GB2107057A - Suspension system - Google Patents
Suspension system Download PDFInfo
- Publication number
- GB2107057A GB2107057A GB08222428A GB8222428A GB2107057A GB 2107057 A GB2107057 A GB 2107057A GB 08222428 A GB08222428 A GB 08222428A GB 8222428 A GB8222428 A GB 8222428A GB 2107057 A GB2107057 A GB 2107057A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fixed structure
- alignment means
- suspension system
- windings
- twist
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 239000000725 suspension Substances 0.000 title claims abstract description 23
- 238000004804 winding Methods 0.000 claims abstract description 23
- 230000004907 flux Effects 0.000 claims abstract description 21
- 230000008878 coupling Effects 0.000 claims description 4
- 238000010168 coupling process Methods 0.000 claims description 4
- 238000005859 coupling reaction Methods 0.000 claims description 4
- 239000004020 conductor Substances 0.000 abstract description 13
- 239000000463 material Substances 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 2
- 229920003223 poly(pyromellitimide-1,4-diphenyl ether) Polymers 0.000 description 2
- 239000010979 ruby Substances 0.000 description 2
- 229910001750 ruby Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 239000004810 polytetrafluoroethylene Substances 0.000 description 1
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 1
- 229920002545 silicone oil Polymers 0.000 description 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
- G01C17/02—Magnetic compasses
- G01C17/28—Electromagnetic compasses
- G01C17/30—Earth-inductor compasses
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Geology (AREA)
- Electromagnetism (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Environmental & Geological Engineering (AREA)
- Mechanical Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
A suspension system suitable for a flux gate compass having compass windings (14) includes a ball joint (4, 5, 6) which permits both tilt and twist about a vertical axis, and a separate alignment element (16) for causing the windings to follow twisting motion of the fixed structure. The alignment element takes the form of a flexible printed circuit made into a double spiral form and carrying electrical conductors to provide the electrical connections to the windings. A zig-zag shape may be used instead of a spiral (Figs. 3, 4 not shown). The suspension does not suffer from the geometric imperfections of a Hooke's joint, and avoids the need for separate flexible conductors which can interfere with the suspension operation and can break. The alignment element (16) has practically no stiffness axially, and acts principally to resiliently connect an instrument platform (9) to a support (15) for rotational movement in azimuth. <IMAGE>
Description
SPECIFICATION
Suspension system
This invention relates to a suspension system for suspending a directionally indicative or sensitive device for a relatively fixed structure, which can be subjected to tilt about orthogonal horizontal axes and to twist about a vertical axis, and which transmits the twist to the device but not the tilt.
Such a suspension finds application for use with marine compasses for example, but could also be used with other devices such as direction finding aerials or optical surveying instruments.
One well-known structure which can be used to provide such suspension is the Hooke's joint.
However, the Hooke's joint is undesirable for two reasons. First, it is geometrically imperfect. It it is tilted in the quadrantal directions (relative to its principal axes), a degree of twist error is also introduced. This can be quite serious. For 30 degrees of tilt up to about 4 degrees of twist error can be introduced while for 45 degrees of tilt as much as 10 degrees of error can result. For accurate compass work this is clearly most undesirable.
A second disadvantage arises with the Hooke's joint if the device being suspended is an electrical device. In such a case, separate conductors are required to connect the device to the fixed mounting. Even if these are made very light indeed, they can still induce a degree of twist into the joint and cause the suspended device to be forced out of the true horizontal plane.
Furthermore, when the wires are light, they are even more likely to break.
In accordance with the invention there is provided a suspension system for suspending a directionally indicative or sensitive device from a relatively fixed structure which can be subject to tilt about orthogonal horizontal axes and to twist about a vertical axis, the system comprising a substantially spherically-symmetrical mechanical coupling which permits relative tilt and twist, and alignment means for causing the device to follow twisting motion of the fixed structure, the alignment means being of a spiral or zig-zag configuration with the ends thereof coupled respectively to the fixed structure and the device.
Preferably, such a system comprises alignment means which provides electrically conductive paths thereon between the fixed structure and the device. Advantageously the alignment means is formed of a flexible printed circuit which is made from a pianar shape and adopts a helical shape in use.
