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Rate Integrating Gyro

Technical Information

Catalogue No: C0597
Category: Gyro
Object Type: Module/Sub-Assembly/Component
Object Name: Rate Integrating Gyro
Part No: 49/X
Serial No: 5653
Manufacturer: British Aircraft Corporation
Division: Guided Weapons [GW - of BAC]
Platform(s):
Year of Manufacture: circa 1975
Dimensions: Width (mm): 55
Height (mm): 55
Depth (mm): 70
Weight (g): 280
Location: Rack RAA09 [Main Store]
Inscription(s):

British Aircraft Corporation
(G.W.Division)
Stevenage, Herts.
Rate-Integrating Gyro.
Type No. 49/X
Serial No. 5653
By Agreement with Honeywell Inc.

Notes:

This Rate Gyro bears the legend ‘By arrangement with Honeywell’and ‘NATO No. 6JA6615991109882’

A Rate Integrating Gyroscope is a Rate Gyroscope with a built in integrator. Therefore a Rate Integrating Gyroscope measures and indicates change of angle.

Inertial devices such as rate gyroscopes, rate integrating gyroscopes, and accelerometers are common in modern navigation systems. Other uses include active stabilization of cameras, platforms, and other motion sensitive applications.

Inertial devices therefore internally contain the required resistance to movement either in the form a spinning mass (a source of inertia) such as in gyroscopes, or a suspended mass such as in accelerometers.

In a typical application (e.g. an aircraft), the output axis could have revolved 180 degrees clockwise in 20 seconds, then 80° anti-clockwise (say if the aircraft was changing direction again). This output would then be fed to a Navigation computer to calculate the total distance traveled.

 

In April 1958 English Electric acquired a licence to manufacture Honeywell gyros at Stevenage. English Electric Aviation Ltd became a founding constituent of the British Aircraft Corporation (BAC) in 1960 and the guided weapons division was added to BAC in 1963. In 1975 BAC bought out the future royalties for the Honeywell license and BAC became part of the new BAE Systems in 1999.

The Miniature Integrating Gyro (MIG) employs a gimbal floated at neutral buoyancy in a fluorocarbon fluid and pivoted between jewelled bearings. The manufacture and assembly of such a gyro called for standards of precision unprecedented not only in industry but even in specialist laboratories. A crucial issue was vibration. The Instrument Wing was located between the Eastern Region main line to the north and the new Stevenage by-pass road, and further vibration came from machinery in the company's plant—and even from the footfalls of the staff. Accordingly, test equipment was mounted on concrete plinths carried on 50-ton concrete rafts supported on air bellows resting on heavy foundations deep in the earth.

The assembly and test area were clean rooms fully temperature and humidity controlled and it is the only miniature inertial quality gyro in production in Europe. These Gyros were used in inertial guidance systems for missiles and torpedoes for example.

Northrop Licence

 Marconi licenced a range of gyros from Northrop; initially the GR-H4 in the mid-60's and then the G1-G6 in 1980.

The GR-H4 rate-gyroscope was built under licence from Northrop, producer of the original version. The gyro is contained in a 1in x 2 in cylinder and is extremely accurate and strong. It is fluid damped, but requires no heater controls. In 1968 Dick Scott and the Gyro Division team landed a major contract for Elliott Nortronics sub-miniature rate gyros for the television guidance head of the Anglo-French Martel air-to-surface missile; the ultimate value of the order iat that time was expected to exceed £900,000.

In 1980 Marconi Avionics of Rochester has just completed its 10,000th rate-gyroscope, marking 15 years of manufacture. The GR-H4 rate-gyroscope is built under licence from Northrop, producer of the original version. Applications of the Marconi Avionics-built gyroscope include the Sea Vixen carrier-borne interceptor guidance, the guidance system of Sky Flash, the RAF's most advanced air-to-air missile, and stabilisation of Harrier and the Sea Dart ship-to-air missile. While building GR-H4s, Marconi Avionics introduced several improvements, independently of Northrop. At the same time unit cost was reduced, by a factor of almost three. (The 1980 cost of the rate-gyroscope was £850-£l,300, depending on application.) Marconi Avionics improvements include replacement of the steel gyro casing with one of Monel nickel alloy incorporation of a mu-metal screen to isolate the gyroscope motor's magnetic field; introduction of chemical etching (in place of lapping) to trim the torsion bar; adaption of semi-automatic test equipment and multiple jigging to simplify production. Marconi Avionics also introducedplastic damping vanes and replaced hand-wired parts by flexi-circuits. In 1980 GR-H4 production rate was roughly 100 units a month.

In 1981 Marconi  introduced the GI-G6 into production in a £750,000 development. The G6 is proposed for the Spearfish torpedo (formally Naval Staff Target 7525), and a strapdown system using the gyro was fitted to the Machan experimental unmanned aircraft.

The input rate range is +/- 10deg/sec to +/- 1000 deg/sec.

 

Allied Signal  aquisition

Allied Signal was an American aerospace, automotive and engineering company created through the 1985 merger of Allied Corp. and Signal Companies. It acquired Bendix Corp. gyroscope business which was later sold to Condor Pacific Industries in 1999. Condor Pacific was established in 1964 to manufacture miniature mechanical, spinning wheel gyros. Condor later went on to acquire Allied Signal's gyro manufacturing business (1999) and shortly afterwards was itself acquired by BAE Systems (2002). BAE Systems acquires Condor Pacific and forms the BAE Systems Inertial Products Division.

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