초록 ▼

Vane pump (10) mechanical losses are reduced by removing vane friction losses and replacing them with lower magnitude journal bearing fluid film viscous drag losses. A freely rotating cam ring (70) is supported by a journal bearing (80). A relatively low sliding velocity is imposed between the cam r

Vane pump (10) mechanical losses are reduced by removing vane friction losses and replacing them with lower magnitude journal bearing fluid film viscous drag losses. A freely rotating cam ring (70) is supported by a journal bearing (80). A relatively low sliding velocity is imposed between the cam ring and the vanes (26). This permits the use of less expensive and less brittle materials in the pump by allowing the pump to operate at much higher speeds without concern for exceeding vane tip velocity limits.

대표청구항 ▼

Having thus described the present invention, it is now claimed: 1. A variable displacement gas turbine fuel pump comprising: a housing having a pump chamber, and an inlet and outlet in fluid communication with the pump chamber; a rotor received in the pump chamber; a cam member surrounding the roto

Having thus described the present invention, it is now claimed: 1. A variable displacement gas turbine fuel pump comprising: a housing having a pump chamber, and an inlet and outlet in fluid communication with the pump chamber; a rotor received in the pump chamber; a cam member surrounding the rotor and freely rotating relative to the housing; a cam sleeve radially interposed between the cam member and the housing; an actuator assembly operatively associated with the cam sleeve in the housing to selectively vary pump output; a spacer ring interposed between the cam sleeve and the housing wherein the spacer ring includes a generally planar cam sleeve rolling surface that allows a centerpoint of the cam sleeve to linearly translate; and a journal bearing interposed between the cam member and the cam sleeve for reducing mechanical losses during operation of the pump. 2. The fuel pump of claim 1 wherein the cam member has a smooth, inner peripheral wall that allows the rotor to rotate freely relative to the cam member. 3. The fuel pump of claim 1 wherein the journal bearing is a continuous annular passage between the cam member and the cam sleeve. 4. The fuel pump of claim 3 wherein the pumped fuel serves as the bearing fluid. 5. The fuel pump of claim 1 further comprising circumferentially spaced vanes operatively associated with the rotor. 6. The fuel pump of claim 1 wherein the journal bearing is a hydrostatic bearing. 7. The fuel pump of claim 6 wherein the pumped fuel serves as the bearing fluid. 8. The fuel pump of claim 1 wherein the journal bearing is a hydrodynamic bearing. 9. The fuel pump of claim 8 wherein the pumped fuel serves as the bearing fluid. 10. The fuel pump of claim 1 wherein the journal bearing is a hybrid hydrostatic/hydro dynamic bearing. 11. The fuel pump of claim 10 wherein the pumped fuel serves as the bearing fluid. 12. The fuel pump of claim 1 wherein the pumped fuel serves as the bearing fluid. 13. The fuel pump of claim 1 wherein a center of the cam sleeve enclosing the cam ring is selectively offset from a rotational axis of the rotor. 14. The fuel pump of claim 1 wherein the vanes are formed of tungsten carbide. 15. The fuel pump of claim 14 wherein the cam ring is formed of a low cost, durable material. 16. The fuel pump of claim 1 wherein the cam ring is formed of a low cost, durable material. 17. The fuel pump of claim 1 wherein the actuator assembly includes first and second oppositely disposed hydraulically operated pistons. 18. The fuel pump of claim 17 wherein the pistons act upon the cam sleeve at a location substantially diametrically opposite the generally planar cam sleeve rolling surface. 19. A variable displacement gas turbine fuel pump comprising: a housing having a pump chamber, and an inlet and outlet in fluid communication with the pump chamber; a rotor received in the pump chamber; a cam member surrounding the rotor and freely rotating relative to the housing; a cam sleeve radially interposed between the cam member and the housing; an actuator assembly operatively associated with the cam sleeve in the housing to selectively vary pump output of the cam sleeve in the housing to selectively vary pump output; a generally planar cam sleeve rolling surface interposed between the cam sleeve and the housing that allows a centerpoint of the cam sleeve to linearly translate; and a journal bearing interposed between the cam member and the cam sleeve for reducing mechanical losses during operation of the pump. 20. A variable displacement gas turbine fuel pump comprising: a housing having a pump chamber, and an inlet and outlet in fluid communication with the pump chamber; a rotor received in the pump chamber; a cam member surrounding the rotor and freely rotating relative to the housing; a cam sleeve radially interposed between the cam member and the housing; an actuator assembly operatively associated with the cam sleeve in the housing to selectively vary pump output; and a journal bearing interposed between the cam member and the cam sleeve for reducing mechanical losses during operation of the pump.