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A gas turbine engine includes a high-pressure compressor having an impeller and an impeller baffle having a generally annular body, the impeller baffle spaced apart from a back face of an impeller to create an airspace therebetween, the airspace communicating between an impeller exit and an apparatu

A gas turbine engine includes a high-pressure compressor having an impeller and an impeller baffle having a generally annular body, the impeller baffle spaced apart from a back face of an impeller to create an airspace therebetween, the airspace communicating between an impeller exit and an apparatus to be pressurized, the impeller baffle including a plurality of generally radially-disposed ribs extending into the airspace for diminishing the velocity of air swirling in the airspace.

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The invention claimed is: 1. A gas turbine engine comprising: a high-pressure compressor having an impeller; and an impeller baffle having a generally annular body, the impeller baffle spaced apart from a back face of an impeller to create an airspace therebetween, the airspace communicating betwee

The invention claimed is: 1. A gas turbine engine comprising: a high-pressure compressor having an impeller; and an impeller baffle having a generally annular body, the impeller baffle spaced apart from a back face of an impeller to create an airspace therebetween, the airspace communicating between an impeller exit and an apparatus to be pressurized, the impeller baffle including a plurality of generally radially-disposed ribs extending into the airspace for diminishing the velocity of air swirling in the airspace, and further including a plurality of air slots disposed on a rear face of the impeller baffle for further reducing air swirl. 2. The gas turbine engine as defined in claim 1 wherein the ribs extend radially from a central opening of the baffle and have a curved profile matching a contour of the impeller backface. 3. The gas turbine engine as defined in claim 2 wherein the annular body of the impeller baffle extends radially into close proximity with an outer surface of a runner supporting a carbon seal to thus define a narrow air gap that functions as a restrictor to restrict airflow over the rear face of the baffle. 4. The gas turbine engine as defined in claim 1 wherein the annular body of the impeller baffle extends radially into close proximity with an outer surface of a runner supporting a carbon seal to thus define a narrow air gap that functions as a restrictor to restrict airflow over the rear face of the baffle. 5. The gas turbine engine as defined in claim 1 wherein the impeller baffle further comprises a plurality of puller grooves formed in a lateral surface of the baffle to facilitate removal of the impeller baffle. 6. The gas turbine engine as defined in claim 1 wherein a lateral surface of the impeller baffle forms a tight fit with the bearing housing to secure the impeller baffle and wherein the impeller baffle is further secured by a retaining ring. 7. An impeller baffle for deswirling air downstream of an impeller in a gas turbine engine, the impeller baffle comprising: a generally annular body; a plurality of ribs formed on a front face of the annular body of the baffle, the ribs adapted to deswirl the air behind an impeller backface; and a plurality of air slots disposed on a rear face of the impeller baffle for further curtailing air swirl and thus further increasing air pressure. 8. The impeller baffle as defined in claim 7 wherein the ribs extend radially from a central opening of the baffle and have a curved profile matching a contour of the impeller backface. 9. The impeller baffle as defined in claim 8 wherein the annular body of the impeller baffle extends radially into close proximity with an outer surface of a runner supporting a carbon seal to thus define a narrow air gap that functions as a restrictor to restrict airflow over the rear face of the baffle. 10. The impeller baffle as defined in claim 7 wherein the annular body of the impeller baffle extends radially into close proximity with an outer surface of a runner supporting a carbon seal to thus define a narrow air gap that functions as a restrictor to restrict airflow aver the rear face of the baffle. 11. The impeller baffle as defined in claim 7 wherein the impeller baffle further comprises a plurality of puller grooves formed in a lateral surface of the baffle to facilitate removal of the impeller baffle. 12. The impeller baffle as defined in claim 7 wherein a lateral surface of the impeller baffle forms a tight fit with the bearing housing to secure the impeller baffle and wherein the impeller baffle is further secured by a retaining ring.