The invention will now be described in more detail, by way of example, with reference to the drawings, in which: Figure 1 is a sectional view through a first flux gate compass suspension in accordance with the invention;
Figure 2 is a plan view on the line Il-Il in
Figure 1 showing the flexible circuit providing alignment between the compass windings and the support;
Figure 3 is a side elevational view of a second flux gate compass suspension system in accordance with the invention;
Figure 4 is a side sectional view taken on the line IV--IV of Figure 3;
Figure 5 is a plan view of the flexible printed circuit of the embodiment of Figure 3; and
Figure 6 is a plan view of a zig-zag flexible printed circuit in accordance with the invention.
Figure 1 of the drawings illustrates a suspension system which is used to suspend the windings 14 of a conventional flux gate compass from a fixed mounting, which in this case is represented by a shaft 1 7. The mounting may, for example, be fixed relative to a boat such that it is subjected to tilt (pitch and roll) about orthogonal horizontal axes, and also to twist about a vertical axis which, of course, represents a change in the direction of the boat.
The flux gate coil windings 14 are suspended by means of a ball 6 received in a bearing mounting which is formed of two opposed housing members 4 and 5 each having opposed part-spherical recess 1 9 for receiving the ball. The ball 6 is a ruby ball having a hole drilled in it to receive a wire 7 on which the flux gate windings 14 are suspended. The member 5 is secured to the threaded lower end of the shaft 17 while the member 4 is held in place opposite member 5 by a screw 1 which clamps it to the member 5. The degree of tightness with which the ball 6 is held in the recesses 1 9 can be adjusted by means of a grub screw 3 which bears against the member 5 to cause the member 4 to pivot and grip the ball 6 more tightly.The ball joint thus formed allows the winding structure suspended on the wire 7 to tilt relative to the fixed shaft 1 7 in two orthogonal horizontal directions, and also to twist about the vertical direction.
With this arrangement, the coil windings 14 tend to remain in their original alignment when the boat changes direction due to the inertia of the windings 14, that is, the windings 1 4 twist relative to the shaft 1 7.
In order that the coil windings 14 follow the twisting or azimuth movement of the fixed shaft 1 7, and hence of the boat, a separate twist communicating or alignment element is provided in the form of a flexible printed circuit 1 6. This is formed from a flat sheet of flexible material on which is printed a pattern of electrical conductors 38 such as to provide a plurality of conductor paths 21, in this case six, between the coil windings 14 and the fixed structure. The flexible circuit 1 6 is formed by cutting the planar sheet of material as shown in Figure 2 along spiral cut lines 40 so as to form a double spiral, with each arm of the spiral executing approximately one and a half turns.The top end, as seen in Figure 1 , of the double spiral takes the form of a disc on which the conductors connect to terminal pins 1 The pins
11 are secured to a printed circuit board 1 5 which connects them to associated compass circuitry (not shown). The board 1 5 is securely mounted on
the shaft 17 by means of a nut 20 which clamps
the board 1 5 against the housing member 5.
The bottom-end of the flexible circuit 16, which
comprises the central disc-shaped portion 1 8 af the printed circuit, carries similar terminal pins 11 A. These connect to a printed circuit board 91 The printed circuit board 9 has printed circuit
conductors which connect each termina! pin Z1A to a further terminal pin 1 18 on the board 9. A flux
gate former element 13 is suspended from printed
circuit board by means of the terminal pins 1 B.
The flux gate former 13 is of annular shape and
carries the twelve coilwindings 14 which are
electrically connected to the terminal pins 11 B and, hence, to the circuit board 1 5 at the top end
of the flexible circuit 1 6.
Immediately above the disc-shaped portion 1 8 of the flexible circuit 16 is a counterbalance
weight 8. The counterbalance weight 8 is fixed to
the circuit board 9 by means of screws 2 which
pass through holes in the circuit board 9 and the
disc portion 18 of the flexible circuit 1 6. From the
top of the counterbalance weight 8 projects the
wire 7 on which the winding structure 14 is
suspended.
