WO2005045466A1 - Cavity monitoring system - Google Patents

Cavity monitoring system Download PDF

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Publication number
WO2005045466A1
WO2005045466A1 PCT/AU2004/001530 AU2004001530W WO2005045466A1 WO 2005045466 A1 WO2005045466 A1 WO 2005045466A1 AU 2004001530 W AU2004001530 W AU 2004001530W WO 2005045466 A1 WO2005045466 A1 WO 2005045466A1
Authority
WO
WIPO (PCT)
Prior art keywords
waveform
antenna
ghz
radar
reflected
Prior art date
Application number
PCT/AU2004/001530
Other languages
French (fr)
Inventor
Graham Michael Brooker
Original Assignee
Cmte Development Limited
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from AU2003906084A external-priority patent/AU2003906084A0/en
Application filed by Cmte Development Limited filed Critical Cmte Development Limited
Publication of WO2005045466A1 publication Critical patent/WO2005045466A1/en

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21CMINING OR QUARRYING
    • E21C39/00Devices for testing in situ the hardness or other properties of minerals, e.g. for giving information as to the selection of suitable mining tools
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21FSAFETY DEVICES, TRANSPORT, FILLING-UP, RESCUE, VENTILATION, OR DRAINING IN OR OF MINES OR TUNNELS
    • E21F15/00Methods or devices for placing filling-up materials in underground workings
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88Radar or analogous systems specially adapted for specific applications
    • G01S13/89Radar or analogous systems specially adapted for specific applications for mapping or imaging
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/03Details of HF subsystems specially adapted therefor, e.g. common to transmitter and receiver

