Access to Archives

Part of the UK archives network

Rolls-Royce Heritage Trust, Coventry Branch - Records of Armstrong Siddeley, Bristol Siddeley etc.


The hierarchical structure of this catalogue is shown below. See the entire contents of the catalogue

Reference PA1716
Covering dates 20th Century
Held by Coventry Archives



Folder icon  Rolls-Royce Limited. Bristol Engine Division: 2 drawings of Olympus 20101, 20201 & 20301 compressor casing; 3 drawings of turbine  PA1716/5/11/3/5  c. 1960

These documents are held at Coventry Archives

1 Item

Contents:
Drawing 7 & 79 compressor casing (rear) also B59432 bracket. Drawing 5 combustion chamber outer casing. Drawing 40 turbine (part 2); Drawing 39 sheet 2 turbine (part 1); 39 sheet 1 turbine (part 1)


No further details   Bristol Aero Engines Limited: Drawing TP.4087 Olympus 201 turbojet Fuel system diagram  PA1716/5/11/3/6  6 February 1959
Expand   Bristol Siddeley Flight Development Section: Olympus 301 Vulcan B.Mk.2 XH557 assessment of 'speed-term' AFRC  PA1716/5/11/3/7  19 July 1963
Expand   MoS: Air Publication AP.1902 Cover 2, Section 4, Chapter 1A AL.86: Vulcan flight idling detent; Maximum friction  PA1716/5/11/3/8  September 1972
Expand   Olympus 300 flame-outs. Rolls-Royce Aero Division Ansty: Olympus 301. Minutes of meeting to discuss flame-out problems held at Parkside  PA1716/5/11/3/9  22 July 1980
Expand   Olympus 300 flame-outs: RAF Headquarters No.1 Group Bawtry Doncaster Yorkshire. Vulcan 300 series engine flame-outs - advice to aircrew  PA1716/5/11/3/10  21 August 1980
Expand   Olympus 300 flame-outs: Olympus 301. Advice on what to do in the event of a surge and flame-out in normal flight conditions  PA1716/5/11/3/11  11 August 1980
Expand   Olympus 300 flame-outs: Olympus 301. Engine 900014 its history from 2 November 1962 to 11 June 1980  PA1716/5/11/3/12  27 August 1980
Expand   Olympus 301 flame-outs: Rolls-Royce Memo. Visit to RAF Waddington re. Olympus 301  PA1716/5/11/3/13  29 July 1980 - 1 August 1980
Expand   Olympus 301 flame-outs: Vulcan B.Mk.2 XL389  PA1716/5/11/3/14  1965 - 1980
Expand   Bristol Siddeley: Olympus B.O1.21 turbojet engine  PA1716/5/11/3/15  August 1960
Expand   Advanced Notification of EMC decisions to Rolls-Royce Coventry  PA1716/5/11/3/16  25 March 1981
Expand   RAF Air diagram 8040: Olympus Mk.301 ECU working cycle conditions and air system  PA1716/5/11/3/17  January 1965
Expand   Bristol Siddeley: Olympus 320 TSR.2 engine & reheat unit flight specification. MoA Contract Ref.KG/M/090/CB(a) Issue 14  PA1716/5/11/3/18  4 January 1965
Expand   Bristol Siddeley Engines Limited: Olympus MK.320 TSR.2 final technical report and development contracts  PA1716/5/11/3/19  21 September 1965
Expand   Bristol Aero Engines Limited. Bristol Gas Turbines: Olympus Mk.200 installation data. Mks. 200, 201  PA1716/5/11/3/20  14 July 1958
No further details   Jets come down to earth: RB 211 unit efficiency allows mid merit prospect  PA1716/5/11/3/21  1973 - 1981
No further details   Rolls-Royce Ltd and the RB 211 Aero-engine - presented to Parliament by the Secretary of State for Trade and Industry  PA1716/5/11/3/22  1972
No further details   The aero deprived gas generator as a prime mover for Gas and Oil Transmission, by H.J. Prince  PA1716/5/11/3/23  c. 1970s
No further details   Presentation Summary: Commercial aero engine developments  PA1716/5/11/3/24  April 1982
