AU7213701A - Apparatus for reducing rotation of an article - Google Patents

Description

AUSTRALIA

Patents Act 1990 COMPLETE SPECIFICATION STANDARD PATENT Applicant(s): 0* THE BROKEN HILL PROPRIETARY COMPANY LIMITED A.C.N. 004 028 077 Invention Title: APPARATUS FOR REDUCING ROTATION OF AN ARTICLE The following statement is a full description of this invention, including the best method of performing it known to me/us: 2 APPARATUS FOR REDUCING ROTATION OF AN ARTICLE This invention relates to an apparatus for reducing rotation of an article and, in particular, but not exclusively, to an apparatus for reducing rotation of a super conducting quantum interference device (SQUID) in the earth's magnetic field. The invention has particular application to airborne transient electromagnetic mineral prospecting. However, it should be understood that the invention has application to environments other than transient electromagnetic mineral prospecting and to payloads other than SQUID magnetometers and, indeed, could be used in many environments in which it is desired to reduce rotational movement of a payload at a particular frequency.

Transient electromagnetic mineral prospecting involves subjecting the ground to a large pulsating magnetic field which is produced by an excitation coil usually mounted on 20 an aircraft. A current is periodically supplied to the aircraft mounted coil for producing the magnetic field.

During intervals in which current flows, the ground is magnetised by the magnetic field and during intervals in 25 which no current flows, the ground maintains a residual 25 magnetism which eventually decays. The decay of the residual magnetism is related to the electrical conductivity of the ground and the decaying magnetic field can thereby provide an indication of minerals below the earth's surface.

In order to detect the decaying magnetic field, the aircraft tows a bird (which is generally in the form of a hollow tear-shaped container). The bird supports a SQUID magnetometer which measures the decaying magnetic field and thereby provides an indication of the material below the surface of the earth in the area being surveyed.

3 The decaying magnetic field which is of interest is many magnitudes smaller than the magnetic field created by the excitation coil. The field created by the excitation coil is also several magnitudes smaller than the earth's magnetic field at the location of the SQUID magnetometer.

Since the decaying magnetic field is usually detected during periods when the current in the excitation coil is not flowing, the decaying magnetic field can be easily distinguished from the magnetic field produced by the aircraft mounted coil.

In order to distinguish the decaying field from the earth's magnetic field, electronic circuitry associated with the SQUID magnetometer compensates for apparent changes in the earth's magnetic field. Linear movement of the SQUID magnetometer through the earth's magnetic field will not interfere to the same extent with monitoring of the decaying field which is of interest. However, since the 4* SQUID magnetometer in the bird is towed by the aircraft, 20 the bird and therefore the SQUID magnetometer is subject to considerable buffeting and movement. Any rotation of the SQUID magnetometer in the earth's magnetic field will result in a signal which can be confused with the signal of *oooo interest which relates to the decaying field.

The object of the present invention is to provide an apparatus which reduces rotation of an article, such as a SQUID magnetometer relative to a particular datum such as the earth's magnetic field.

The invention may be said to reside in an apparatus for reducing rotation of an article, at a desired frequency including: an article support member for supporting the article; a plurality of strings coupled to the article support member at one end; 4 a plurality of spring members respectively coupled to each of the plurality of strings at the other end of the strings; and a holding means to which the plurality of spring members is coupled.

Preferably the article support member comprises a spherical support member having an inner shell and an outer shell defining a cavity for receiving a damping liquid.

Preferably the holding means comprises a bird for towing by an aircraft.

Preferably each of the spring members includes a damping means and preferably the damping means comprises resilient pads or air bellows.

Preferably the article is a dewar for containing a SQUID magnetometer.

Preferably the anti-rotation means comprises baffle means in the cavity and a plurality of spring members coupled to the casing and a plurality of strings respectively .e connected to the spring members and to the support member for suspending the support member within the casing.

Preferred embodiments of the invention will be described, by way of example, with reference to the accompanying drawings in which: Figure 1 is a schematic view of an apparatus embodying the invention; Figure 2 is a view of the apparatus in further detail; Figure 3 is a view along the line A-A of Figure 2; Figure 4 is a view in schematic form showing further detail of a bird according to the preferred 5 embodiment of the invention; Figure 5 is a schematic view showing one form of damping according to one embodiment of the invention; Figure 6 is a view showing a further form of damping according to another embodiment of the invention; Figure 7 is a view showing a baffle plate used in the preferred embodiment of the invention; Figures 8, 9, 10 and 11 are schematic views showing various suspension arrangements; and Figures 12 and 13 are diagrams illustrating operation of the apparatus according to the preferred embodiment of the invention.

The preferred embodiment of the invention will be described with reference to the support of a SQUID magnetometer for airborne transient electromagnetic prospecting in which the apparatus according to the preferred embodiment of the invention reduces the amount of angular motion which the SQUID magnetometer would otherwise suffer as it is towed 20 through the air.

