Rolls-Royce Archives
From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
Rolls-Royce Experimental Archives                
Choose Archive


Browsing Records        Page 2172 of 2367        Sort by   Box   Date   Description

Filter      from        to             identifier   [all]
DescriptionDateIdentifier
Test results for engine cooling system components, including radiator calibration and condenser performance.19th Dec 1932Box 179b \ 2  img236
Condenser performance tests, comparing plain and finned condensers and methods of condensate return.30th Dec 1932Box 179b \ 2  img237
Condenser testing, detailing the replacement of a blow-off valve and conclusions on the advantages of finned designs.30th Dec 1932Box 179b \ 2  img238
Graph comparing coolant performance in a Hawker Fury radiator using water and ethylene glycol mixtures.28th Dec 1932Box 179b \ 2  img239
Blueprint detailing the test arrangement of a leading edge condenser on a High Speed Fury aircraft.28th Dec 1932Box 179b \ 2  img240
Diagram of the method used for returning condensate to the header tank for the High-Speed Fury's centre section leading-edge condenser.28th Dec 1932Box 179b \ 2  img241
Full-size section drawing of a leading edge condenser with fins.20th Dec 1932Box 179b \ 2  img242
Arrangement of a model condenser in a wind stream.20th Dec 1932Box 179b \ 2  img243
Graph showing the calibration curve for Brass Constantan thermo-couples.20th Dec 1932Box 179b \ 2  img244
Graph showing the relationship between heat flow and the surface temperature of a condenser.20th Dec 1932Box 179b \ 2  img245
Graph plotting cooling over a leading edge condenser (without fins) against air speed on logarithmic scales.20th Dec 1932Box 179b \ 2  img246
Graph comparing the cooling performance of plain versus finned condensers against air speed.20th Dec 1932Box 179b \ 2  img247
Graph illustrating the relationship between servo multiplication of torque and brake force distribution for I.M. Brakes.20th Dec 1932Box 179b \ 2  img248
Interim report on tests conducted on leading edge condensers.20th Dec 1932Box 179b \ 2  img249
Tests on leading edge condensers, including temperature measurements and wind stream analysis.20th Dec 1932Box 179b \ 2  img250
Schematic diagram and calculations for a brake layout.20th Dec 1932Box 179b \ 2  img251
Partial blueprint showing a mechanical component with annotations.20th Dec 1932Box 179b \ 2  img252
Blueprint showing two views of a 66-inch panel with internal partitions and a scrap view detail.20th Dec 1932Box 179b \ 2  img253
Blueprint for a fabricated brass component with stiffeners.20th Dec 1932Box 179b \ 2  img254
Blueprint showing a detail of a condenser shell and a vent connection made of brass.20th Dec 1932Box 179b \ 2  img255
Blueprint detailing the construction and dimensions of a condenser, including fin placement and specifications.20th Dec 1932Box 179b \ 2  img256
Blueprint of an outline section for an experimental component made from brass sheet.20th Dec 1932Box 179b \ 2  img257
Drawing for a leading edge condenser, detailing the arrangement of internal stiffeners and fins.14th Nov 1932Box 179b \ 2  img258
Schematic for a brass condenser component with dimensions and assembly instructions.14th Nov 1932Box 179b \ 2  img259
Test results and further experiments on a damper governor control system.2nd Jan 1933Box 179b \ 3  img001
Test report on damper governor control, detailing pressure and time lag measurements.30th Dec 1932Box 179b \ 3  img002
Graph plotting valve spring rating against control movement percentage for the R.R.S 269 hand control system at various RPMs.23th Dec 1932Box 179b \ 3  img003
Four performance graphs for a J III Rear 40/40 LB Low Pressure double diaphragm system at various RPMs.23th Dec 1932Box 179b \ 3  img004
Tests and standardisation of an air silencer for the 25 HP carburetter.4th Jan 1933Box 179b \ 3  img005
Decision to order and standardise a new type of shock absorber for the 20/25 HP model.4th Jan 1933Box 179b \ 3  img006
Flight experience and proposed modifications for the Goshawk I carburettor's accelerating pump.4th Jan 1933Box 179b \ 3  img007
Continued description of a fuel pump plunger system's operation and comparison with a spring-loaded system.4th Jan 1933Box 179b \ 3  img008