Definitions

  • TITLE CAVITY MONITORING SYSTEM Field of the Invention
  • the present invention relates to underground mining and in particular, to the use
  • the invention has been developed primarily for use in monitoring underground voids or stopes formed as a result of removal of ore during mining and will be described hereinafter with reference to this application. However, it will be described hereinafter with reference to this application. However, it will be described hereinafter with reference to this application. However, it will be described hereinafter with reference to this application. However, it will be described hereinafter with reference to this application. However, it will be described hereinafter with reference to this application. However, it will be
  • the invention is not limited to this particular field of use and may be applied to other areas either above or below ground.
  • CAF is significantly more costly than crushed rock.
  • CMS cavity monitoring systems
  • narrow beam can be produced from a small aperture, which results in high angular
  • particulates in the air include dust, smoke and water droplets, or
  • the invention provides an underground cavity monitoring
  • the system including a radar having an operating wavelength in the millimetre band.
  • the wavelength is in the range of about 1mm to 1cm.
  • the radar uses a waveform with an operational frequency of between
  • the radar has uses a waveform with operational frequency of between
  • the radar has uses a waveform with operational frequency selected
  • the radar uses a waveform with an operational frequency of
  • the invention provides an underground cavity monitoring
  • a radar system including a radar system having: a transmitter for generating a modulated electromagnetic waveform; a transmit antenna for radiating the waveform into space toward a distant
  • a receive antenna for receiving the waveform reflected from the distant object; a receiver for measuring the amplitude of the reflected waveform
  • the invention provides a deployable antenna module for a
  • the antenna is transformable between a stored mode, where the
  • antenna is collapsed and disposed within a housing, and an operational mode, where
  • the antenna is deployed outside the housing.
  • the antenna is transformed between stored and operational modes by
  • Fig. 1 is a graph displaying signal frequency vs. signal absorption
  • Fig 2 is a schematic representation of a cavity monitoring system in operation
  • Figs 3 A and 3B are examples of images produced by a cavity monitoring system in accordance with the invention
  • Figs 4A - 4D are a sequence of schematic representations of a deployable antenna in accordance with the invention
  • Figs 5 A and 5B are representations of an alternative antenna deployment.
  • the selected wavelength of the emitted radiation is in the millimetre range. That is, waveforms having a wavelength from about 1cm to 1mm corresponding to a frequency range of about 30GHz to 300GHz.
  • the cavity monitoring system includes a time-of-flight electromagnetic radar
  • system having a transmitter for generating a modulated waveform of a predetermined wavelength; transmit and receive antennas for respectively radiating the waveform into space as a constrained beam electromagnetic signal and receiving the signal reflected from any distant objects; and a receiver, for detecting small values of radiation received by the receiver antenna and discriminating the time delay between
  • a control system collates the distance to the object with the horizontal and
  • the width of a radiated electromagnetic beam is a function of the ratio of its
  • Figure 1 is an example of a graph showing absorption against increasing frequency. It will be appreciated that the penetration of a waveform may be effected by airborne particles. Different frequencies will be affected differently by different particles. That is to say, an atmosphere containing one type of particle, for instance dust or water droplets of a certain size, will often exhibit a reduction in penetration at
  • Trace line 1 provides an indication of the penetration of an increasing frequency waveform through an atmosphere having a number of different types of airborne particles.
  • the peaks show frequencies with relative increased absorption characteristics while the troughs indicate frequencies with better penetration.
  • Trace line 2 provides an indication of the penetration of fog which is indicative of the atmosphere (smoke, dust, water droplets and other airborne particles) expected within the slope cavity.
  • frequencies of about 77 GHz and 94 GHz have been selected as being most suitable. However in other embodiments, other frequencies in
  • the millimetre band may be used, particularly those having frequencies of 35, 140 and
  • the CMS according to the invention can scan the stope surface and build up a contour map of the surface so that the position of the rock fill and the CAF can de determined (and controlled) in real time. This allows the appropriate fill ratios to be maintained and the CAF wall thickness
  • the angle of the reflecting surface indicates the lay of the fill. Referring to Figure 2, the CMS, 3 is positioned to survey
  • the stope 4 the CAF, 5 is substantially liquid and therefore tends to self level and lie
  • the magnitude of the reflected signal can be analyzed. Differences
  • FIGs 3 A and 3B An example of an image produced by a CMS is shown in Figs 3 A and 3B.
  • stope floor 7 and tunnels 8 and 9 can clearly be seen.
  • access to the stope may be limited. For instance, in some
  • the invention provides a
  • the antenna is an inflatable structure. As shown in Fig 4A,
  • the deflated antenna in stored mode is housed in a tubular antenna module 10
  • the module is
  • the antenna may be deployed by inflating a shaped bladder with air or another gas.
  • the antenna now in operational mode, can then be used to scan the stope as required, Fig 4C.
  • a compact powered cradle holds the antenna and is able to swivel on at least two axes to direct and accurately aim the antenna.
  • the bladder is deflated, thereby collapsing the antenna.
  • the collapsed antenna is then retracted into the housing and the module is withdrawn.
  • Figs. 5A and 5B show a collapsible antenna 10 including four hinged panel sections 13 which fold out for deployment. The folded antenna in the stored mode is shown in Fig 5 A whilst the
  • Fig. 5B deployed antenna in operational mode is shown in Fig. 5B.
  • the structure shown in Figs. 5A and 5B would be located within a protective housing.
  • the antenna is mounted for rotation on longitudinal and lateral axes. Specifically, the antenna portion, is able to yaw within cradle 14. The entire cradle can be longitudinally rotated around 15. It will be appreciated that the invention provides a cavity monitoring system
  • the invention represents practical and commercially significant

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Electromagnetism (AREA)
  • Mining & Mineral Resources (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

The invention provides an underground cavity monitoring system (CMS). The CMS uses a radar system operating in the millimetre wavelength band. The radar system includes a transmitter for generating a modulated electromagnetic waveform, transmit and receive antennas housed in and antenna module (10) for respectively radiating the waveform into space toward a distant object and receiving the waveform reflected from the distant object, and a receiver for measuring the amplitude of the reflected waveform and determining the time delay between the transmitting of the waveform and receiving the reflected waveform. A control system collates information received from the receiver and controls the antennas. The antenna module (10) is transformable between a stored mode, where the antenna is collapsed and an operational mode, where the antenna is unfurled and deployed.

