Abstract: A laundry treatment composition which comprises a surfactant and from 0.0001 to 0.1 wt % of a combination of dyes which together have a visual effect on the human eye as a single dye having a peak absorption wavelength on cotton of from 540 nm to 650 nm, preferably from 570 mn to 630 mn, the combination comprising a photostable dye which is substantive to cotton.

Abstract: A laundry treatment composition which comprises a surfactant and from 0.0001 to 0.1 wt % of a combination of dyes which together have a visual effect on the human eye as a single dye having a peak absorption wavelength on cotton of from 540 nm to 650 nm, preferably from 570 nm to 630 nm, the combination comprising a photostable dye which is substantive to cotton.

Abstract: A laundry treatment composition which comprises a surfactant and from 0.0001 to 0.1 wt % of a combination of dyes which together have a visual effect on the human eye as a single dye having a peak absorption wavelength on cotton of from 540 nm to 650 nm, preferably from 570 mn to 630 mn, the combination comprising a photostable dye which is substantive to cotton.

Abstract: A particulate laundry detergent composition having an equilibrium relative humidity value at 25° C. and 1 atmosphere of at least 10% and comprising an effervescent granule, the effervescent granule comprising an acid source, a carbonate source and a desiccant is provided. The granules are stable even though they are contained within a humid environment.

Abstract: A particulate laundry detergent composition comprising effervescent granules, at a level of from 0.1 to less than 2 wt %, the effervescent granules comprising (a) from 20 to 80 wt % of an acid source and (b) from 20 to 80 wt % of a carbonate source is provided. Surprisingly the effervescent granules provide dispensing benefits at very low concentration levels.

Abstract: An effervescent granule for use in particulate detergent compositions which comprises (a) a particulate acid source; and (b) a particulate carbonate source characterised in that the ratio of the d50 particle size of the acid source to the carbonate source is from less than 2:1 to greater than 1:1 is provided. The granules are surprisingly more effective if the particle sizes of the reacting constituents are similar.

Abstract: An effervescent granule for use in particulate detergent compositions characterised in that it comprises an acid source, a carbonate source and solid surfactant particles is provided.

Abstract: An antireflective multilayer coating including a thin film optical coating as well as a method for producing such a coating are provided. The thin film optical coating includes a layer of sol-gel derived cerium oxide, silicon dioxide, and at least one oxide of a transition metal selected from Group IIIB through Group VIB of the Periodic Table which is capable of providing a refractive index of at least about 1.90. The thin film may optionally include colloidal gold particles. A method is provided for producing a thin film optical coating including a layer of sol-gel derived cerium oxide, silicon dioxide, and at least one oxide of a transition metal selected from Group IIIB through Group VIB of the Periodic Table by immersing a substrate in a solution comprising cerium nitrate hexahydrate, an alcohol and a chelating agent, withdrawing the substrate from the solution and heat treating the coated substrate to form the metal oxides.

Abstract: A ducted fan gas turbine powerplant is mounted to aircraft structure via a single plane mounting which comprises a single peripheral array of struts which connect the core gas generator, the fan cowl and the aircraft structure. The structure which connects the struts to the core gas generator is extended downstream of the array of struts and terminates in a plain bearing. A downstream portion of the core gas generator includes a cylindrical portion which is in sliding engagement with the plain bearing, so that radial forces generated by the movement arm, the fulcrum of which coincides with the strut connection with the core gas generator are transmitting via the struts to the aircraft structure and relative axial expansion between the extension and the core gas generator is enabled.

Abstract: A device for controlling the clearance between the blade tips of a gas turbine engine turbine rotor and associated segmented shrouds comprises a control ring which is secured to the engine casing by a plurality of dowels. The control ring is supplied with cooling fluid to its hollow interior and is covered with a thermally insulating layer, whereby the rate of movement of the shroud segments can be maintained substantially equal to that of the adjacent turbine rotor.