The ball joint formed by the ball 6 and housing
members 4 and 5 permits both tilting and twisting
movement of the suspended winding structure
relatively to the fixed shaft 17. The twisting
movement is, however, restrained by the flexible
printed circuit 16, which adopts the configuration
of a double spiral helix extending between the
fixed shaft 1 7 and the flux gate winding support
structure 13. Any relative twist which may
develop between the suspended structure 13 and
the fixed shaft 1 7 causes a 'winding up' or
'unwinding' of the spiral flexible circuit 16 which it
immediately dissipates by twisting the suspended
structure 1 3 back to its proper position relative to
the fixed shaft 1 7 in which the flexible circuit 1 6 again occupies an unstressed configuration.As a
result, the winding 14 return to their proper
alignment with the fixed shaft 1 7 whenever the
boat changes direction despite the inertia of the
winding structure 1 3. Such a construction is found
to provide remarkably consistent and accurate
orientation of the suspended device relative to the
fixed mounting 17.
A modified version of the suspension system
shown in Figures 1 and 2 will now be described
with reference to Figures 3 and 5.
In these Figures, the flux gate coil structure 7 is
suspended by means of a ball joint formed by a
ruby ball 62 and two opposed bearing members
55 supported by means of a suspension fork 56.
The bearing members 55 are formed with conical
bearing surfaces 57 which grip the ball 62 and the
members 55 are slidable in the suspension fork 56
so that the tightness with which the ball 62 is
gripped can be adjusted. The bearing members 55
are held in position by means of grub screws 59. A
degree of damping of the movement of the
suspended structure 70 is obtained by smearing
the conical bearing surfaces 57 with heavy PTFE
loaded silicone oil.
The ball 62 is drilled on a diameter to form a
hole which receives one arm of a generally
trapezoidal wire frame 61 which carries the flux
gate coil-structure- 70. As the frame 61 can pivot about the arm which passesgthrough the ball 62
and the ball 62 can pivot about a horizontal axis
perpendicular to the arm, the flux gate coil structure- 70 hangs horizontally irrespective of any -tiiting of the form 56 from- which is suspended. It
is also possible for the ball 62 and suspended
structure 70 to rotate relative to the fork 56 in so
far as rotation is not prevented by the wire frame
61 contacting the fork 56.
In order that the coil windings of the flux gate
assembly 70 follow accurately the azimuth
movement of the fork 56 and, hence, of the
supporting structure (in order to sense the heading
of the vessel or vehicle), a separate alignment
element is provided in the form of a flexible
printed circuit 58, shown diagrammatically in
Figures 3 and 4. This is formed from a flat sheet of
flexible printed circuit material 80 on which is
formed a pattern of conductors 83 such as to
provide the necessary electrical connections
between the fixed mounting and the moving parts
of the flux gate assembly. This flexible circuit 58 is
formed by cutting the planar sheet 80 as shown in
Figure 5 along cut lines 82 so as to form a double
spiral with each arm of the spiral executing
approximately 14 turns.
The flexible circuit 58 may consist of a kapton
base of thickness 50 um with conductors of
35 um soft-rolled copper and a 50 um kapton
coverlay. In order to make the finished circuit 58
as flat as possible, the base and coverlay are
bonded together so that their respective directions
of curvature are perpendicular to one another.
The central area 84 of the circuit 59 is attached
to the suspended moving part of the system and
the periphery to the fixed structure at the top. The
top end of the flexible circuit 58 is annular in
shape and is secured to the top side of a circuit
board 51 by six eyelets 66. The eyelets 66 also
provide electrical connections from the flexible
conductors 83 to tracks on the underside of the
rigid board 51 and thence to external circuits by
means of a connector block 52.
The two spiral arms of the flexible circuit 58
pass down through two cut-outs in the rigid board
51 in helical fashion until they join at the bottom
end in the central disc shaped area 84. Here the
same type of eyelet termination connects the
flexible conductors 83 to tracking on the
underside of a lower, smaller rigid printed circuit board 69.
The flux gate assembly 70 is secured
underneath this board 69 by ten pins which are
soldered into holes in the board. Connection is
thus made via the track to the flexible conductors
83 to electrically connect the externai circuits
through the flexible conductors 83 to the flux gate
assembly 70. To ensure that the moving assembly
hangs accurately horizontally a balance washer 67
is mounted on the underside of the lower board
69 and the assembly also includes two screws 68
arranged at right angles for precise adjustment.
The 'legs' of the wire fra-me 61 are soldered into
hollow terminals 71 fitted to the lower board 69.
-Thus the ball 62 support the moving assembly.
