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GB2069105A - Guns - Google Patents

Guns Download PDF

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Publication number
GB2069105A
GB2069105A GB8004425A GB8004425A GB2069105A GB 2069105 A GB2069105 A GB 2069105A GB 8004425 A GB8004425 A GB 8004425A GB 8004425 A GB8004425 A GB 8004425A GB 2069105 A GB2069105 A GB 2069105A
Authority
GB
United Kingdom
Prior art keywords
gun
optical
barrel
muzzle
optical means
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.)
Withdrawn
Application number
GB8004425A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BAE Systems Electronics Ltd
Original Assignee
Marconi Co Ltd
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
Application filed by Marconi Co Ltd filed Critical Marconi Co Ltd
Priority to GB8004425A priority Critical patent/GB2069105A/en
Priority to EP19810300462 priority patent/EP0034441A1/en
Publication of GB2069105A publication Critical patent/GB2069105A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G3/00Aiming or laying means
    • F41G3/32Devices for testing or checking
    • F41G3/323Devices for testing or checking for checking the angle between the muzzle axis of the gun and a reference axis, e.g. the axis of the associated sighting device

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

1
GB 2 069 105 A 1
SPECIFICATION
Improvements in or relating to guns
This invention relates to guns and is particularly applicable to guns having a relatively long and 5 massive barrel such as a battle tank. The direction of travel of a shell fired by a gun depends on the boreline direction of the barrel in the region of the muzzle and even very small boreline errors can give rise to significant aiming errors at long range. 10 It has been found that even when relatively sophisticated optical aiming sights are used to lay the gun on a target significant aiming errors can remain. These errors are at least in part due to uncertainties in the direction of the boreline of the 15 muzzle and they can stem from the presence of temperature gradients across the diameter of the barrel which can cause the barrel to bend slightly. It has been proposed to compensate for this particular source of error by aligning the aiming 20 mark of an optical sight with a reference image obtained via a reflector mounted on the muzzle of the gun, so that movement of the muzzle caused by distortion of the barrel can be detected. However, this error can only be detected when the 25 optical sight is being used at unusually low optical magnifications and when the barrel is moved to a low angle of elevation, and thermal stresses set up in the barrel during firing cannot easily be taken into account. Moreover this ignores muzzle 30 boreline errors caused by other factors.
The present invention seeks to provide an improved gun.
According to this invention a gun includes a barrel mounted so as to be rotatable in elevation; 3 5 optical means for monitoring the boreline direction of the barrel in the region of its muzzle, said optical means including an optical detector arranged to receive an image from an optical source via a reflector mounted on the muzzle, and 40 the optical means being mounted so as to be movable in elevation with said barrel.
When a gun is fired, the reaction of the shell produces a recoil, and in a tank gun the barrel is slidably mounted within a cradle so as to enable 45 the recoil force to be safely dissipated. The cradle is rotatably mounted on trunnions by means of which the cradle and hence the barrel can be rotated in elevation. The barrel is subject to violent shock, vibration, and acceleration when the gun is 50 fired and for this reason it is not desirable to mount the optical means directly on the barrel.
Preferably the optical means is mounted on a member which moves with and is rigidly coupled to the cradle.
55 Preferably again the optical means is mounted on the mantlet of a gun. The mantlet is usually in the form of a strong metal plate and its function is to shield the elevation mechanism of the gun at all elevation angles, i.e. it closes what would 60 otherwise be an exposed vertically arranged aperture within which the barrel moves in elevation.
The optical source may be arranged to generate visible light, or alternatively the light may be in a
65 region of the spectrum which is invisible to the human eye, and conveniently the illumination is in the infra-red region.
