Language selection

Search

Patent 2104180 Summary

Third-party information liability

Some of the information on this Web page has been provided by external sources. The Government of Canada is not responsible for the accuracy, reliability or currency of the information supplied by external sources. Users wishing to rely upon this information should consult directly with the source of the information. Content provided by external sources is not subject to official languages, privacy and accessibility requirements.

Claims and Abstract availability

Any discrepancies in the text and image of the Claims and Abstract are due to differing posting times. Text of the Claims and Abstract are posted:

  • At the time the application is open to public inspection;
  • At the time of issue of the patent (grant).
(12) Patent: (11) CA 2104180
(54) English Title: LAPLACE GRAVITY GRADIOMETER
(54) French Title: GRADIOMETRE DE PESANTEUR LAPLACE
Status: Term Expired - Post Grant Beyond Limit
Bibliographic Data
(51) International Patent Classification (IPC):
  • G01V 07/02 (2006.01)
  • G01V 07/00 (2006.01)
(72) Inventors :
  • PANENKA, JERRY R. (Canada)
(73) Owners :
  • CANAGRAV RESEARCH LTD.
(71) Applicants :
  • CANAGRAV RESEARCH LTD. (Canada)
(74) Agent: GOWLING WLG (CANADA) LLP
(74) Associate agent:
(45) Issued: 1999-08-10
(22) Filed Date: 1993-08-16
(41) Open to Public Inspection: 1995-02-17
Examination requested: 1993-08-16
Availability of licence: N/A
Dedicated to the Public: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): No

(30) Application Priority Data: None

Abstracts

English Abstract


A gravity gradiometer which derives the vertical component T zz of the gravity
gradient tensor out of the two measured horizontal components T xx and T yy
based on
Laplace equation: T zz = - (T xx + T yy) comprises a single disc, and two
pairs of
radially-oriented horizontal axis accelerometers oppositely-mounted on such
disc
along respective X and Y axes. Each pair provides, respectively, T xx T x1 + T
X2 and
T yy=T y1, + T y2 where T X1 and T X2 are the respective outputs of the X axis
accelerometers and T y1, and T y2 are the respective outputs of the Y axis
accelerometers. The gravity gradiometer provides all five independent
components of the gravity gradient tensor based on the above Laplace equation
and tensor symmetry as follows: One of the above pairs of horizontal axis
accelerometers further comprises tangentially oriented horizontal
accelerometers capable of providing the T xy component of the gravity gradient
tensor, and an accelerometer module consisting of two horizontal
accelerometers aligned with the radially and tangentially oriented combination
is mounted at a location on the Z axis of the disc above or below the disc to
provide the T zx and T zy, components by substracting the values of T x and T
y ,
respectively, at that location from average values of T x and T y at the disc
plane.


Claims

Note: Claims are shown in the official language in which they were submitted.


CLAIMS
1. A gravity gradiometer for obtaining the vertical component T zz of the
gravity
gradient tensor out of the two horizontal components T xx and T yy based on
Laplace
equation T zz = - (T xx + T yy) comprising:
a. a single disc; and
b. two pairs of radially-oriented horizontal axis accelerometers oppositely-
mounted
on said disc along respective X and Y axes, each pair providing, respectively,
T xx = T x1 - T x2 and T yy = T y1 - T y2 where T x1 and T x2 are the
respective outputs of the X
axis accelerometers and T y1 and T y2 are the respective outputs of the Y axis
accelerometers.
2. A gravity gradiometer for obtaining all five independent components of the
gravity gradient tensor based on the Laplace equation T zz = - (T xx + T yy )
and tensor
symmetry, comprising:
a. a single disc; and
b. two pairs of radially-oriented horizontal axis accelerometers oppositely-
mounted
on said disc along respective X and Y axes, each pair providing respectively,
T xx = T x1 - T x2 and T yy = T y1 - T y2 where T x1, and T x2 are the
respective outputs of the X
axis accelerometers and T y1 and T y2 are the respective outputs of the Y axis
accelerometers;
wherein one of the pairs of horizontal axis accelerometers further comprises
tangentially
oriented horizontal accelerometers to provide by substraction the T xy
component of the
gravity gradient tensor, and further comprising an accelerometer module
consisting of
two horizontal accelerometers aligned with the radially and tangentially
oriented
combination mounted at a location on the Z axis of the disc above or below the
disc to
provide the T zx and T zy components by subtracting the values of T x and T y,
respectively,
at said location from average values of T x and T y at the disc plane.
3. A gravity gradiometer as defined in claim 1 or 2, wherein the disc is
rotatable
around the Z axis.