Description

TITLE: CAVITY MONITORING SYSTEM Field of the Invention The present invention relates to underground mining and in particular, to the use
of underground radar systems.
Background of the Invention The invention has been developed primarily for use in monitoring underground voids or stopes formed as a result of removal of ore during mining and will be described hereinafter with reference to this application. However, it will be
appreciated that the invention is not limited to this particular field of use and may be applied to other areas either above or below ground. Once the mining process is completed, the stopes are filled with crushed rock and concrete to stabilize the surrounding rock. The concrete, is actually a cemented
aggregate fill, or CAF and is normally poured or pumped down through bore-holes drilled from the surface to strengthen the walls of the stope. The ratio of CAF to crushed rock is critical in providing a safe environment below the surface, however, because there is no method to accurately monitor the ratio, a large safety factor, and excess of CAF is used. This is uneconomical because
CAF is significantly more costly than crushed rock. A number of cavity monitoring systems (CMS) already exist that produce images of stopes. These present CMS's use a time-of-flight laser range finder integrated onto a motorised scanning head to scan the interior surface of the void from which an image can be constructed. Laser radar, generally operating in the infrared band, is used because a very
narrow beam can be produced from a small aperture, which results in high angular
resolution measurements. However this technology is limited in its application -
because laser wavelengths are strongly absorbed and scattered by suspended
particulates in the air. These particulates include dust, smoke and water droplets, or
combinations of these. This is particularly a problem during filling of stopes when an accurate real time
image of the stope is required to regulate the filling of the stope and ratio of CAF to
crushed rock. It is an object of the present invention to overcome or ameliorate at least one of
the disadvantages of the prior art, or to provide a useful alternative.
Disclosure of the Invention h a first aspect, the invention provides an underground cavity monitoring
system including a radar having an operating wavelength in the millimetre band. Preferably, the wavelength is in the range of about 1mm to 1cm.
Preferably, the radar uses a waveform with an operational frequency of between
about 30 GHz and 300 GHz.
Preferably, the radar has uses a waveform with operational frequency of between
35 GHz and 225 GHz. Preferably, the radar has uses a waveform with operational frequency selected
form the frequencies of about 35 GHz, 77GHz, 94 GHz, 140 GHz and 225 GHz.
More preferably, the radar uses a waveform with an operational frequency of
77 GHz or approximately 94 GHz which corresponds to an atmospheric window.. In a second aspect the invention provides an underground cavity monitoring
system including a radar system having: a transmitter for generating a modulated electromagnetic waveform; a transmit antenna for radiating the waveform into space toward a distant
object; a receive antenna for receiving the waveform reflected from the distant object; a receiver for measuring the amplitude of the reflected waveform and
determining the time delay between the transmitting of the waveform and receiving
the reflected waveform; and a control system for collating information received from the receiver and
controlling the antennas.
In another aspect, the invention provides a deployable antenna module for a
cavity monitoring radar system.
Preferably, the antenna is transformable between a stored mode, where the
antenna is collapsed and disposed within a housing, and an operational mode, where
the antenna is deployed outside the housing.
Preferably the antenna is transformed between stored and operational modes by
respectively deflating or inflating a bladder.
The selection of the operating frequency and the size of the deployed antenna
offer a good compromise between atmospheric attenuation and the angular resolution
required to produce clear images of the interior of the cavity.
Brief Description of the Drawings
A preferred embodiment of the invention will now be described, by way of
example only, with reference to the accompanying drawings, in which: Fig. 1 is a graph displaying signal frequency vs. signal absorption;