The optical detector comprises a two dimensional receiving surface which is positioned 70 so as to receive light via the reflector from the optical source with the optical detector being arranged to provide as an output an indication of the position of the received image on the receiving surface. The optical detector may therefore consist 75 of a matrix of individual light sensitive devices, or alternatively of a sheet of material whose electrical properties are modified by the presence of an optical image.
The boreline direction of a gun is affected by 80 temperature gradients which are present across the diameter of its barrel. After the gun has been fired for some time the barrel will become hot and the effect of a side wind or rain is to cool the barrel unevenly. As a result, the coolest face of the barrel 85 shrinks slightly and the barrel bends into the direction of the cooling effect. Similarly, the effect of solar radiation on the barrel is very similar and a temperature gradient can exist from the top surface of the barrel to the lower surface whether 90 the gun has been fired or not, thereby causing the barrel to droop very slightly. The effects of the distortion can be vary marked and can significantly influence the aiming accuracy of a gun. For example, a 5°C difference from one surface of the 95 barrel to the other can at long range produce an aiming error of a few metres.
It has been previously suggested that aiming errors due to this effect can be minimised by using the conventionally provided optical sight in 100 combination with a reflector mounted on the muzzle of the barrel. The optical sight is used by the gunner and is consequently mounted on a rotatable turret in conventional tanks. Because of this it is off-set from the axis of the barrel and it 105 can be used to view a reflector mounted on the muzzle of the barrel only at magnifications which are less than those which would normally be used in firing the gun. Additionally, it is necessary to bring the elevation of the barrel to a 110 predetermined low angular position and to insert an optical prism into the gunner's sight by means of a mechanical lever mechanism to allow the gunner to view the reflector mounted on the muzzle when using the high-gain optical channel 115 of the sight. Boreline errors measured in this way do not take any account of mechanical backlash which might be present between the barrel and the turret in which it is mounted and these backlash errors can also be significant.
120 The invention is further described by way of example with reference to the accompanying drawing in which,
Figure 1 shows a side view of a gun in accordance with the present invention mounted 125 on a tank,
Figure 2 is a diagrammatic plan view of the gun barrel and
Figure 3 is an explanatory diagram illustrating part of the optical means of which muzzle boreline
2
GB 2 069 105 A 2
errors can be corrected.
Referring to the drawing, a battle tank 1 is provided with a turret 2, which is mounted so as to be rotatable in azimuth about a vertical axis 3.
5 The turret supports a long barrel 4 which is mounted within the turret 2 so as to be rotatable in elevation relative to the turret. A gunner who controls the firing of the gun is located within the turret 2 in a position to one side of the axis of the 10 barrel 4. An optical reflector 5 is mounted at the muzzle 6 of the barrel 4 with the reflector 5 being arranged to co-operate with optical means 7. These optical means 7 comprises an optical source 8 and an optical detector 9, which are 15 mounted side by side and are illustrated diagrammatically in Figure 3. These optical means 7 are mounted on the mantlet 10 of the gun.
It is necessary to allow for the recoil of the barrel when a shell is fired and for this reason the 20 barrel 4 is slidably mounted within a cradle 11. The cradle 11 is illustrated in plan view in Figure 2 and it is arranged to surround the barrel 4 and is mounted within the turret 2 so as to be rotatable in elevation about a horizontal axis 12. The cradle 25 11 is rotatable by means of suitably shaped trunnions which align with the axis 12 and allow the cradle 11 to be rotatably mounted on members 13, which are rigidly secured to the body of the turret 2.
30 Thus when the gun is fired and a shell is ejected from the muzzle 6, the barrel 4 recoils and slides backwardly within the cradle 11. The cradle 11 is provided with bearing surfaces so as to permit the barrel 4 to slide with the minimum of sideways 35 movement, but even so a certain amount of lateral movement due to mechanical tolerances and sliding clearances is inevitable.