Description

Note: Descriptions are shown in the official language in which they were submitted.


CA 02104180 1998-OS-11
-2-
LAPLACE GRAVITY GRADIOMETER
This invention relates to a gravity gradiometer which obtains
components of the gravity gradient tensor using the Laplace equation and
tensor symmetry with horizontal accelerometers only.
Background of the invention
Existing commercial gravity gradiometers depend on measurement of
gravity gradients along axes inclined 45 degrees to the vertical (umbrella
configuration). Examples of these are the Bell gravity gradient survey system
GGSS of Bell-Textron of Buffalo, N.Y. which operates at room temperature,
and an experimental University of Maryland gradiometer which requires
cryogenic temperatures.
Gravity gradients at 45 degrees to the vertical are more difficult to
measure since compensation for a large gravity component (G cos 45 ~) is
required. This involves springs, which are subject to non-linearities,
hysteresis, fatigue, tares, inter-atomic slippage, etc. The above Bell GGSS
model uses three rotating discs, each populated with four tangentially-
oriented
single axis pendulous accelerometers.
Furthermore, gradiometer signals are measured in a relatively strong
aircraft motion acceleration noise field, with the vertical components
typically
several times higher than the horizontal components.
Statement of the invention
Applicant has found that there is no need to measure anomalous
gradients on a background of strong aircraft sub-vertical gravity
accelerations
directly, since the full tensor can be derived from horizontal gradients using
Laplace equation and the tensor symmetry.

CA 02104180 1998-OS-11
-3-
Horizontal gradients can be measured more simply than gradients in the
vertical directions by such means as pendulum - based accelerometers such as
Bell VII or XI models of Bell-Textron of Buffalo, N.Y.). A pendulum is
stabilized by the force of gravity, and is, therefore, a reliable, sensitive
and
frequently used inertial element.
A first embodiment of the gravity gradiometer in accordance with the
present invention comprises two pairs of radially-oriented horizontal axis
accelerometers oppositely-mounted on a support , such as a single disc along
respective X and Y axes, each pair providing, respectively, TXX TXI + Txz and
Tri Ty, + Ty2 where Tx, and Tx2 are the outputs of the X axis accelerometers
and TY, and Ty2 are the outputs of the Y axis accelerometers.
A second embodiment of the gravity gradiometer in accordance with the
present invention provides all five independent components of the gravity
gradient tensor using the Laplace equation and tensor symmetry. In this
embodiment, one of the two pairs of horizontal axis accelerometers further
comprises tangentially oriented horizontal accelerometers providing the TXy
component of the gravity gradient tensor. In addition, an accelerometer module
consisting of two horizontal accelerometers aligned with the above radial and
tangential combination is mounted at a location on the Z axis of the disc
above
and/or below the disc to provide the T~ and TZY components by subtracting the
values of TX and Ty at that location respectively, from average values of TX
and
TY at the disc plane. Both embodiments include signal processing means for
combining the outputs of the accelerometers in order to derive corresponding
gravity gradients.
Brief Description of the Drawings
The invention will now be disclosed, by way of example, with reference
to the accompanying drawings in which:
Figure 1 illustrates an embodiment of a gravity gradiometer which
provides the vertical component TZZ of the gravity gradient from measurement

' CA 02104180 1998-OS-11
-4-
of horizontal components Txx and TYY and
Figure 2 illustrates an embodiment of a gravity gradiometer providing
all five independent components of the gravity gradient tensor from
measurement of horizontal components.
Detailed Description of Preferred Embodiments
Before proceeding with the description of the preferred embodiments,
let us provide the following well known definitions:
Basic Formulas
Gravity Gradient is a second derivative of Gravity Potential T. It is
represented
by the second-order nine-component symmetric tensor T;~.
TXX TXY TXZ
TiJ TYx TYY TYz
TZX TZY TZZ
On and above the earth surface the value of its in-line
(diagonal) components conforms to a well known Laplace equation:
TXX+TYY+T~=0
from which follows:
Tzz = - (Txx + TYY)
Thus we can obtain vertical component out of the two horizontal components.
By virtue of gradient tensor symmetry
T;~ = T~;
it is clear that only five of the nine components are independent (which is a
well known theorem). Therefore, in order to describe fully the tensor it is
sufficient to measure two in-line (diagonal) components and three independent
cross-components. None of these has to be a vertical component.
Sensor Geometry
In a first embodiment of the invention illustrated in Figure 1, the vertical
gravity gradient TZZ is obtained through Laplace equation TZZ = - (Txx + TYY)
from two horizontal gradients Txx and TYY combining the outputs of two pairs 1