Fig 2 is a schematic representation of a cavity monitoring system in operation; Figs 3 A and 3B are examples of images produced by a cavity monitoring system in accordance with the invention; Figs 4A - 4D are a sequence of schematic representations of a deployable antenna in accordance with the invention; and Figs 5 A and 5B are representations of an alternative antenna deployment.
Preferred Embodiments of the Invention The invention provides an underground cavity monitoring system including an electro-magnetic radar utilising an operating wavelength selected to provide an
increased penetration of smoke, dust, water droplets and other airborne particles while still maintaining reasonably good angular resolution from a small antenna aperture. The selected wavelength of the emitted radiation is in the millimetre range. That is, waveforms having a wavelength from about 1cm to 1mm corresponding to a frequency range of about 30GHz to 300GHz. The cavity monitoring system includes a time-of-flight electromagnetic radar
system having a transmitter for generating a modulated waveform of a predetermined wavelength; transmit and receive antennas for respectively radiating the waveform into space as a constrained beam electromagnetic signal and receiving the signal reflected from any distant objects; and a receiver, for detecting small values of radiation received by the receiver antenna and discriminating the time delay between
the radiated and returned signal to calculate the distance of the object from the radar. The magnitude of the reflected signal is also important and used to provide an indication of the nature of the reflecting surface. A control system collates the distance to the object with the horizontal and
vertical rotational direction to provide a relative coordinate location of the object from
the system, hi this way, by scanning the surface of the stope, a detailed picture of its
surface can be attained. This is presented in a plot extractor or graphical interface. When selecting the appropriate frequency it is important to take into account the
penetration of the waveform through the medium it travels. Generally, absorption
increases with increasing waveform frequency, thus the lower the frequency the better
penetration.
Higher frequency systems operating in the infrared or visible bands do not
penetrate the vapour and airborne particles particularly well and so cannot be used to
perform this monitoring function at all.
Lower frequency systems operating in the microwave band exhibit good
penetration characteristics, but do not allow for a sufficiently narrow beam to give the
required angular resolution to generate a contour map of the surface. This is because
the width of a radiated electromagnetic beam is a function of the ratio of its
wavelength and the antenna aperture (disk diameter). In many applications the size of
the antenna is not an important consideration. However, in this application, operating
in confined spaces underground, it is particularly preferred to have an aperture of
under 300mm. Whilst still producing a beam width of less than 1°. It is not possible
to obtain the same narrow beam in the millimetre wave band as is possible in the
infrared band without resorting to a large aperture.
Accordingly, a compromise must be reached between the dust penetration
capability, the required angular resolution and the size of the aperture that can be
accommodated for a specific task. Figure 1 is an example of a graph showing absorption against increasing frequency. It will be appreciated that the penetration of a waveform may be effected by airborne particles. Different frequencies will be affected differently by different particles. That is to say, an atmosphere containing one type of particle, for instance dust or water droplets of a certain size, will often exhibit a reduction in penetration at
a particular, confined range of frequencies. Trace line 1 provides an indication of the penetration of an increasing frequency waveform through an atmosphere having a number of different types of airborne particles. The peaks show frequencies with relative increased absorption characteristics while the troughs indicate frequencies with better penetration.
Trace line 2 provides an indication of the penetration of fog which is indicative of the atmosphere (smoke, dust, water droplets and other airborne particles) expected within the slope cavity. By studying these peaks and troughs, waveform frequencies are selected which
