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Bristol Aeroplane Company Limited. Engineering Department. Engine Stress investigation....
Catalogue reference: PA1716/5/11/2/380
What’s it about?
This record is a file about the Bristol Aeroplane Company Limited. Engineering Department. Engine Stress investigation.... dating from 22 February 1954.
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Full description and record details
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Reference (The unique identifier to the record described, used to order and refer to it)
- PA1716/5/11/2/380
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Title (The name of the record)
- Bristol Aeroplane Company Limited. Engineering Department. Engine Stress investigation. Olympus overspeed. Experimental clearance B.OL.4 LP 4th & 5th stage rotor blades for overspeed testing
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Date (When the record was created)
- 22 February 1954
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Description (What the record is about)
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Ref: 4096/4. Stress Office. In order to test a coned assembly of the 4th & 5th stage rotor discs schedule assembly B.91681 has been prepared listing the existing parts to be obtained from the rotor assembly, also a new part B.91862 Blade weight retainer (4th stage), which is to be manufactured. Test Plant Design Office will make an adaptor to suit these discs
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Held by (Who holds the record)
- Coventry Archives & Research Centre
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Language (The language of the record)
- English
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Physical description (The amount and form of the record)
- 1 Item
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Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/60bf004e-86f0-4e6c-98b6-23c80dd759d2/
Series information
PA1716/5/11/2
Bristol Gas Turbines: Olympus stress reports & calculations for all models
See the series level description for more information about this record.
Catalogue hierarchy
This record is held at Coventry Archives & Research Centre
Within the fonds: PA1716
Rolls-Royce Heritage Trust, Coventry Branch - Records of Armstrong Siddeley, Bristol...
Within the sub-fonds: PA1716/5
Armstrong Siddeley/Bristol Siddeley & Rolls-Royce Gas Turbines
Within the sub-sub-fonds: PA1716/5/11
Olympus Engine
Within the series: PA1716/5/11/2
Bristol Gas Turbines: Olympus stress reports & calculations for all models
You are currently looking at the file: PA1716/5/11/2/380
Bristol Aeroplane Company Limited. Engineering Department. Engine Stress investigation. Olympus overspeed. Experimental clearance B.OL.4 LP 4th & 5th stage rotor blades for overspeed testing