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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
06 Apr 1977
TL;DR: In this article, a pair of complementary rod electrodes are added to the circuitry of an electro-discharge machining system in which holes are drilled into existing passages in a workpiece, by other machining electrodes.
Abstract: A pair of complementary rod electrodes, one of which machines the other, is added to the circuitry of an electro-discharge machining system in which holes are drilled into existing passages in a workpiece, by other machining electrodes. When a machining electrode breaks into the passage, the resulting sharp increase in electrical potential thereacross is prevented from affecting the electrode advance control mechanism because the mechanism only senses the low potential across the continuously machining rod electrodes. Thus the electrode which machines the workpiece is prevented from rapidly traversing the passage and machining the opposite wall.

11 citations

Patent
27 Mar 1970
TL;DR: In this article, a method of producing a fibrous article comprising employing at least one former at least of whose surfaces is provided with substantially parallel recesses, laying a plurality of transverse lengths of fibrous material over the former so that the said transverse length extend transversely of the recesses and are spaced from each other longitudinally of the re-sealings.
Abstract: The invention concerns a method of producing a fibrous article comprising employing at least one former at least one of whose surfaces is provided with substantially parallel recesses, laying a plurality of transverse lengths of fibrous material over the former so that the said transverse lengths extend transversely of the recesses and are spaced from each other longitudinally of the recesses, laying a longitudinal length of fibrous material in each said recess so that the said longitudinal lengths extend over the said transverse lengths and force respective portions of the latter into the recesses, forming at least one fibrous assembly having the shape of the respective said surface by bonding the transverse and longitudinal lengths together while the latter are on the former, and effecting relative separation between the said assembly and the former.

11 citations

Patent
12 Nov 1981
TL;DR: In this article, a seeding tube allows magnetic powder to be supplied to the gap to make good any loss of powder, and the fin of the turbine is maintained approximately the same regardless of the position of the fin in the gap.
Abstract: A seal for use in rotating machinery such as a gas turbine engine comprises two pole pieces attached to the engine casing and defining a gap in which a magnetic powder is held by a magnetic field generated by a permanent magnet, electro-magnet or a combination of the two. The non-magnetic fins of the adjacent rotor (e.g. turbine blades), extend into the gap and distort the magnetic field so that while there is a small clearance between the fin and the powder, this small clearance can be maintained approximately the same whatever the position of the fin in the gap. A seeding tube allows magnetic powder to be supplied to the gap to make good any loss of powder.

11 citations

Patent
Frank Cork1
14 Dec 1979
TL;DR: In this paper, a method of removing aluminium containing alloy coatings from nickel or cobalt base alloy substrates in which the coated substrate is immersed in an aqueous mixture of nitric and sulphamic acids until coating dissolution is complete.
Abstract: A method of removing aluminium containing alloy coatings from nickel or cobalt base alloy substrates in which the coated substrate is immersed in an aqueous mixture of nitric and sulphamic acids until coating dissolution is complete. A solution containing 5 to 30% vol./vol. nitric acid and from 5 to 30% wt./vol. sulphamic acid is preferred.

11 citations

Patent
05 Dec 1969
TL;DR: In this article, a gas turbine engine nozzle assembly for landing or taking off is described, where the nozzle is variable between a cruise configuration in which it has a section which is circular or of regular polygonal form and a noise reduction configuration, in which the nozzle dimension in one direction is substantially greater than that in a perpendicular direction.
Abstract: A nozzle assembly for a gas turbine engine intended to effect noise reduction when the aircraft carrying the nozzle is landing or taking off. The nozzle is variable between a cruise configuration in which it has a section which is circular or of regular polygonal form and a noise reduction configuration in which the nozzle dimension in one direction is substantially greater than that in a perpendicular direction. A pair of clamshell doors effect the change in configuration for the nozzle.

11 citations


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