provide a reduced tendency to be absorbed. Specific frequencies of around 35, 77, 94, 140 and 225 GHz have been identified as providing good, relative penetration in clear
air and also through smoke, dust and water particles. In this embodiment, frequencies of about 77 GHz and 94 GHz have been selected as being most suitable. However in other embodiments, other frequencies in
the millimetre band may be used, particularly those having frequencies of 35, 140 and
225 GHz. Advantageously, using these frequencies the CMS according to the invention can scan the stope surface and build up a contour map of the surface so that the position of the rock fill and the CAF can de determined (and controlled) in real time. This allows the appropriate fill ratios to be maintained and the CAF wall thickness
reduced. This may be accomplished in two ways. The angle of the reflecting surface indicates the lay of the fill. Referring to Figure 2, the CMS, 3 is positioned to survey
the stope 4, the CAF, 5 is substantially liquid and therefore tends to self level and lie
generally horizontally whilst the crushed rock 6 will tend to heap in a pile under the
point at which it enters the stope. Thus by analyzing the shape of the bottom floor of the stope as it is filled, the interface between the CAF and crushed rock can be
estimated as the stope is filled.
In addition, the magnitude of the reflected signal can be analyzed. Differences
in strength of the signal can be used to indicate the different surfaces of the crushed
rock pile and CAF fill.
An example of an image produced by a CMS is shown in Figs 3 A and 3B.
Normally a colour representation would be presented to the operator but in these
monochrome figures the stope floor 7 and tunnels 8 and 9 can clearly be seen. In certain applications, access to the stope may be limited. For instance, in some
cases access to the cavity is available only via a borehole or small passageway. In
such applications the antenna required for the above millimeter band CMS will not fit
through the passageway. Therefore in a second aspect, the invention provides a
deployable antenna for a cavity monitoring system. In this embodiment, the antenna is an inflatable structure. As shown in Fig 4A,
the deflated antenna in stored mode is housed in a tubular antenna module 10
dimensioned to be inserted into a bore hole 11 of reduced diameter. The module is
connected by an umbilical cord that is used to power and control the antenna. Other systems such as the receiver, transmitter and control system may be disposed within the module housing or located remotely. As seen in Fig 4B, once the module clears the borehole and enters the cavity, the antenna may be deployed by inflating a shaped bladder with air or another gas. The antenna, now in operational mode, can then be used to scan the stope as required, Fig 4C. A compact powered cradle holds the antenna and is able to swivel on at least two axes to direct and accurately aim the antenna. Once scanning has been completed the bladder is deflated, thereby collapsing the antenna. The collapsed antenna is then retracted into the housing and the module is withdrawn. This can be seen in Fig 4D. hi other embodiments the inflatable antenna may be replaced with a ribbed, folding or otherwise collapsible structure. For instance, Figs. 5A and 5B show a collapsible antenna 10 including four hinged panel sections 13 which fold out for deployment. The folded antenna in the stored mode is shown in Fig 5 A whilst the
deployed antenna in operational mode is shown in Fig. 5B. It will be appreciated that the structure shown in Figs. 5A and 5B would be located within a protective housing. As can be seen, the antenna is mounted for rotation on longitudinal and lateral axes. Specifically, the antenna portion, is able to yaw within cradle 14. The entire cradle can be longitudinally rotated around 15. It will be appreciated that the invention provides a cavity monitoring system
which is able to present a real time image of the surface of a stope through an atmosphere containing suspended particulates such as smoke, dust and water droplets. In all these respects, the invention represents practical and commercially significant
improvement over the prior art. The present invention has been described herein by way of example only. Skilled workers in this field will readily recognise many variations and modifications which do not depart from the spirit and scope of the broad inventive concept.