CA 02104180 1998-OS-11
-S-
and 2 of radially oriented horizontal axis accelerometers mounted on a
horizontal disc 6 along X and Y axes, respectively. Accelerometer pairs 1 and
2
provide T,~ and Tyy.
In a second embodiment of the invention illustrated in Figure 2, a11 five
independent components of the gravity gradient tensor can be obtained from
horizontal gradients based on Laplace equation and tensor symmetry. In this
embodiment, one of the pairs of radially-oriented horizontal accelerometers
(pair 1) is replaced with a pair 3 of radially and tangentially oriented
horizontal
accelerometers 3 providing the TXy component of the gravity gradient sensor.
In addition, an accelerometer module 4 consisting of two horizontal
accelerometers aligned with the above radial and tangential combination is
mounted at a location on the Z axis above or below the disc to provide the TZX
and TZY components by subtracting the values of TX and Ty respectively, at
that
location from average values of TX and TY at the disc plane.
As noted previously, both embodiments include signal processing
means for combining the outputs of the several accelerometers in order to
derive corresponding gravity gradients. The signal processing means, as those
skilled in this art will appreciate, may be of a standard off the-shelf
variety.
The accelerometer disc may be rotated around the vertical axis in order
to narrow the signal bandwidth and reduce noise thus increasing
signal-to-noise ratio, which is a standard industry practice, as for example
in
Bell GGSS gravity gradiometer.
The second embodiment can obtain the full tensor using a single
stationary or rotating horizontal disc configuration rather than three discs
in a
45 degree umbrella orientation such as employed in Bell GGSS, or three pairs
of spring accelerometers in the same configuration like in the above mentioned
University of Maryland cryogenic gradiometer. This simplification results in
lower noise as well as a decrease in complexity and cost.

CA 02104180 1998-OS-11
-6-
Although the invention has been disclosed, by way of example, with
reference to preferred embodiments, it is to be understood that other
alternatives are also envisaged within the scope of the following claims:

Representative Drawing
A single figure which represents the drawing illustrating the invention.
Administrative Status

2024-08-01:As part of the Next Generation Patents (NGP) transition, the Canadian Patents Database (CPD) now contains a more detailed Event History, which replicates the Event Log of our new back-office solution.

Please note that "Inactive:" events refers to events no longer in use in our new back-office solution.

For a clearer understanding of the status of the application/patent presented on this page, the site Disclaimer , as well as the definitions for Patent , Event History , Maintenance Fee  and Payment History  should be consulted.

Event History

Description Date
Inactive: Expired (new Act pat) 2013-08-16
Small Entity Declaration Determined Compliant 2007-08-16
Inactive: IPC from MCD 2006-03-11
Inactive: Entity size changed 2000-08-21
Grant by Issuance 1999-08-10
Inactive: Cover page published 1999-08-09
Notice of Allowance is Issued 1999-06-07
Inactive: Approved for allowance (AFA) 1999-05-17
Letter Sent 1999-03-08
Reinstatement Request Received 1999-02-10
Reinstatement Requirements Deemed Compliant for All Abandonment Reasons 1999-02-10
Amendment Received - Voluntary Amendment 1999-02-10
Inactive: Abandoned - No reply to s.30(2) Rules requisition 1998-11-10
Inactive: Adhoc Request Documented 1998-11-06
Inactive: S.30(2) Rules - Examiner requisition 1998-07-10
Letter Sent 1998-06-25
Withdraw from Allowance 1998-06-25
Inactive: Application prosecuted on TS as of Log entry date 1998-06-25
Inactive: Reversal of dead status 1998-06-18
Pre-grant 1998-05-11
Amendment After Allowance (AAA) Received 1998-05-11
Reinstatement Requirements Deemed Compliant for All Abandonment Reasons 1998-05-11
Reinstatement Request Received 1998-05-11
Inactive: Final fee received 1998-05-11
Final Fee Paid and Application Reinstated 1998-05-11
Inactive: Status info is complete as of Log entry date 1998-04-16
Deemed Abandoned - Failure to Respond to Maintenance Fee Notice 1997-08-18
Inactive: Dead - Final fee not paid 1997-07-21
Application Published (Open to Public Inspection) 1995-02-17
Request for Examination Requirements Determined Compliant 1993-08-16
All Requirements for Examination Determined Compliant 1993-08-16

