Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
260 words
A hollow, longitudinally extending airfoil including a cooled wall having an outer surface defining a pressure and suction surface of said airfoil, said pressure and suction surfaces adapted to have a hot gas stream flowing thereover in a downstream direction substantially perpendicular to said longitudinal direction, said cooled wall also having an inner surface adapted to define a portion of a coolant compartment for receiving coolant therein under pressure, the improvement comprising: a longitudinally extending cylindrical diffuser channel formed within said wall defining a cylindrical surface and having an axis; a pair of spaced apart, facing side surfaces forming a slot within said wall, said side surfaces intersecting said outer surface at a shallow angle to form a longitudinally extending slot outlet, and intersecting said channel cylindrical surface to form a slot inlet extending longitudinally substantially the full length of said cylindrical channel, said slot being oriented to direct coolant fluid therefrom as a continuous, longitudinally extending film over said outer surface downstream of said slot outlet; a single one of said slots intersecting each channel; and at least one metering passage formed within said wall for controlling the rate of flow of coolant fluid into said slot, said metering passage intersecting said inner surface of said wall to form an inlet for said metering passage and intersecting said diffuser channel cylindrical surface to form an outlet for said metering passage, said metering passage being oriented to direct coolant fluid into said diffuser channel so as to impart a swirling motion to the fluid about the axis of said channel.
Claim 2
Dependent Claim
260 words
A hollow, longitudinally extending airfoil including a cooled wall having an outer surface defining a pressure and suction surface of said airfoil, said pressure and suction surfaces adapted to have a hot gas stream flowing thereover in a downstream direction substantially perpendicular to said longitudinal direction, said cooled wall also having an inner surface adapted to define a portion of a coolant compartment for receiving coolant therein under pressure, the improvement comprising: a longitudinally extending cylindrical diffuser channel formed within said wall defining a cylindrical surface and having an axis; a pair of spaced apart, facing side surfaces forming a slot within said wall, said side surfaces intersecting said outer surface at a shallow angle to form a longitudinally extending slot outlet, and intersecting said channel cylindrical surface to form a slot inlet extending longitudinally substantially the full length of said cylindrical channel, said slot being oriented to direct coolant fluid therefrom as a continuous, longitudinally extending film over said outer surface downstream of said slot outlet; a single one of said slots intersecting each channel; and at least one metering passage formed within said wall for controlling the rate of flow of coolant fluid into said slot, said metering passage intersecting said inner surface of said wall to form an inlet for said metering passage and intersecting said diffuser channel cylindrical surface to form an outlet for said metering passage, said metering passage being oriented to direct coolant fluid into said diffuser channel so as to impart a swirling motion to the fluid about the axis of said channel.
Claim 3
Dependent Claim
32 words
The airfoil according to claim 1, wherein said slot side surfaces diverge to said slot outlet over at least a portion of the distance from said slot inlet to said slot outlet.
Claim 4
Dependent Claim
19 words
The airfoil according to claim 1 including a plurality of said metering passages spaced apart in said first direction.
Claim 5
Dependent Claim
63 words
The airfoil according to claim 1 wherein said cooled wall includes a plurality of said slots and a separate one of said channels for each slot, said slots disposed in a longitudinal row and spaced apart in said longitudinal direction and said channels aligned and spaced apart in said longitudinal direction, at least one of said metering passages intersecting each of said channels.
Claim 6
Dependent Claim
25 words
The airfoil according to claim 1 wherein said wall comprises a plurality of chordwise wafers which are stacked in said longitudinal direction and bonded together.
Claim 7
Dependent Claim
17 words
The cooled wall according to claim 4 wherein only one metering passage intersects each of said channels.