When the gun is to be fired at a target, an aiming mark 30 in an optical sight 31 is manually 40 aligned with the target by the gunner, as the aiming mark is normally to be superimposed on the target when the gun is correctly aimed. The aiming mark is positioned within the optical sight so as to allow for a number of factors, such as the 45 characteristics of the shell, its initial velocity, cross wind, range etc. These variable factors can be stored in a gun fire control 32 system into which they are entered via leads 33 and used to modify the position of the aiming mark in the sight as 50 necessary. The invention provides for the positioning of the aiming mark to additionally take into account boreline direction errors, that is to say, the errors which stem from the fact that the boreline direction 15 of the muzzle 6 may not be 55 exactly correctly orientated relative to the aiming sight. As previously described these errors can stem from temperature gradients set up across the barrel. Additionally, errors can stem from mechanical movements of the barrel within cradle 60 11. In particular, this mechanical movement can be caused by wear in the cradle as the barrel slides within it. Even a relatively small mechanical movement at this point can produce a relatively large error in the boreline pointing direction 15. 65 For example, if the boreline direction is accurately measured whilst the tank is stationary, the errors may change when the tank is used on an incline which imposes a sideways gravitational thrust upon the cradle and trunnion. Such errors cannot be predicted in advance, since they depend on a large number of variable factors, e.g. the slope of the ground on which the tank is standing, the angle of elevation of the barrel and the angle of azimuth or traverse of the turret. If the tank is to be fired whilst it is on the move, the dynamic flexing of the gun barrel due to its length can cause further errors of an unpredictable nature. The invention provides means for monitoring these errors so as to modify the position of an aiming mark in the optical sight to compensate.
The operation of the gun is as follows. The optical source 8 produces a narrow beam of infrared light which is directed towards the reflector 5 mounted on the muzzle 6 of the barrel 4. The reflector 5 is mounted very securely so that it is not displaced by the recoil of the gun when it is fired. The position and direction of the reflecting surface are very important and must be maintained constant relative to the muzzle. The beam of light is reflected back to an optical detector 9. The movement of the optical beam across the detecting surface of the detector 9 is twice that of the movement of the reflector 5, due to the double path length. Typically the distance between the mantlet 10 and the reflector 5 is 5 metres or more. Consequently even extremely small movements of the reflector 5 produce significant and measurable movements of the light beam across the surface of the detector 9. To allow for large errors, the surface area of the detector 9 should typically be several centimetres square. Alternatively, if a proprietary detector of small area is employed, an optical arrangement placed in front of the detector can be used to reduce the area swept by the light beam to the available area of the detector surface.
The detector 9 may comprise a two dimensional planar matrix of photosensitive diodes, with typically the diodes being spaced about 1 millimetre apart to provide the required degree of resolution. Of course the actual size of the detector 9 and its resolution will depend on the characteristics of the gun and the required degree of accuracy. Instead of forming the detector 9 of an array of individual photo diodes, it may instead comprise an area of a light sensitive receiving surface surrounded by a number of electrodes. In this case the signal amplitude provided at each electrode is related to the position of the optical beam on the surface and these signals are fed to the fire control system 32. One device of this kind is an opto electronic analogue sensor type S1200 or S1300 produced by Hamamatsu TV Co. Limited, Japan.
Although the optical beam and detector may be operated continuously, this is not necessary since it need only be energised during the period immediately preceding the firing of the gun. It may be arranged to be automatically engaged at the commencement of a fire control sequence. Since
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3
GB 2 069 105 A 3
the system is capable of operating continuously, whilst the gun is being layed for firing, the effect of errors can be corrected as they develop and are detected.

