GB2137342A - Mounting a unit in a casing - Google Patents

Abstract

The inner unit (1) of a gyroscope is of circular shape and is formed with an inclined outer edge (36) at one end. The inner unit (1) slides within an outer casing (2) having a transverse end face (38) atone end. An annular recess (37) of triangular section is thereby defined between the inner unit (1) and casing (2) which receives a ring (40) of resilient material. During assembly the inner unit (1) is urged against the end of the casing (2), to compress the ring (40) within the recess (37), by reducing pressure within the casing. The inner unit (1) is held in position, with the ring (40) compressed, by soldering an end plate (4) to the casing (2). The pressure within the casing (2) can then be returned to normal. <IMAGE>

Description

SPECIFICATION Arrangements and methods of mounting a unit in a casing This invention relates to arrangements and methods of mounting a unit in a casing.

The invention is more particularly, but not exclusively concerned with arrangements and methods of mounting gyroscope equipment in a casing.

Because ofthe high rotational speeds of gyroscopes they can be prone to vibration. Although attempts are usually made to ensure that mechanical components ofthe gyroscope are a close fit within the casing, so as to reduce any vibration within the casing, there has to be sufficient clearance between the casing to allow for easy insertion and removal. There is also the problem that the heat produced by the gyroscope can cause differential thermal expansion with respect to the casing. If no room is leftwithin the casing to accommodate such expansion it can resu It in stress on the gyroscope components.

It is an object ofthe present invention to provide apparatus that can be used to alleviate these problems.

According to one aspect ofthe present invention there is provided apparatus including an inner unit contained within an outer casing,the casing being provided with a transverse face towards one end, and the inner unit being provided at one end with an inclined edge surface that defines, with the transverse face, an annular recess of substantiallytriangular section, the apparatus including a ring of resilient material that extends within the recess, and the inner unit being secured in the casing such that the ring is held in compression between the inner unit and the outer casing.

The resilient ring exerts a restraining force on the inner unitthat helps reduce vibration ofthe inner unit relative to the casing.

The edge surface may be inclined to the transverse face at an angle of about 60". The recess and the ring may be of circular shape. The ring may have a substantially circular cross-section in its natural state.

The inner unit may be spaced from the casing atthe one end. Thetransverseface may be provided by the inside face of one end ofthe casing. The inclined edge surface may be the outer edge surface of the inner unit The outer casing may be sealed at its other end.

The inner unit may include gyroscope apparatus.

According to another aspect of the present invention there is provided a method of mounting an inner unitwithin an outer casing, the outer casing having a transverse face therein towards one end, and the inner unit having an inclined edge surface at one end, a ring of resilient material being positioned in said casing againstthetransverseface, said inner unit being inserted within the outer casing so that said edge surface contacts said ring, pressure within said casing being reduced relative to pressure outside the casing so as thereby to force the inner unit further into the casing, and the inner unit being then secured in position relative to the casing with the ring in compression.

The pressure within the casing may be made equal to pressure outside the casing after the inner unit is secured in position.

Gyroscope apparatus, and a method of assembly of gyroscope apparatus, in accordance with the present invention, will now be described, by way of example, with reference to the accompanying drawings, in which: Figure lisa sectional side elevation of the apparatus; and Figure 2 isa cross-section of the apparatus along the line Il-Il of Figure 1.

The apparatus comprises an inner unit 1, including the gyroscope mechanics, that extends within an outer casing 2 that is closed at one end 3. The other end ofthe apparatus is sealed by an end plate 4that abuts the inner unit 1.

The construction and operation ofthe gyroscope mechanism is substantially the same as that described in the specification of UK Patent Application GB 2063 471Aso itwill only be described briefly here. The inner unit 1 is of generally cylindrical configuration having a tubular rotor 10 that is supported at opposite ends by bearings 11 and 12. The rotor 10 is rotated aboutthe longitudinal axis 13 of the apparatus by a motor 14 located towards the right hand end of the unit 1. A gimbal ring 15 is supported by two flexure pivots 16 and 17 on the left hand endofthe rotor l0sothatthe gimbal ring is free for limited angular displacement about an axis 18 at right angles to the longitudinal axis 13.An inertia ring 20 encirclesthe gimbal ring 15 and is supported on it by two furtherflexure pivots (not shown), located intermediate the pivots 16 and 17. In this way, the inertia ring isfreefordisplacementabout an axis 21,at right anglesto the other axes 13 and 18 and hence is supported aboutthetwo perpendicular axes 18 and 21.

Displacement ofthe gyroscope apparatus having a component about either axis 18 or 21 causes displace ment ofthe inertia ring 20 relative to the remainder of the apparatus, since the inertia ring tends to retain its original attitude. This relative displacement is sensed by a pick-off 22 the output of which is used to control the supply of currentto torquer coils 23. The torquer coils 23 exert a restoring force on the inertia ring to keep it in a datum position relative to the gyroscope structure, the current supplied to the coils being used to provide an indication of the displacement rate of the gyroscope.

At the rear end of the inner unit 1 there is a dish-shape base member 30 that is formed around its outer edge with a circumferential lip 31. The lip 31 engages a cooperating shoulder 32 formed around the inside ofthe outer casing 2, close to its rear end. The shoulder 32 forms a shallow step between the forward end of the casing 2 and the rear end which is of slightly greater internal diameter. Engagement of the lip 31 with the shoulder 32 locates the inner unit 1 against forward axial movement.

The forward end of the inner unit 1 carries a radially-extending plate member 35 that is a close fit around its edge withintheforward end of the casing 2.