S.i Figure 1 is a schematic representation of the apparatus according to the preferred embodiment of the invention. A ooe bird 10 of generally known structure is intended to be 25 towed behind or supported under an aircraft (not shown) to move a SQUID magnetometer (not shown) over an area to be •surveyed. The bird 10 defines an internal space 12 in which is mounted a plurality of leaf springs 14. The leaf springs 14 are mounted in cantilever fashion so that one 30 end 14a is attached to a suitable coupling mechanism 16 .o.o.i S" attached to the internal surface of the bird 10. Each of the springs 14 is provided with a damper 18 for damping movement of the respective spring 14.

A support member 20 in the form of a hollow spherical ball is arranged within the space 12. The support member 20 is generally spherical in configuration having eight holes 22 6 (of which four are shown). A plurality of springs 24 have one end connected to a respective spring 14 and the other end to an anchoring point within the spherical support member Figures 2 and 3 show the apparatus in more detail. As shown in Figure 2, the bird 10 is of teardrop configuration and the spherical mounting member 20 is located at the large diameter end of the bird As is best shown in Figure 3, the spherical support member has an outer shell 21 and an inner shell 23 which define a cavity 25 therebetween. A damping liquid such as water fills the cavity 25 completely so that there is no air space or bubbles within the cavity 25. The support member may also have a device for removing air bubbles, such as a suction device (not shown), so that any bubbles which may form in the cavity 25 from dissolved air in the water after S: sealing of the support member can be removed. The 20 spherical ball member 20 also supports an internal frame structure 27 for providing some rigidity to the spherical

C.

S" support member 20 and also providing a support for a dewar (not shown in Figures 2 and 3) within which the SQUID •magnetometer is located.

Figure 5 is a schematic broken away view of the bird showing in schematic form the frame structure 27 and also a dewar 30 and counterweight 32 which can be supported by the frame 27 within the spherical support member 20. The dewar 30 typically contains a cryogenic liquid such as liquid S" nitrogen, liquid helium or the like in which the SQUID magnetometer is immersed for maintaining the SQUID magnetometer at the correct operating temperature. The counterweight 32 simply balances the weight of the dewar within the spherical support structure The bird 10 may include a high drag tail 34 at one end and 7 a coupling schematically shown at 36 for connecting the bird to a tether for towing behind an aircraft (not shown).

Figure 6 shows one embodiment of damping 18 associated with each spring 14. In the embodiment of Figure 6, the damping 18 comprises a plurality of resilient pads which are tied together by a line 38 so that when the spring 16 is flexed by movement of the spherical support member 20, the resilient pads 18 are compressed by the line 38 against a back plate 38a so as to apply a restoring force to dampen movement of the spring 16.

In the embodiment of Figure 7, the damping comprises an air bellows 40 which, when spring 16 moves, expresses air from the interior of the bellows 40 to an orifice of precise diameter to dampen movement of the spring 16.

Arranged within the cavity 25 are a plurality of damping baffles 50 shown in Figure 7. The baffles 50 (not shown in Figures 1 to 6) are arranged within the cavity 25 for damping rotational movement of the ball 20 as will be described in more detail hereinafter.

In the embodiment shown in Figure 7, the baffle 50 merely 25 comprises an apertured plate. In other embodiments, the baffle 50 could be in the form of a block with venturishaped passages through the block.

The strings 24 are anchored to an anchorage location (see Figure 3) provided on the frame structure 27 within •the spherical support member 20. As can be seen in Figure 3, the strings 24 are not anchored at the exact centre point of the spherical support member 20, but rather are offset from the centre of the spherical member 20 by a prescribed distance. In the preferred embodiment of the invention, the spherical member 20 has a diameter of approximately 340 mm and the strings 24 at their anchoring 8 points on the anchorage 45 are spaced radially from the centre of the spherical member 20 by a distance of approximately 8 mm.

Figures 8 to 11 show various embodiments of spring and damping arrangements which can be employed to obtain successively greater reduction of payload motion.

Figure 8 shows the simplest arrangement in which spring 16 and damper 18 are arranged in parallel. Figure 9 shows an arrangement with a double spring arrangement in which a second spring 16' is arranged in series with the spring 16 and damper 18. Figure 10 shows an arrangement in which the damping is the same as in Figure 9 between bird 10 and the spherical support member 20 with a further spring and damping arrangement 16"' arranged between the member 20 and auxiliary mass 35. Figure 11 shows yet a further arrangement in which a frame 47 is interposed between the bird 10 and the support member 20 with the frame 47 being suspended by a spring 16'' and damper 18''.