Abandonment History

Abandonment Date Reason Reinstatement Date
1999-02-10
1998-05-11
1997-08-18

Maintenance Fee

The last payment was received on 1998-08-13

Note : If the full payment has not been received on or before the date indicated, a further fee may be required which may be one of the following

  • the reinstatement fee;
  • the late payment fee; or
  • additional fee to reverse deemed expiry.

Patent fees are adjusted on the 1st of January every year. The amounts above are the current amounts if received by December 31 of the current year.
Please refer to the CIPO Patent Fees web page to see all current fee amounts.

Fee History

Fee Type Anniversary Year Due Date Paid Date
Reinstatement 1998-05-11
MF (application, 4th anniv.) - standard 04 1997-08-18 1998-05-11
Final fee - standard 1998-05-11
MF (application, 5th anniv.) - standard 05 1998-08-17 1998-08-13
Reinstatement 1999-02-10
MF (patent, 6th anniv.) - standard 1999-08-17 1999-08-12
MF (patent, 7th anniv.) - small 2000-08-16 2000-08-11
MF (patent, 8th anniv.) - small 2001-08-16 2001-08-16
MF (patent, 9th anniv.) - small 2002-08-16 2002-08-08
MF (patent, 10th anniv.) - small 2003-08-18 2003-08-14
MF (patent, 11th anniv.) - small 2004-08-16 2004-08-16
MF (patent, 12th anniv.) - small 2005-08-16 2005-08-11
MF (patent, 13th anniv.) - small 2006-08-16 2006-08-15
MF (patent, 14th anniv.) - small 2007-08-16 2007-08-16
MF (patent, 15th anniv.) - small 2008-08-18 2008-08-15
MF (patent, 16th anniv.) - small 2009-08-17 2009-08-17
MF (patent, 17th anniv.) - small 2010-08-16 2010-08-11
MF (patent, 18th anniv.) - small 2011-08-16 2011-08-15
MF (patent, 19th anniv.) - small 2012-08-16 2012-08-13
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
CANAGRAV RESEARCH LTD.
Past Owners on Record
JERRY R. PANENKA
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
Documents

To view selected files, please enter reCAPTCHA code :



To view images, click a link in the Document Description column. To download the documents, select one or more checkboxes in the first column and then click the "Download Selected in PDF format (Zip Archive)" or the "Download Selected as Single PDF" button.

List of published and non-published patent-specific documents on the CPD .

If you have any difficulty accessing content, you can call the Client Service Centre at 1-866-997-1936 or send them an e-mail at CIPO Client Service Centre.


Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Claims 1999-02-09 1 40
Representative drawing 1999-08-01 1 6
Abstract 1998-05-10 1 33
Description 1998-05-10 5 181
Drawings 1998-11-05 1 22
Abstract 1998-05-10 1 33
Claims 1998-05-10 2 45
Representative drawing 1998-05-10 1 4
Courtesy - Abandonment Letter (Maintenance Fee) 1997-09-30 1 188
Notice of Reinstatement 1998-06-24 1 172
Courtesy - Abandonment Letter (R30(2)) 1999-01-04 1 171
Notice of Reinstatement 1999-03-07 1 173
Commissioner's Notice - Application Found Allowable 1999-06-06 1 165
Fees 2003-08-13 1 33
Correspondence 1999-02-09 2 76
Correspondence 1998-05-10 2 59
Fees 1999-08-11 1 28
Fees 2001-08-15 1 25
Fees 2002-08-07 1 30
Fees 1998-08-12 1 36
Fees 1998-05-10 2 57
Fees 2000-08-10 1 30
Fees 2004-08-15 1 36
Fees 2005-08-10 1 28
Fees 2006-08-14 1 29
Fees 2007-08-15 1 33
Correspondence 2007-08-15 1 40
Fees 2008-08-14 1 30
Fees 2009-08-16 1 31
Fees 2010-08-10 1 35
Fees 1995-07-16 1 44
Fees 1996-08-05 1 31