The forward face ofthe plate member 35 is parallel with the closed end of the casing 2 and is separated from it by a small clearance 33. The edge ofthe plate member 35 is bevelled its forward end to form an annular surface 36thatis inclined at about 300 to the curved wall ofthe casing 2 and at about 600 to its closed end. This inclined edge 36 defines an annular cavity 37 of triangular section with the innerface 38 of the closed end 3 ofthe casing 2. Within the cavity 37 there is located a resilient support ring 40, such as of rubber or plastics material.The ring 40 has, in its natural state, a circular cross-section. The thickness of the ring 40 is such that, when the inner unit 1 is pushed forwardlyto itsfull extent, the ring is compressed between the forward end ofthe inner unit and the casing 2. The compressive forces exerted againstthe inner unit 1 are directed perpendicularto the inclined edge 36, along the arrow F in Figure 1. This force therefore has a component parallel to the axis ofthe gyroscope and a component transverse of the gyroscope. These componentsthereby act on the inner unit 1 to resist and damp any transverse or axial displacement, such as may be caused by vibration.

The small clearance 33 between the forward end ofthe inner unit 1 and the casing allows for some limited relative axial displacement and, in this respect accommodates differential thermal expansion ofthe central unit.

At its rear end, the base member 30 has an annular step 42 of square section that receives a sealing ring 43.The ring 43 engages the inner surface ofthe casing 2 and the forward surface ofthe end plate 4. The end plate 4 carries various terminals 50 that serve to make electrical connection with an electronics unit 51 located between the base member 30 and the end plate 4. Aroundits rear end,the end plate 4 also has an annular step 52 of rectangular section that receives two sealing rings 53 and 54. The inner sealing ring 53 is of a resilient material and of a thickness that ensures that it is compressed within the step 52 in close contact with the end plate 4 and the casing 2.The outer ring 54 is of metal and serves primarily as a filler, the ring being secured in the step 52 by means of solder 55 which provides an effective seal with the casing 2. A sealable spigot 56 is located centrally ofthe plate 4.

The spigot 56 provides a passageway to the interior of the gyroscope apparatus which can be used to remove airfrom, or introduce gasto,the apparatus, and is subsequently sealed.

The gyroscope is readily assembled by first placing the support ring 40 in the forward end ofthe casing 2.

The inner unit 1 is then slid into the casing 2 that the inclined edge 36 engages the support ring 40. The sealing ring 43 is then inserted in the step 42 atthe rear ofthe inner unit 1. The next operation isto insert the end plate 4which must be pushed forwardly so that the lip 31 on the inner unit 1 engages the shoulder 32 on the casing 2,so as to compress the support ring 40.

In the preferred embodiment, the force to urge the inner unit 1 forwardly is obtained by applying suction to the spigot 56 so asto obtain a reduced pressure within the casing of, for example, between a quarter and a half atmosphere. When the reduced pressure has been achieved and the inner unit 1 is correctly located within the casing 2, the end plate 4 is sealed to the casing by means ofthe rings 53 and 54 and the solder 55. Afterthe solder 55 has hardened, the suction may be removed, thereby allowing the pressurewithin the casing to revert to its desired level before the spigot 56 is sealed. The seal formed by the solder 55 is sufficientto retain the inner unit 1 against the forces exerted by the support ring 40 even without a reduced pressure within the casing 2.

It will be appreciated that various other arrangements could be used to retain the inner unit 1 in its correct location while the end plate4is being sealed to the casing 2. lnthisrespect,theend plate4could be urged forwardly intothe casing 2 by means, for example, ofclamps.

It will be appreciated that the arrangement described above is not confined to use with gyroscope apparatus but can be used to mount other apparatus in a casing.

Claims (14)

1. Apparatus including an innerunitcontained within an outer casing, wherein the casing is provided with a transverse face towards one end, andthe inner unit is provided at one end with an inclined edge surface that defines, with the transverse face, an annular recess of substantially triangular section, wherein the apparatus includes a ring of resilient material that extends within the recess, and wherein the inner unit is secured in the casing such thatthe ring is held in compression between the inner unit and the outer casing.

2. Apparatus according to Claim 1, wherein the edge surface is inclined to the transverse face at an angle of about 600.

3. Apparatus accordingto Claim 1 or2,wherein the recess and the ring areof circular shape.

4. Apparatus according to any one of the preceding claims, wherein the ring has a substantially circular cross-section in its natural state.

5. Apparatus according to any one of the preceding claims, wherein the inner unit is spaced from the casing atthe one end.

6. Apparatus according to any one ofthe preceding claims, wherein the transverse face is provided by the inside face of one end ofthe casing.

7. Apparatus according to any one ofthe preceding claims, wherein the inclined edge surface is the outer edge surface ofthe inner unit.

8. Apparatus according to any one ofthe preceding claims, wherein the outer casing is sealed at its other end.

9. Apparatus according to any one of the preced- ing claims, wherein said inner unit includes gyroscope apparatus.

10. Apparatus substantially as hereinbefore described with reference to the accompanying drawings.

11. A method of mounting an innerunitwithin an outer casing, the outer casing having atransverse face therein towards one end, and the inner unit having an inclined edge surface atone end, wherein a ring of resilient material is positioned in said casing against the transverseface, wherein said inner unit is inserted within the outer casing so that said edge surface contacts said ring, wherein pressure within said casing is reduced relative to pressureoutsidethe casing so astherebyto force the inner unitfurther into the casing, and wherein the innerunitis then secured in position relative to the casingwith the ring in compression.

12. A method according to Claim 11, wherein the pressure within the casing is made equal to pressure outsidethe casing afterthe inner unit is secured in position.

13 A method substantially as hereinbefore described with reference to the accompanying drawings.

14. Any novelfeature or combination offeatures as hereinbefore described.