Claims

1. An underground cavity monitoring system including a radar having an
operating wavelength in the millimetre band.
2. A system according to claim 1 wherein, the wavelength is in the range of about
10mm to 1cm.
3. A system according to claim 1 or 2 wherein, the radar uses a waveform with an
operational frequency of between about 30 GHz and 300 GHz.
4. A system according to claim 3 wherein, the radar has uses a waveform with
operational frequency of between 35 GHz and 225 GHz.
5. A system according to claim 4 wherein, the radar has uses a waveform with
operational frequency selected form the frequencies of about 35 GHz, 77GHz, 94
GHz, 140 GHz and 225 GHz.
6. A system according to claim 5 wherein, the radar uses a waveform with an
operational frequency of about 77 GHz.
7. A system according to claim 5 wherein, the radar uses a waveform with an
operational frequency of approximately 94 GHz.
8. A system according to any one of the preceding claim, including a radar system
having: a transmitter for generating a modulated electromagnetic waveform; a transmit antenna for radiating the waveform into space toward a distant
object; a receive antenna for receiving the waveform reflected from the distant object; a receiver for measuring the amplitude of the reflected waveform and
determining the time delay between the transmitting of the waveform and receiving
the reflected waveform; and a control system for collating information received from the receiver and
controlling the antennas.
9. An underground cavity monitoring system including a radar system having: a transmitter for generating a modulated electromagnetic waveform; a transmit antenna for radiating the waveform into space toward a distant
object; a receive antemia for receiving the waveform reflected from the distant object; a receiver for measuring the amplitude of the reflected waveform and
determining the time delay between the transmitting of the waveform and receiving
the reflected waveform; and a control system for collating information received from the receiver and
controlling the antennas.
10. A deployable antenna module for a cavity monitoring radar system.
11. An antenna according to claim 10 wherein the antenna is transformable
between a stored mode, where the antenna is collapsed and an operational mode,
where the antenna is unfurled and deployed.
12. An antenna according to claim 11 wherein the antenna is stored within a
housing, and deployed outside the housing.
13. An antenna according to claim 11 or 12 wherein the antenna is transformed between stored and operational modes by respectively inflating or inflating a bladder.
14. An antenna according to claim 11 or 12 wherein the antenna includes a plurality of hinged panel sections which are moveable between a closed position in the stored mode, and an open position in the operational mode.
PCT/AU2004/001530 2003-11-04 2004-11-04 Cavity monitoring system WO2005045466A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU2003906084 2003-11-04
AU2003906084A AU2003906084A0 (en) 2003-11-04 Cavity monitoring system

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WO2005045466A1 true WO2005045466A1 (en) 2005-05-19

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4380013A (en) * 1981-02-17 1983-04-12 General Dynamics Corp./Convair Division Expandable panel and truss system/antenna/solar panel
US4814768A (en) * 1987-09-28 1989-03-21 The United States Of America As Represented By The United States Department Of Energy Downhole pulse radar
JPH09304517A (en) * 1996-05-10 1997-11-28 Mitsubishi Electric Corp Millimeter-wave imaging radar
US6373449B1 (en) * 1999-09-21 2002-04-16 The Johns Hopkins University Hybrid inflatable antenna
JP2003050274A (en) * 2001-08-06 2003-02-21 Junichi Takeno Device for visualizing simultaneously three-dimensional space and object emitting characteristic energy as stereoscopic vision in environment having poor visibility
CN1405330A (en) * 2001-08-13 2003-03-26 宝山钢铁股份有限公司 Blast furnace top full-charge-level millimeter-wave three-dimensional imaging instrument
WO2003041117A2 (en) * 2001-11-09 2003-05-15 Robert Bosch Gmbh Integrated semiconductor component for conducting high-frequency measurements and the use thereof

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4380013A (en) * 1981-02-17 1983-04-12 General Dynamics Corp./Convair Division Expandable panel and truss system/antenna/solar panel
US4814768A (en) * 1987-09-28 1989-03-21 The United States Of America As Represented By The United States Department Of Energy Downhole pulse radar
JPH09304517A (en) * 1996-05-10 1997-11-28 Mitsubishi Electric Corp Millimeter-wave imaging radar
US6373449B1 (en) * 1999-09-21 2002-04-16 The Johns Hopkins University Hybrid inflatable antenna
JP2003050274A (en) * 2001-08-06 2003-02-21 Junichi Takeno Device for visualizing simultaneously three-dimensional space and object emitting characteristic energy as stereoscopic vision in environment having poor visibility
CN1405330A (en) * 2001-08-13 2003-03-26 宝山钢铁股份有限公司 Blast furnace top full-charge-level millimeter-wave three-dimensional imaging instrument
WO2003041117A2 (en) * 2001-11-09 2003-05-15 Robert Bosch Gmbh Integrated semiconductor component for conducting high-frequency measurements and the use thereof

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Title
DATABASE WPI Week 199807, Derwent World Patents Index; Class W06, AN 1998-066978 *
DATABASE WPI Week 200323, Derwent World Patents Index; Class W06, AN 2003-234699 *
DATABASE WPI Week 200346, Derwent World Patents Index; Class M24, AN 2003-483258 *

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