No further details   Brochure: RB.211 in Lockheed Tristar, Propulsion System Maintainability  PA1716/5/11/3/25  July 1971
No further details   Customer Training Centre: Course Notes - RB.211  PA1716/5/11/3/26  23 January 1973
No further details   Brochure: Progress on the RB.211  PA1716/5/11/3/27  1971
No further details   Customer Training Centre: Course Notes - Rb.211  PA1716/5/11/3/28  1973
No further details   Brochure: RB.211 in Lockheed Tristar, Propulsion System Maintainability  PA1716/5/11/3/29  August 1980
No further details   Brochure: RB.211 in Lockheed Tristar, Propulsion System Maintainability  PA1716/5/11/3/30  December 1971
No further details   Brochure: RB211-524, further improving the product  PA1716/5/11/3/31  September 1984
No further details   Brochure: RB211-524 for the Lockheed L1011 Tristar  PA1716/5/11/3/32  October 1977
No further details   Brochure: RB211 - Powerful, clean, quiet...  PA1716/5/11/3/33  July 1972
No further details   Brochure: RB211  PA1716/5/11/3/34  November 1981
No further details   Leaflet: A 300B - being built today, in service tomorrow  PA1716/5/11/3/35  c. 1970s
No further details   Technical Features: Rolls-Royce RB.207/211 three shaft turbofans  PA1716/5/11/3/36  May 1968
Expand   Bristol Gas Turbines: Olympus 593 Concorde engine  PA1716/5/11/4  1961 - 1979
Expand   Concorde publicity material  PA1716/5/11/5  1975 - 1980
Expand   Olympus gas turbine aero engine school: From Bristol Aero-Engines Limited to Rolls-Royce/SNECMA  PA1716/5/11/6  1950 - 1963
Expand   Olympus gas turbine industrial engines  PA1716/5/11/7  1959 - 1981
Expand   Olympus Industrial gas turbine engines. Hams Hall & later power stations  PA1716/5/11/8  1962 - 1976
Expand   Olympus Marine gas turbine engines  PA1716/5/11/9  [n.d.]
Expand   Olympus 593 Industrial development  PA1716/5/11/10  1963 - 1978
Expand   Olympus 593 Industrial development. Press cuttings  PA1716/5/11/11  1971 - 1998
Expand   Rolls-Royce Customer Training Centre Ansty: Course notes  PA1716/5/11/12  1965 - 1978
Expand   Bristol Siddeley Power Division: Outside Erection Department - Power station master log books  PA1716/5/11/13  6 November 1963 - 27 November 1968
Expand   Industrial and Marine Division  PA1716/5/11/14  [n.d.]
Expand   Olympus Drawings and Photographs  PA1716/5/11/15  [n.d.]
Expand   Bristol Siddeley 17.5 / 20 MW Generating Set Fuel Control Sytem  PA1716/5/11/16  20th Cent.
Expand   Olympus Engines Reports and Engine Stress Investigations  PA1716/5/11/17  1959 - 1964
No further details   An Account of an Engineering Investigation into the Cause of an Aircraft Engine Failure  PA1716/5/11/18  30 January 1958
Expand   Olympus 320 Final Development Position  PA1716/5/11/19  15 June 1965
Expand   Avon Engine  PA1716/5/12  [n.d.]
Expand   M.45 Engine  PA1716/5/13  [n.d.]
Expand   Gnome Engine  PA1716/5/14  [n.d.]
Expand   Orpheus Engine  PA1716/5/15  [n.d.]
Expand   Pegasus Engine  PA1716/5/16  [n.d.]
Expand   Tyne Engine  PA1716/5/17  [n.d.]
Expand   Allison Engine  PA1716/5/18  [n.d.]
Expand   Orion Engine  PA1716/5/19  [n.d.]
Expand   Orenda Engine  PA1716/5/20  [n.d.]
Expand   Gas Turbine (General)  PA1716/5/21  [n.d.]
Expand   Adour Engine  PA1716/5/22  [n.d.]
Expand   RB 199 Engine  PA1716/5/23  [n.d.]
