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Institution

Rolls-Royce Limited

About: Rolls-Royce Limited is a based out in . It is known for research contribution in the topics: Gas compressor & Rotor (electric). The organization has 624 authors who have published 623 publications receiving 10751 citations. The organization is also known as: Rolls Royce Limited.


Papers
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Patent
03 May 1978
TL;DR: In this article, the operation of an electrolytic machine tool is monitored over equal periods of time, so as to detect the number of short circuits, if any, which occur.
Abstract: The operation of an electrolytic machine tool is monitored over equal periods of time, so as to detect the number of short circuits, if any, which occur. Where a given number of short circuits are detected in any one time period, a signal is derived from the last of that number and utilised to switch off the electrode traverse motor through power and electrolyte flow are maintained to enable sludge clearance and observation of the resultant reduction in short circuits.

8 citations

Patent
20 Oct 1978
TL;DR: In this article, the rotor and stator of a turbine a gaz are modelled as cerclees d'un bandage, and a turbulence sopposant a la fuite des gaz chauds moteurs par l'entrefer a.
Abstract: L'invention concerne un dispositif destine a ameliorer l'etancheite entre le rotor et le stator d'une turbine a gaz. Les aubes 22 du rotor sont cerclees d'un bandage 24 comportant un flasque radial 26 formant joint avec le stator 28 et en amont duquel ce stator est perce d'orifices 30 d'alimentation d'air froid creant au voisinage du joint une turbulence s'opposant a la fuite des gaz chauds moteurs par l'entrefer a. Le dispositif ameliore le rendement de la turbine et abaisse la consommation de carburant du moteur.

8 citations

Patent
10 Jan 1978
TL;DR: In this paper, a ducted fan gas turbine power plant consists of a core gas generator, which may be a single or two-shaft gas generator and which drives a fan at the downstream end of the power plant.
Abstract: A ducted fan gas turbine powerplant consists of a core gas generator, which may be a single or two-shaft gas generator, and which drives a fan at the downstream end of the powerplant. The exhaust from the gas generator is mixed with flow in the fan duct and the fan operates on the mixed stream as a working fluid.

8 citations

Patent
10 Dec 1982
TL;DR: In this paper, a pyrometer which senses blade temperature in the engine is also used to detect the onset of an engine surge, and if the duration exceeds a given time, set by the monostable, an output from the duration detector actuates a fuel chopper to minimize the effect of the surge.
Abstract: A pyrometer which senses blade temperature in the engine as also used to detect the onset of an engine surge. The output of the pyrometer 2 (FIG. 1) passes to a level detector unit, comprising a differential amplifier and a constant reference voltage, and which produces an output when the pyrometer signal exceeds the reference voltage. A duration detector comprising a monostable 12, inverter 14, delay line 18 and AND gate 16 determines the duration of the excess level signal and if the duration exceeds a given time, set by the monostable, an output from the duration detector actuates a fuel chopper to minimize the effect of the surge.

8 citations

Patent
01 Apr 1971
TL;DR: The blocker flaps in the fan duct of a gas turbine ducted fan engine are mounted for simultaneous pivoting across the fan and movement bodily downstream thereof so as to attain the required throat area for the subsequently reversed flow of fan air through the reverser aperture in the Fan cowl as mentioned in this paper.
Abstract: The blocker flaps in the fan duct of a gas turbine ducted fan engine are mounted for simultaneous pivoting across the fan duct and movement bodily downstream thereof so as to attain the required throat area for the subsequently reversed flow of fan air through the reverser aperture in the fan cowl.

8 citations


Authors
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Performance
Metrics
No. of papers from the Institution in previous years
YearPapers
20211
20201
20131
20111
20062
19931