Claims (9)

5 CLAIMS
1. A gun including a barrel mounted so as to be rotatable in elevation; optical means for monitoring the boreline direction of the barrel in the region of its muzzle, said optical means 10 including an optical detector arranged to receive an image from an optical source via a reflector mounted on the muzzle, and the optical means being mounted so as to be movable in elevation with said barrel.
15
2. A gun as claimed in claim 1 and wherein the optical means is mounted on a member which moves with and is rigidly coupled to a cradle within which the barrel is slidably mounted.
3. A gun as claimed in claim 2 and wherein the 20 optical means is mounted on a mantlet.
4. A gun as claimed in claims 1,2 or 3 and wherein the optical source is arranged to generate a narrow beam of infra-red light.
5. A gun as claimed in claim 4 and wherein the 25 optical detector comprises a two dimensional receiving surface which is positioned so as to receive light via said reflector from the optical source.
6. A gun as claimed in claim 5 and wherein the 30 receiving surface comprises a two dimensional matrix of individual photosensitive devices.
7. A gun as claimed in claim 6 and wherein the photosensitive devices are photo diodes.
8. A gun as claimed in claim 5 and wherein the 35 optical detector comprises a two dimensional receiving surface which is constituted by a sheet of material whose electrical properties are modified by the presence of an optical image.
9. A gun substantially as illustrated in and 40 described with reference to the accompanying drawing.
Printed for Her Majesty's Stationery Office by the Courier Press, Leamington Spa, 1981. Published by the Patent Office, 25 Southampton Buildings, London, WC2A 1AY, from which copies may be obtained.
GB8004425A 1980-02-09 1980-02-09 Guns Withdrawn GB2069105A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB8004425A GB2069105A (en) 1980-02-09 1980-02-09 Guns
EP19810300462 EP0034441A1 (en) 1980-02-09 1981-02-04 Optical means for monitoring the boreline direction of a gun

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8004425A GB2069105A (en) 1980-02-09 1980-02-09 Guns

Publications (1)

Publication Number Publication Date
GB2069105A true GB2069105A (en) 1981-08-19

Family

ID=10511245

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8004425A Withdrawn GB2069105A (en) 1980-02-09 1980-02-09 Guns

Country Status (2)

Country Link
EP (1) EP0034441A1 (en)
GB (1) GB2069105A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0092324A2 (en) * 1982-04-17 1983-10-26 The Marconi Company Limited Gun with means for verifying the boreline direction
US4879814A (en) * 1987-08-28 1989-11-14 Texas Instruments Incorporated Method and apparatus for boresight alignment of armored battlefield weapons

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1223652A (en) * 1983-04-29 1987-06-30 Raymond Carbonneau Gun muzzle reference system
US4843485A (en) * 1983-12-23 1989-06-27 General Electric Company Multiple format digital video tape record and replay system
NL8402659A (en) * 1984-08-31 1986-03-17 Optische Ind De Oude Delft Nv METHOD AND APPARATUS FOR JUSTING THE SIMILARITY OF A VISOR DEVICE AND A SWIVEL ORGAN.
DE3623455C3 (en) * 1986-07-11 1994-07-07 Krauss Maffei Ag Optical visor
DE3707443A1 (en) * 1987-03-07 1988-09-15 Zeiss Carl Fa FIELD ADJUSTMENT FOR THERMAL IMAGING DEVICES
BE1009299A3 (en) * 1995-02-16 1997-02-04 Belge De Const Aeronautiques E Detection method and device for the use of said method
GB9503485D0 (en) * 1995-02-22 1995-04-12 Pilkington Perkin Elmer Ltd Displacement measurement apparatus and method
SE524435C2 (en) * 2002-12-17 2004-08-10 Saab Ab Methods and apparatus for screening of sight and fire pipes

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE325494B (en) * 1969-04-22 1970-06-29 Bofors Ab

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0092324A2 (en) * 1982-04-17 1983-10-26 The Marconi Company Limited Gun with means for verifying the boreline direction
EP0092324A3 (en) * 1982-04-17 1985-07-31 The Marconi Company Limited Gun with means for verifying the boreline direction
US4879814A (en) * 1987-08-28 1989-11-14 Texas Instruments Incorporated Method and apparatus for boresight alignment of armored battlefield weapons

Also Published As

Publication number Publication date
EP0034441A1 (en) 1981-08-26

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Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)