Liquid fuel atomiser

Claim 2

A liquid fuel atomiser comprising a body within which are defined a fuel supply passage, a swirl chamber and annularly-distributed internal passages for fuel to flow from said supply passage to said swirl chamber to rotate therein about an axis of rotation passing through said chamber, an orifice defined by said body coaxially with said axis, said orifice having an inlet opening communicating with said chamber and an outlet opening from which fuel exits from said orifice in a substantially hollow diverging frusto-conical pattern, an external wall having an inner diameter greater than said outlet opening being formed on said body coaxially with said axis immediately downstream, relative to fuel flow, of said orifice and external formation extending both parallel to said axis and radially inwardly from said wall at circumferentially spaced-apart positions about said wall, said external wall being continuous both in a direction parallel to said axis and in a circumferential direction, and each of said radially inwardly extending formations terminating in an inward edge, the radial distance between generally opposite inward edges thereof being greater than the diameter of the outlet opening of said orifice, thereby to interact with the fuel exiting from said orifice to alter the shape of said frustoconical pattern into a split pattern.

Claim 3

An atomiser according to claim 1, which a fuel return passage is defined within said body, said fuel return passage being in communication with said swirl chamber whereby fuel circulates through said body.

Claim 4

An atomiser according to claim 1 in which a lance is mounted within said body coaxially with said axis for movement therealong between a first position in which the tip of said lance closes said orifice and a second position in which the tip of said lance is withdrawn from said orifice.

Claim 5

An atomiser according to claim 1, in which said orifice is bounded by a plain cylindrical surface opposite ends of which define respectively said inlet opening and said outlet opening.

Claim 6

An atomiser according to claim 1, in which said external formations change said frusto-conical pattern into a pattern having discrete lobes.

Claim 7

An atomiser according to claim 1, in which the cross-section of each said external formation in a plane normal to said axis tapers in a direction substantially towards said axis.

Claim 8

An atomiser according to claim 1, in which said external formations are located at positions concentric with said axis.

Claim 9

An atomiser according to claim 1, in which the sides of said external formations are bounded by plane surfaces.

Claim 10

An atomiser according to claim 1, in which the sides of said external formations are bounded by surfaces which are concave when viewed in a direction parallel to said axis.

Claim 11

An atomiser according to claim 1, in which the junctions of said surfaces of said external formations with one another or with radially inner surfaces comprise sharp corners.

Claim 12

An atomiser according to claim 1, in which said external formations each have a respective radially inner surface lying on a circle coaxial with said axis.

Claim 13

An atomiser according to claim 11, in which the circumferential extent of each said radially inner surface is relatively small whereby the shape of said frusto-conical pattern is changed by radial splitting of said pattern.

Claim 14

An atomiser according to claim 11, in which the circumferential extent of each said radially inner surface is relatively large whereby the shape of said frusto-conical pattern is changed by deflecting portions of the fuel film.

Claim 15

An atomiser according to claim 1, in which said external formations each have a respective radially inner surface which is part-circular and has a curvature opposite to the curvature of a circle concentric with said axis.

Claim 16

An atomiser according to claim 14, in which the sides of the external formations are bounded by surfaces tangential to said part-circular radially inner surface.

Claim 17

An atomiser according to claim 1, in which said external formations have radially innermost extents lying on a common circle concentric with said axis.

Claim 18

An atomiser according to claim 1, in which the radially innermost extents of said external formations are located no closer to said axis than a circle having a radius (R) equal to 1.25 times the radius of said orifice and said external formations have a minimum height (H) greater than 0.45 R tan (90-α/2) where α is the included cone angle of said frusto-conical pattern.

Claim 19

A liquid fuel atomiser comprising a body within which are defined a fuel supply passages, a swirl chamber and annularly-distributed internal passages for fuel to flow from said supply passage to said swirl chamber to rotate therein about an axis of rotation passing through said chamber, an orifice defined by said body coaxially with said axis, said orifice having an inlet opening communicating with said chamber and an outlet opening from which fuel exits from said orifice in a substantially hollow diverging frustoconical pattern, an external wall having an inner diameter greater than said outlet opening being formed on said body coaxially with said axis immediately downstream, relative to fuel flow, of said orifice and external formations extending both parallel to said axis and radially inwardly from aids wall at circumferentially spaced-apart positions about said wall, said external wall being continuous both in a direction parallel to said axis and in a circumferential direction, and each of said radially inwardly extending formations terminating in an inward edge, all said inward edges together defining a circle which is coaxial with and has a diameter greater than the outlet opening of said orifice, thereby to interact with the fuel exiting from said orifice to alter the shape of said frusto-conical pattern into a split pattern.

Claim 20

A liquid fuel atomiser comprising a body within which are defined a fuel supply passages, a swirl chamber and annularly-distributed internal passages for fuel to flow from said supply passage to said swirl chamber to rotate therein about an axis of rotation passing through said chamber, an orifice defined by said body coaxially with said axis, said orifice having an inlet opening communicating with said chamber and an outlet opening from which fuel exits from said orifice in a substantially hollow diverging frustoconical pattern, an external wall having an inner diameter greater than said outlet opening being formed on said body coaxially with said axis immediately downstream, relative to fuel flow, of said orifice and external formations extending both parallel to said axis and radially inwardly from aids wall at circumferentially spaced-apart positions about said wall, said external wall being continuous both in a direction parallel to said axis and in a circumferential direction, and each of said radially inwardly extending formations terminating in an inward edge, all said inward edges together defining a circle which is coaxial with and has a diameter greater than the outlet opening of said orifice, thereby to interact with the fuel exiting from said orifice to alter the shape of said frusto-conical pattern into a split pattern.