Blueprint diagram and explanation of the Goshawk Carburettor's accelerating pump.3rd Jan 1933Box 179b \ 3  img009
Cross-sectional diagram of a pump assembly, noting the filling cap, piston, and spring.3rd Jan 1933Box 179b \ 3  img010
Preliminary rig test report for a combined pump and injector unit.6th Jan 1933Box 179b \ 3  img011
Preliminary rig test results for a combined pump and injector for a four-stroke C.I. engine.6th Jan 1933Box 179b \ 3  img012
Specifications and performance analysis of a fuel pump, including plunger details and injection pressure.6th Jan 1933Box 179b \ 3  img013
Fuel injection pump calculations, test rig setup, and initial performance results.6th Jan 1933Box 179b \ 3  img014
Test report detailing modifications and performance analysis of a fuel injection pump.6th Jan 1933Box 179b \ 3  img015
Fuel pump delivery calculations, performance testing, and future development plans.6th Jan 1935Box 179b \ 3  img016
Design improvements for injector pumps, specifically the relief passage and needle valve.2nd Jan 1935Box 179b \ 3  img017
Graph showing the discharge control position curve for a combined pump and injector.2nd Jan 1935Box 179b \ 3  img018
Blueprint graph of a combined pump and injector delivery curve, plotting injection quantity against pump speed.2nd Jan 1935Box 179b \ 3  img019
Cross-sectional blueprint diagram of a pump mechanism, labelled as Figure 1.30th Oct 1940Box 179b \ 3  img020
Blueprint cross-section of a fuel pump and injector.30th Oct 1940Box 179b \ 3  img021
Technical report on issues with the Peregrine clutch, specifically concerning slipping, torque, and casing distortion.7th Jan 1933Box 179b \ 3  img022
Continued analysis of clutch slipping and overheating, with a comparative table of different clutch specifications.7th Jan 1933Box 179b \ 3  img023
Comparison table of specifications for three different clutch types.7th Jan 1933Box 179b \ 3  img024
Modifications to improve the power output of a Bensport saloon engine.11th Jan 1933Box 179b \ 3  img025
Results of engine modifications on power output and reliability.11th Jan 1933Box 179b \ 3  img026
Performance graph comparing power output modifications for Mr. Bensport's J1 engine car.11th Jan 1933Box 179b \ 3  img027
Graph of Brake Horse Power (BHP) against RPM, with camshaft timing diagrams for a standard 25 HP and a Bensport camshaft.12th Jan 1933Box 179b \ 3  img028
Blueprint for a modification to a Bensport J.I. cylinder head, involving machining and trepanning.12th Jan 1933Box 179b \ 3  img029
Steering positions and the suitability of the 'E' Type steering column for the Peregrine model.11th Jan 1933Box 179b \ 3  img030
Acceptance test report for a Kestrel II.S. engine intended for a high-speed 'Fury' aircraft.12th Jan 1933Box 179b \ 3  img031
Engine power curves, adjustments, and performance tests.12th Jan 1933Box 179b \ 3  img032
Final engine test graph for a Kestrel II S engine, showing power curves, boost, and fuel consumption.10th Jan 1933Box 179b \ 3  img033
Visit to Curtiss Wright in Paterson, New Jersey, discussing engine design and ethylene glycol cooling.14th Jan 1931Box 179b \ 3  img034
Aircraft engine development, discussing cooling systems, brazing techniques, and competitor engines.14th Jan 1931Box 179b \ 3  img035
Notes on the design and performance of rotor, diffuser, piston, and bearing components.14th Jan 1931Box 179b \ 3  img036
Technical notes on the inspection and design of various engine components.1st Sep 1932Box 179b \ 3  img037
Comparative analysis of fuel, engine performance, detonation, and airscrew technology.1st Sep 1932Box 179b \ 3  img038
Technical report discussing motor mounting, propellers, mechanical failures, and observations on various aircraft.29th Jan 1930Box 179b \ 3  img039
Blueprint detailing features of Curtiss Wright engine construction.29th Jan 1930Box 179b \ 3  img040
Diagrams showing a piston profile, big end bearings, and a master rod arrangement.3rd Jan 1929Box 179b \ 3  img041
Diagrams for a radio screened ignition system and streamlined cowling with a spinner.24th Jan 1935Box 179b \ 3  img042
Investigation into fuel boiling and freezing problems with a Goshawk carburetter on a Kestrel engine.17th Jan 1933Box 179b \ 3  img043