Expand   National Engineering Laboratory, East Kilbride  PA1716/5/24  [n.d.]
Expand   Spey Gas Generator  PA1716/5/34  [n.d.]
Expand   Product Support - Product Assurance Manual  PA1716/5/35  June 1979
Expand   Turbine Engine and Power Plant Design Materials  PA1716/5/36  1950s
Expand   Air Registration Board Notices  PA1716/5/37  1964 - 1967
Expand   General Requirements for the Overhaul of Gas Turbine Aero-Engines - Engine Change Units, Engine Modules and Jet Pipes  PA1716/5/38  1968 - 1975
No further details   Drawing Number Registers  PA1716/5/39  c.1960s - c.1970s
Expand   Helium Gas Turbine Plant for Gas Cooled Reactors  PA1716/5/40  November 1967
Expand   Proposal for Gas Tyrbine HTR  PA1716/5/41  May 1969
Expand   The Case for Closed-Cycle Gas Turbines with the High Temperature Helium-Cooled Nuclear Reactor  PA1716/5/42  November 1974
Expand   Guide to the AVRO Single-Engine Advanced Trainer aircraft  PA1716/5/43  c.1960s
Expand   Civil 'A' Nos  PA1716/5/44  c.1969
Expand   Internal Drawings Register  PA1716/5/45  c.1960s
Expand   Drawing Register Books Index  PA1716/5/46  c.1960
Expand   Part No. Registers  PA1716/5/47  [n.d.]
Expand   Unified Threads ?Register  PA1716/5/48  1950-1963
Expand   Compendium of Design and Development Information  PA1716/5/49  September 1954
Expand   Interim Report on Bending Fatiue Tests on Gear Teeth  PA1716/5/50  c.1960s
No further details   Armstrong Siddeley Motors Gas Turbine Production Order Book  PA1716/5/51  November 1953 - June 1954
Expand   Cost Analysis of the Development and Research Programme for the first 22 Weeks, April 1st to August 30th, of the current year 1950/1951  PA1716/5/52  2 October 1950
Expand   Cost Analysis of the Development and Research Programme for the first 30 weeks, April 1st to October 25th of the current year 1950/1951  PA1716/5/53  12 December 1950
Expand   Draft Sales Plan for submission to the Ministry of Supply  PA1716/5/54  18 January 1952
No further details   Serration Root Index and Photographs  PA1716/5/55  c.1960
Expand   Drawing for First Rotor Blade  PA1716/5/56  1973
Expand   Correspondence concerning visit of Mr E. Hawthorne and work on nuclear reactors  PA1716/5/57  1955
Expand   Reports on Gas Turbine Engines and Aircraft  PA1716/5/58  1958 - 1959
Expand   Letter from Peter Geliot to Dear Mr Harvey-Bailey  PA1716/5/59  1 October 1993
Expand   Armstrong Siddeley Gas Turbines  PA1716/5/60  c.1960s
Expand   An Introduction to Gas Turbines  PA1716/5/61  1949 - 1950
Expand   Reports on Icing Tests  PA1716/5/62  1956 - 1962
Expand   Laboratory Reports  PA1716/5/63  1952
Expand   Proposed Research Programme for year 1953 / 1954  PA1716/5/64  c.1953
Expand   Test Results for Turbine Blade Materials  PA1716/5/65  c.1980s
Expand   Diagram of Hydr. Torque Converter  PA1716/5/66  1956 - 1966
Expand   Nuclear Gas Turbines  PA1716/5/67  [n.d.]
Expand   Naval Marine Wing Note No. 20/69  PA1716/5/68  October 1969
Expand   Naval Marine Wing Note No. 21/69  PA1716/5/69  November 1969
Expand   Gas Turbines in the 1980's  PA1716/5/70  c.1977
Expand   General Material relating to Gas Turbines  PA1716/5/71  1969 - 1990
Expand   Small Gas Turbine Engines - The State of the Art in the World Today  PA1716/5/72  c.1955
Expand   Advanced Engineering - Archived Drawings  PA1716/5/73  November 1988
Expand   Proposal for a New 7 1/2 MW Vapour Turbine  PA1716/5/74  c.1966
