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Bristol Aeroplane Company Limited. Engine Stress investigation Memo. Olympus overspeed:...
Catalogue reference: PA1716/5/11/2/375
What’s it about?
This record is a file about the Bristol Aeroplane Company Limited. Engine Stress investigation Memo. Olympus overspeed:... dating from 18 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)
- PA1716/5/11/2/375
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Title (The name of the record)
- Bristol Aeroplane Company Limited. Engine Stress investigation Memo. Olympus overspeed: Overspeeding of Olympus 4 components. Acceptance tests on the 4th stage LP coned rotor assembly
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Date (When the record was created)
- 18 February 1954
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Description (What the record is about)
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Ref: 4096R/4. It was decided at a meeting on the 16th February that spinning tests should be carried out on the 4th and 5th stage LP compressor coned assembly in view of the recent findings on the first two stages of this rotor
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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/3a6927c9-bf4c-47f3-9de6-7ba22556fe96/
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: PA1716/5/11/2/375
Bristol Aeroplane Company Limited. Engine Stress investigation Memo. Olympus overspeed: Overspeeding of Olympus 4 components. Acceptance tests on the 4th stage LP coned rotor assembly