Test report detailing the investigation into fuel boiling within a carburetter and its effects on engine performance.17th Jan 1931Box 179b \ 3  img044
Tests on fuel boiling and temperature changes within a carburetter floatchamber under various engine conditions.17th Jan 1933Box 179b \ 3  img045
Test report on carburetter water jacketing, fuel temperatures, and flooding causes.17th Jan 1931Box 179b \ 3  img046
Graph investigating fuel boiling in a Goshawk carburetter, showing fuel and water temperatures against engine RPM.1st Feb 1933Box 179b \ 3  img047
Chart investigating fuel boiling in a Goshawk carburettor on a Kestrel 27 engine.17th Jan 1934Box 179b \ 3  img048
Graph showing an investigation of fuel boiling on a Goshawk carburetter for a Kestrel 27 engine.6th Jul 1932Box 179b \ 3  img049
Performance of a Borg & Beck clutch for the 20/25 HP engine and related patent obligations.17th Jan 1933Box 179b \ 3  img050
Letter from Borg & Beck Company Ltd. concerning collaboration on clutch features and materials.12th Jan 1933Box 179b \ 3  img051
The condition of shock dampers from a 10,000-mile trial car.19th Jan 1933Box 179b \ 3  img052
Inspection report detailing the condition and wear of various engine components.19th Jan 1933Box 179b \ 3  img053
Analysis of external pressure cylinders, glands, and dampers, noting their condition and weakest features.19th Jan 1933Box 179b \ 3  img054
Confirming an investigation into substituting dole fittings for banjos on the governor control for shock dampers.23th Jan 1933Box 179b \ 3  img055
US motor show, focusing on a new G.M. body ventilation system and its potential application.23th Jan 1933Box 179b \ 3  img056
Letter from New York detailing new features at a Motor Show, including automatic systems and the 'Fisher' No-Draft ventilating scheme.23th Jan 1933Box 179b \ 3  img057
Review of innovations in radiator fans, valve springs, and frame stiffeners from other car manufacturers.23th Jan 1933Box 179b \ 3  img058
Flexible engine mounting and a detailed sketch of an aero screened ignition system.23th Jan 1933Box 179b \ 3  img059
Outlining a travel and meeting schedule across various US cities.23th Jan 1933Box 179b \ 3  img060
Road test of a car with a mock-up J.1 unit, evaluating its performance and handling.23th Jan 1933Box 179b \ 3  img061
Covering memo for a report on the Peregrine 2 engine after 12,000 miles of testing in France.24th Jan 1933Box 179b \ 3  img062
The condition of engine FER.11 after being dismantled following a 12,000 miles test.24th Jan 1933Box 179b \ 3  img063
Inspection report detailing wear and issues with an automatic governor, water pump, and clutch assembly.24th Jan 1933Box 179b \ 3  img064
Inspection report detailing wear on various engine and drivetrain components.24th Jan 1933Box 179b \ 3  img065
The condition of vehicle components following a strip-down inspection.24th Jan 1933Box 179b \ 3  img066
Faults with hydraulic dampers, axle brackets, and the chassis frame.24th Jan 1933Box 179b \ 3  img067
Photographic record of various upper and lower engine bearing halves.25th Jan 1933Box 179b \ 3  img068
Proposing to standardize a larger 28-gallon petrol tank for the Phantom II model to increase its range.25th Jan 1933Box 179b \ 3  img069
Development, modifications, and production plans for the Bensport car.27th Jan 1933Box 179b \ 3  img070
Production economics of the proposed Bentsport model and the strategy for the Bentley business.27th Jan 1933Box 179b \ 3  img071
Flight tests of a steam-cooled Hart aircraft, focusing on modifications to the cooling system to prevent freezing.30th Jan 1933Box 179b \ 3  img072
Proposal to build and test a 'HASL' pump for the Kestrel.24th Sep 1934Box 179b \ 3  img073
Schematic diagram of the Steam Cooled Hart system.31th Jan 1933Box 179b \ 3  img074
Graph plotting various temperatures against altitude during a climb test of a Hart K.1102 aircraft.18th Feb 1923Box 179b \ 3  img075
Lever test rig failure, where the case cracked and bearings seized due to a hollow shaft deforming.30th Jan 1933Box 179b \ 3  img076


Copyright Sustain 2025, All Rights Reserved.    whatever is rightly done, however humble, is noble
An unhandled error has occurred. Reload 🗙