quality, broadcast standard video tape on site. The resultant
tape can then be analysed by Thermal Survey's image processing computer
systems. The image is also available for viewing whilst filming is taking
place. In this way, a Client Engineer can often plan remedial action
at the scene.
The original black/white
signal contains the maximum amount of information, certainly more than
the eye can distinguish. However, in order to ease general interpretation
and facilitate subsequent presentation, the thermal image can be artificially
colourised. This is achieved by allocating desired colours to blocks
of grey levels to produce the familiar colourised images. This enables
easier image interpretation to the untrained observer. Additionally,
by choice of the correct colourisation palette, the image may be enhanced
to show particular energy levels in detail. For example, the operator
can choose a palette to highlight cryogenic temperatures or by selecting
another palette, objects at high temperatures.
As mentioned above, the amount
of infra-red radiation emitted from a surface depends partly upon the
emissivity of that surface. For this reason, extreme care is needed
if using an infra-red imager to give accurate temperature measurements
within an image. By far and away, the main benefit of thermal imaging
is obtained from qualitative rather than quantitative use. Infra-red
non-contact thermometers do exist but they all require accurate assessment
of surface emissivities if the result is to be meaningful.
When interpreting infra-red
images, remember that the image is comprised purely of radiated thermal
energy. The effects of the sun, shadows, moisture and subsurface detail
must all be taken into account as described below.
Often with infra-red building
surveys, the item looked for, or the problem to be diagnosed, is not
immediately apparent. Bear in mind that the imager is looking at the
radiation emitted from the surface. The imager does not have the ability
to see below the surface as such; however, the radiation from the surface
is often influenced by subsurface detail such as buried conduit, cracks,
wall ties etc. which all effect the thermal characteristics of the adjoining
material. When conducting aerial surveys, sub-surface detail becomes
even more apparent with buried pipework (hot or cold) being clearly
visible because of their effect on the surface temperature and emissivity.
In the same way, air flow
can often be detected by its cooling or heating effects as it enters
or leaves the building structure. Moisture can often be seen as a result
of cooling of the surface material by evaporation. If a wall is subject
to dampness, the resulting image will show an uneven response due to
the varying degrees of evaporation. It is sometimes possible to follow
the path of water ingress through the building structure in this way.
This does however, mean that surveys should not be carried out in the
rain or whilst the building structure is wet as misleading results will
result.
The following factors should
also be borne in mind:
The effect of solar gain
on the thermal structure of a building can lead to confusion. In general,
infra-red surveys are carried out sometime after sunset so that all
such effects have dissipated from the structure. However, this is
not always possible and the position of the sun relative to the building
should be considered. In this case, shadows falling on the building
or shadows that have been on the building, can also have an appreciable
effect on the thermal radiation viewed.
When looking at a large
area, the emissivity of various surfaces must be considered. Most
materials found on the surface of buildings will have a relatively
high emissivity (~ 0.95) but there will still be noticeable differences
in the perceived image due to a change in surface material. This can
be overcome by a detailed knowledge of the building under investigation.
When imaging surfaces
such as metal or glass, special care must be taken. Polished
metal surfaces tend to reflect infra-red radiation in the same
way that they do visible light. Hence, an apparent 'hot-spot'
may be a reflection of a hot object some distance away from
the area under investigation. Such anomalies can be detected
by moving the imager around so that the reflective angles change.
Glass is predominantly
opaque to infra-red radiation (particularly so at 8 - 14µm)
and in most cases, the image will be dominated by reflection. Hence,
in ground floor windows, a reflected image of the survey team will
often be noted and in upper floor windows the reflection of the cold
sky temperature will be apparent. Glass is a selective radiator with
an emissivity which fluctuates markedly with wavelength. These examples
serve to emphasise that the radiation properties of the target materials
being surveyed need to be known. Are the surfaces blackbody, grey
body or selective radiators?
Survey
Techniques
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The primary considerations
for all survey activity are the environmental conditions.
If looking at buildings,
as per the majority of ground surveys, a temperature differential must
exist between the inside and outside of the building. In this case,
in the event of an insulation defect, warmth will be seen leaving the
building structure if viewed from the outside. If the survey is being
conducted from the inside, conduction from the external cold air in
the vicinity of a defect will be noticed.
To achieve this differential,
surveys are most often conducted in the winter months when the outside
air temperature is at a minimum and the buildings are heated. The exceptions
to this are refrigerated buildings which may be surveyed during summertime
to achieve maximum differential.
As mentioned previously,
areas of dampness will give an uneven thermal response. This may be
confused with defective areas of insulation so care should be taken
to avoid surveying when walls may be damp. (Unless of course, the object
of the survey is to identify areas of dampness).
Wet ground, snow or frost
will give rise to misleading survey images so care must be taken
if conducting surveys during such periods.
Very much the same conditions
apply to aerial surveying. Additionally, the cloudbase must not extend
below the survey height since the water vapour in the clouds makes them
opaque to infra-red. Care must be taken to ensure that survey flights
are not made in excessively windy conditions. If the wind is too high,
the effects of wind-chill will be seen around the edges of buildings
and the image quality may be poor if the aircraft has difficulty remaining
on a stable track heading. The exact threshold speed will depend upon
aircraft type and the nature of the images required, but would be generally
around 15 knots.
For aerial surveying, the
imager may be mounted in a camera hatch of any suitable modified observation
aircraft. A typical Thermal Survey survey would be flown at 610 metres
altitude above ground level. This gives a field of view swathe 420 metres
wide. The survey area is then divided up into parallel tracks 300 metres
apart. This gives a degree of overlap to allow for wind gusts, aircraft
roll or positional error.
The resultant video output
from the camera is fed to a time/date generator which superimposes a
time/date stamp on the video signal. This can then be used to cross
reference the images with the tracks plotted on a map.
Used correctly, infra-red
thermal imaging is a valuable tool for evaluating the conditions of
buildings, plant & machinery. They are of use in diagnostic, quality
control and work prioritisation roles to name but a few.