To minimise angular motion of the SQUID magnetometer, the SQUID magnetometer obviously cannot be rigidly attached to the bird 10 because the bird undergoes vastly more rotational motion than would be permitted at the frequency of interest. The apparatus for reducing rotation according to the preferred embodiments of the invention provides a suspension system for mounting the SQUID magnetometer within the bird to reduce and most preferably eliminate any rotational movement of the SQUID magnetometer with S• reference to the earth's magnetic field. The apparatus according to the preferred embodiments of the invention comprises two main parts, one which seeks to damp out translational motion and which basically comprises the strings 24, springs 14 and dampers 18 and another part which minimises rotational motion and which is comprised by the spherical support member 20 having the outer shell 21 9 and inner shell 23 which define the cavity 25 for containing the damping liquid and baffle plates Although strictly speaking, translational motion does not degrade measurements in practice, any translational motion nearly always suffers some parametric conversion into rotational motion. Thus, one of the main imports of the translational system provided by the springs 14, damper 18 and strings 24 is to minimise the cross-coupling between translation and rotation.

The damping liquid, such as deionised water, within the cavity 25 fills the cavity 25 between the shells 21 and 23 and therefore gives the system a large moment of inertia.

The water is viscously coupled to the shells 21 and 23 through the use of the internal baffles 50. Consequently, when an external torque is applied to the spherical member an angular acceleration results which is initially equal to the torque divided by the moment of inertia. The rotational energy rapidly dissipates as a consequence of i 20 the viscous damping and thus the oscillation of the spherical member 20 is kept to a minimum.

As previously explained, the strings 24 which support the o member 20 are attached at points roughly 8 mm from the 25 centre of the spherical member 20. The strings 24 and the springs 14 and dampers 18 damp out as much translational motion as possible since translational motion will crossooo* couple into rotational motion thereby compromising the performance of the SQUID magnetometer.

Poe* Cross-coupling can be best understood with reference to Figure 12. Assuming that the strings 24 exert a combined force of the spherical member 20 which is equal to Fu.

This will be equal to the weight of the member 20 plus the force exerted by the lower springs, FL. It is principally because FU FL and also because the strings 24 do not meet precisely in the centre of the ball that cross-coupling 10 occurs. If the upper and lower forces were equal then if the member 20 moved sideways through a distance x, the restoring force would be the same both top and bottom and there would be no net torque on the ball. Because these forces are different, however, there is a torque on the ball which is approximately given by the expression shown.

For a system in static equilibrium the term Fu-FL is a constant and is precisely equal to the mass of the member mB, times the gravitational constant g. There is little that can be done to change that. however, it can be seen that the torque is proportional to the radius of the attachment points and inversely proportional to the length of the strings 24. Clearly the longer the strings 24 and the smaller the radius the lower will be the torque. Of particular interest is the remaining term, x(w) which describes the displacement and is a function of the translational oscillation frequency, o. To minimise the torque it is obviously desirable that the translational displacement be kept as small as possible.

Additional translational cross-coupling will occur if there i is a mass imbalance of the total suspended mass. A means to adjust the mass balance in each of three directions, such as counterweights, needs to be included on spherical member Apart from translational cross-coupling, rotational motion of the sensor will also occur quite simply if the bird to which the springs are attached, rotates. This is depicted in Figure 13. Here the restoring torque is proportional to the rotation angle e(o) and to the sum of the upper and lower spring forces and as well as to the attachment radius R, once more. It should at this stage be pointed out that the restoring torques cannot be made arbitrarily small; some restoring force is required, otherwise there would be no way of maintaining the correct orientation of the SQUID magnetometer. Consequently the 11 radius, R, cannot be shrunk completely to zero. At the same time, however, it is important that this non-zero restoring torque occur essentially at low frequencies and be negligible in the frequency range of interest 20 Hz).

It should also be mentioned that it is not torque per se which is of concern but rotational motion. Consequently, the moment of inertia to which angular acceleration is inversely proportional is a critical parameter. It is desirable that the moment of inertia be large while keeping the overall mass small and this is one of the reasons that the water is concentrated in a spherical member 20 as far from the centre of the member 20 as possible.

Since modifications within the spirit and scope of the invention may readily be effected by persons skilled within the art, it is to be understood that this invention is not limited to the particular embodiments described by way of example hereinabove.

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Claims (5)

1. 2. The apparatus of claim 1, wherein the article support member comprises a spherical support member having an inner shell and an outer shell defining a cavity for receiving a damping liquid. tOO 0.
2. 3. The apparatus of claim i, wherein the holding means comprises a bird for towing by an aircraft.
3. 4. The apparatus of claim i, wherein each of the spring members includes a damping means. The apparatus of claim i, wherein the article is a dewar for containing a SQUID magnetometer. o
4. 6. A bird for towing behind an aircraft to move a 30 SQUID magnetometer over an area to be surveyed, the bird including: a casing defining an interior space; an apparatus as defined in any one of claims 1 to positioned in the interior space; and a SQUID magnetometer supported by the article support member. 13
5. 7. The apparatus of claim 2 including baffle means in the cavity. Dated this 14th day of September 2001 THE BROKEN HILL PROPRIETARY COMPANY LIMITED By their Patent Attorneys GRIFFITH HACK Fellows Institute of Patent and Trade Mark Attorneys of Australia .g