Expand   Rolls-Royce SM1A & SM2B Gas Turbines for Marine Propulsion  PA1716/5/75  July 1977
Expand   Specification and Design of a Shore Trials Facility for C.A.H. Machinery  PA1716/5/76  c.1971
Expand   Guidance Notes for the Design of Gas Turbine Intakes and Exhausts for Ships  PA1716/5/77  1978
Expand   Fuel  PA1716/5/78  c.1951 - 1977
Expand   Fluidised Bed Gas Generation Presentation Overhead Projections and Photographs  PA1716/5/79  c.1978
Expand   Rolls-Royce Range of Gas Turbine Generating Sets  PA1716/5/80  14 November 1975
Expand   Glacier Bearings in Gas Turbine Generating Sets  PA1716/5/81  1970
No further details   Rolls-Royce Gas Turbines for Electrical Generation and Gas and Oil Pumping  PA1716/5/82  1977
Expand   'A New Look in Gas Transmission'  PA1716/5/83  October 1966
Expand   2,500 H.P. Recuperative Gas Turbine  PA1716/5/84  October 1965
Expand   Free Power Turbine Dart Engine for Rail Traction - Development Plan  PA1716/5/85  May 1968
Expand   General Description of Dart Free Power Turbine Unit for Railway Traction  PA1716/5/86  c.1968
Expand   Proposals for Hih Temperature Turbines  PA1716/5/87  2 January 1969
Expand   Gas Turbine Power for Railways Report  PA1716/5/88  1967
Expand   Correction Chart for Gas Turbine Engines  PA1716/5/89  March 1952
Expand   Bristol Siddeley Centaur Marine Gas Turbine  PA1716/5/90  1966
Expand   Centaur Marine Gas Turbine  PA1716/5/91  November 1966
Expand   A Survey of Gas Generator Prospects  PA1716/5/92  November 1957
Expand   Super Sonic Nozzles for Gas Turbines  PA1716/5/93  12 January 1947
Expand   Operation of Gas Turbines on Liquid Hydrogen  PA1716/5/94  1981
Expand   Windage Losses of Small Turbines  PA1716/5/95  22 September 1953
Expand   Dimensional Analysis as applied to the Gas Turbine  PA1716/5/96  12 June 1950
Expand   Gas Turbunes for ACVs - past, present and future  PA1716/5/97  19 November 1964
Expand   List of British and Canadian Gas Turbine Aero Engines  PA1716/5/100  10 May 1950
No further details   Photographs and Drawings of Camm Engines, Propulsion Engines, Friction Drive and Cyclye Systems  PA1716/5/101  c.1967
Expand   Estimation of Aircraft Intake Losses at Take-Off and Subsonic Flight  PA1716/5/102  14 September 1959
Expand   The Performance of a Small Axial Flow Turbine  PA1716/5/103  15 June 1962
Expand   A Graphical Method of Obtaining Turbine Blade Loss Coefficients  PA1716/5/104  15 Aoril 1959
Expand   The Performance of a Small Axial Flow Turbine  PA1716/5/105  10 August 1962
Expand   The Effect of Pitch Chord Ratio on the Perfoamnce of a Single Stage Turbine  PA1716/5/106  14 January 1954
Expand   Feasibility Study - Model Centripetal Turbine Tests  PA1716/5/107  c.1966
Expand   10 Stage Research Compressor Profile Producer  PA1716/5/108  22 November 1960
Expand   The S.R.D.A.S. Brochure  PA1716/5/109  c.1969 - 1972
Expand   The S.R.D.A.S. Coding Manual  PA1716/5/110  c.1968 - 1972
Expand   Gas Turbine Reduction Gear Data Spur Gears  PA1716/5/111  1961
Expand   Accessories  PA1716/5/112  [n.d.]
Expand   Blackburn Gas Turbines  PA1716/5/113  c.1960
Expand   Engine Drawings  PA1716/5/114  c.1960s

The contents of this catalogue are the copyright of Coventry Archives
Rights in the Access to Archives database are the property of the Crown, © 2001-2013

The records described on this page are held by Coventry Archives