This arrangement will allow swinging of the
suspended assembly 70 in two directions but only
limited rotation about a vertical axis as described
above. Such rotation is further restricted by the
behaviour of the flexible circuit 58 which in this configuration has a pronounced resistance to
coiling and uncoiling. It therefore serves to align the
aximuth of the flux gate assembly 70 with that of the supporting structure (e.g. boat), even under
conditions of pitch and roll, to a much-greater
precision than was formerly achievable with a
Hooke's Joint type suspension. It is anticipated that an accuracy as good as one degree may be
obtainable with an arrangement such as
described.
While the examples illustrated use a double
spiral helix in order to provide the required
alignment function, an alternative arrangement
would be to use a single spiral. In appropriate
circumstances, the spiral arrangement could be
substituted by a zig-zag configuration using one or
more zig-zag elements 90 as shown in Figure 6.
The examples illustrated have been given in the
context of a flux gate compass. It will be
appreciated however, that the arrangement may
be suitable for other purposes where a direction
sensitive or direction indicative function is
required, such as in different forms of compass, in
direction finding systems, or in optical surveying
instruments.
Claims (11)
1. A suspension system for suspending a
directionally indicative or sensitive device from a
relatively fixed structure which can be subject to
tilt about orthogonal horizontal axes and to twist
about vertical axis, the system comprising a
substantially spherically-symmetrical mechanical
coupling which permits relative tilt and twist, and alignment means for causing the device to follow twisting motion of the fixed structure, the alignment means being of a spiral or zig-zag configuration with the ends thereof coupled respectively to the fixed structure and the device.
-
2. A system according to claim 1 , in which the alignment means is of double-spiral configuration.
3. A system according to claim 1 or 2, in which the alignment means is formed from a flat sheet and adopts a-helical shape in use.
4. A system according to any preceding claim, in which the alignment means provides electrically conductive paths between the fixed structure and the device.
5. A system according to claim 4 in which the alignment means is a flexible printed circuit having electrically conductive paths printed thereon.
6. A system according to any preceding claim, in which the mechanical coupling is a ball joint.
7. A suspension system substantially as hereinbefore described with reference to Figures 1 and 2 of the drawings.
8. A suspension system substantially as hereinbefore described with reference to Figures 3, 4 and 5 of the drawings.
9. A suspension system substantially as hereinbefore described with reference to Figure 6 of the drawings.
10. A flux gate compass arrangement comprising flux gate compass windings supported by a suspension system from a relatively fixed structure which can be subject to tilt about orthogonal horizontal axes and to twist about a vertical axis, the suspension system comprising a substantially spherically-symmetrical mechanical coupling which permits relative tilt and twist, and alignment means for causing the windings to follow twisting motion of the fixed structure, the alignment means being in the form of a spiral or zig-zag strip with its ends coupled respectively to the fixed structure and the windings.
11. A flux gate compass arrangement according to claim 10 in which the suspension system is in accordance with any of claims 2 to 9.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB08222428A GB2107057B (en) | 1981-08-03 | 1982-08-03 | Suspension system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8123726 | 1981-08-03 | ||
GB08222428A GB2107057B (en) | 1981-08-03 | 1982-08-03 | Suspension system |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2107057A true GB2107057A (en) | 1983-04-20 |
GB2107057B GB2107057B (en) | 1985-01-03 |
Family
ID=26280338
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08222428A Expired GB2107057B (en) | 1981-08-03 | 1982-08-03 | Suspension system |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2107057B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0246138A1 (en) * | 1986-05-13 | 1987-11-19 | Thomson-Csf | Weakly magnetic compass |
CN112378393A (en) * | 2020-09-24 | 2021-02-19 | 杭州瑞利超声科技有限公司 | Floating type anti-inclination orientation fluxgate probe detection device |
-
1982
- 1982-08-03 GB GB08222428A patent/GB2107057B/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0246138A1 (en) * | 1986-05-13 | 1987-11-19 | Thomson-Csf | Weakly magnetic compass |
FR2598798A1 (en) * | 1986-05-13 | 1987-11-20 | Thomson Csf | LOW MAGNETIC COMPASS |
US4774766A (en) * | 1986-05-13 | 1988-10-04 | Thomson-Csf | Weakly magnetic compass |
CN112378393A (en) * | 2020-09-24 | 2021-02-19 | 杭州瑞利超声科技有限公司 | Floating type anti-inclination orientation fluxgate probe detection device |
Also Published As
Publication number | Publication date |
---|---|
GB2107057B (en) | 1985-01-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |