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TF600-52 Main Gear Fuel Pump - Eaton

Main Gear fuel PumpsTable of Contents Models 704300, 708300, 708400, 708600, 714900 3 Model 724400 4 Model 828300 5 Model 828500 6 Model 838000 7 Model 721400 8 Model 830800 9 Model 830100 10 Model 825500 11 Model 723300 12 Model 829500 13 Models 828200, 831000 14 Model 715200 15 Models 373400, 382400, 389400, 705300, 705400, 705500, 706800,71500 16 Models 386900, 390600, 720500, 720600 833700, 83800 17 Models 243600, 358200, 371900, 378200, 835800 18 Models 384300, 835900 19 For over 50 years Eaton has been the leading manufacturer of highly reliable main engine fuel pumps . These main engine fuel pumps are highly designed, precision mechanical pumps , mounted to the aircraft s engines that maintain the fl ow of fuel to the engine at a precise rate and pressure. Eaton s main engine fuel pumps are installed on 70% of the commercial jet engines currently fl ying today. They are utilized on military, commercial, regional and business aircraft engines series of gear fuel pumps contain a centrifugal boost stage, fuel fi lter, and gear stage.

Eaton’s 724400 model gear fuel pump contains a centrifugal boost stage, fuel fi lter and gear stage. Fuel supplied by the aircraft boost pump enters the

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Transcription of TF600-52 Main Gear Fuel Pump - Eaton

1 Main Gear fuel PumpsTable of Contents Models 704300, 708300, 708400, 708600, 714900 3 Model 724400 4 Model 828300 5 Model 828500 6 Model 838000 7 Model 721400 8 Model 830800 9 Model 830100 10 Model 825500 11 Model 723300 12 Model 829500 13 Models 828200, 831000 14 Model 715200 15 Models 373400, 382400, 389400, 705300, 705400, 705500, 706800,71500 16 Models 386900, 390600, 720500, 720600 833700, 83800 17 Models 243600, 358200, 371900, 378200, 835800 18 Models 384300, 835900 19 For over 50 years Eaton has been the leading manufacturer of highly reliable main engine fuel pumps . These main engine fuel pumps are highly designed, precision mechanical pumps , mounted to the aircraft s engines that maintain the fl ow of fuel to the engine at a precise rate and pressure. Eaton s main engine fuel pumps are installed on 70% of the commercial jet engines currently fl ying today. They are utilized on military, commercial, regional and business aircraft engines series of gear fuel pumps contain a centrifugal boost stage, fuel fi lter, and gear stage.

2 fuel supplied by the aircraft boost pump enters the boost stage, which increases pressure 125 psi (862 kPa). This pressure forces heated and fi ltered fuel through internal passages to the gear stage. fuel is directed to the fuel control where it is re-fi ltered and returned to the fuel fuel GEAR PUMP 1000 PSIG @ 6000 RPM704300, 708300, 708400, 708600, 714900 APPLICATIONS CFM56-2, CFM56-2A, CFM 56-2B CFM56-3, CFM56-3B, CFM56-3C CFM56-5, CFM56-5A, CFM56-5B, CFM56-5C3 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 708600 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed6000 RPMI nlet Pressure30 psig (138 kPag)Boost Stage Pressure Rise140 psid (965 kPag)Discharge Pressure1000 psig (6895 kPag) fuel Flow Rate58 gpm (220l/min)CRANKING CHARACTERISTICSS peed 625 RPMI nlet Pressure30 psig (207 kPag)Discharge Pressure 305 psig (2103 kPag) fuel Flow gpm ( )RotationClockwiseWeight 44 pounds ( kg)Model shown 708600 Eaton s 724400 model gear fuel pump contains a centrifugal boost stage, fuel fi lter and gear stage.

3 fuel supplied by the aircraft boost pump enters the boost stage, which increases pressure. This pressure forces heated and fi ltered fuel through internal passages to the gear stage. fuel is directed to the fuel control system where it is re-fi ltered and returned to the aircraft fuel GEAR PUMP 1145 PSIG @ 6250 RPM724400 APPLICATIONS CFM56-5B CFM56-5C4 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 724400 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed6250 RPMI nlet Pressure30 psig (207 kPag)Boost Stage Pressure Rise140 psid (965 kPad)Discharge Pressure1145 psig (7895 kPag) fuel Flow gpm (247 l/min)Main Inlet Filter (Disposable)40 micron nominal/80 micron absoluteCRANKING CHARACTERISTICSS peed (RPM)625 RPMI nlet Pressure30 psig (207 kPag)Discharge Pressure 305 psig (2103 kPag) fuel gpm ( l/min)RotationClockwiseWeight pounds ( kg)Model shown 724400 fuel supplied by the aircraft boost pump enters the fuel pump boost stage, which increases pressure.

4 Boost stage output fl ows through a cooler, main heat exchanger, and the pump fuel fi lter and then into the high-pressure gear stage. Bypass fl ow from the fuel control joins the boost stage discharge and re-enters the gear stage. A high-pressure relief valve permits the entire pump discharge fl ow to return to the gear stage inlet. This limits gear stage fuel GEAR PUMP 1145 PSIG @ 6250 RPM828300 APPLICATIONS CFM56-7B5 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 828300 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed6250 RPMI nlet Pressure30 psig (207 kPag)Boost Stage Pressure Rise110 psid (758 kPad)Discharge Pressure1145 psig (7895 kPag) fuel Flow Rate65 gpm (246 l/min)CRANKING CHARACTERISTICSS peed (RPM)625 RPMI nlet Pressure30 psig (207 kPag)Discharge Pressure 305 psig (2100 kPag) fuel gpm ( l/min)RotationClockwiseWeight pounds (22 kg)Model shown 828300 Eaton s 828500 model pump inlet feeds into the centrifugal boost stage, which raises the pressure of the fuel .

5 Discharge from the boost stage mixes with returned fuel from the fuel control and is fi ltered before entering the high-pressure gear stage, which forces the fuel through heat exchangers. The fuel re-enters the pump through the main fuel fi lter and servo wash fuel fi lter assemblies and into the hydro-mechanical unit (HMU). The HMU measures fuel fl ow and returns unused fuel and servo discharge to the pump bypass return fuel GEAR PUMP 1600 PSIG @ 7380 RPM828500 APPLICATIONS GE 90-76B, GE 90-77B GE 90-85B GE 90-90B GE 90-92B GE 90-94B6 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 828500 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed7603 RPMI nlet Pressure15 psig (103 kPag)Discharge Pressure1600 psig (11032 kPag) fuel Flow gpm (429 l/min)CRANKING CHARACTERISTICSS peed (RPM)455 RPMI nlet Pressure15 psig (103 kPag)Discharge Pressure 165 psig (1138 kPag) fuel gpm ( l/min)RotationClockwiseWeight pounds ( kg)Model shown 828500 The pump inlet feeds into the centrifugal boost stage, which raises the pressure of the fuel .

6 Discharge from the boost stage mixes with returned fuel from the fuel control and is fi ltered before entering the high-pressure gear stage which forces the fuel through heat exchangers. The fuel re-enters the pump through the main fuel fi lter and servo wash fuel fi lter assemblies and then into the hydromechanical unit (HMU). The HMU measures fuel fl ow and returns unused fuel and servo discharge to the pump bypass return fuel GEAR PUMP 1700 PSIG @ 7863 RPM838000 APPLICATIONS GE 90-112B GE 90-115B7 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 838000 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed7863 RPMI nlet Pressure20 psig (138 kPag)Discharge Pressure1700 psig (11722 kPag) fuel Flow gpm (595 l/min)PERFORMANCE SPECIFICATIONS CRANKING CHARACTERISTICSS peed (RPM)455 RPMI nlet Pressure20 psig (138 kPag)Discharge Pressure 305 psig (2103 kPag) fuel gpm ( l/min)RotationClockwiseWeight pounds ( kg)Model shown 838000 Eaton s 721400 gear fuel pump couples a high-pressure gear pump with an intermediate-pressure centrifugal boost pump.

7 Low-pressure fuel leaves the pump outlet and re-enters at the high-pressure pump inlet port. The gear stage high-pressure fuel is discharged to the fuel metering unit (FMU). MAIN fuel GEAR PUMP 1630 PSIG @ 6841 RPM721400 APPLICATIONS Trent 768 and Trent 772 Trent 877, Trent 884, Trent 892 and Trent 892B8 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 721400 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed6841 RPMI nlet Pressure20 psig (138 kPad)Boost Stage Pressure Rise160 psid (1103 kPag)Discharge Pressure1630 psig (11239 kPag) fuel Flow Rate115 gpm (435 l/min)CRANKING CHARACTERISTICSS peed (RPM)435 RPMI nlet Pressure20 psig (138 kPag)Discharge Pressure 305 psig (2103 kPag) fuel gpm ( l/min)RotationCounterclockwiseWeight 49 pounds ( kg)Model shown 721400 The gear fuel pump couples a high-pressure gear pump with an intermediate-pressure centrifugal boost pump. Low-pressure fuel leaves the pump outlet and then re-enters at the high-pressure pump inlet port.

8 The gear stage increases the fuel pressure, and the high-pressure fuel is discharged to the fuel metering unit (FMU).MAIN fuel GEAR PUMP 20 PSIG @ 7088 RPM830800 APPLICATIONS Trent 8959 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 830800 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed7088 RPMI nlet Pressure20 psig (138 kPag)Boost Stage Pressure Rise140 psid (965 kPad)Discharge Pressure1731 psig (11935 kPag) fuel Flow gpm (48,576 phr) (479 l/min)CRANKING CHARACTERISTICSS peed (RPM)435 RPMI nlet Pressure20 psig (138 kPag)Discharge Pressure 310 psig (2137 kPag) fuel gpm (1459 phr) ( l/min)RotationCounterclockwiseWeight pounds ( kg)Model shown 830800 Eaton s main gear fuel pump consists of a high pressure gear stage and fuel fl ow relief valve. This pump is mounted to the engine with a V-band clamp, providing fuel inlet, high pressure outlet, spill return and pressure sensing. fuel supplied to the pump is pressurized by a separate, engine-driven low-pressure fuel fuel GEAR PUMP 1210 PSIG @ 6228 RPM83010 0 APPLICATIONS RB211-53510 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 830100 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed6228 RPMI nlet Pressure130 psig ( kPag)Discharge Pressure1210 psig (8343 kPag) fuel Flow Rate81 gpm ( l/min)CRANKING CHARACTERISTICSS peed (RPM)777 RPMI nlet Pressure30 psig (207 kPag)Discharge Pressure 350 psig (2413 kPag) fuel gpm ( l/min)RotationCounterclockwiseWeight pounds ( kg)Model shown 830100 fuel enters the pump at a pres-sure of approximately 20 psi (138 kPa) from the air-craft booster pump.

9 The centrif-ugal boost stage raises the fuel pressure and forces heated and fi ltered fuel through the gear housing to the high-pressure gear stage. The high-pressure gear stage discharges fuel to the fuel monitoring unit (FMU). fuel is ported back to the pump through the heat exchanger, re-fi ltered and returned to the fuel GEAR PUMP 1235 PSIG @ 6580 RPM825500 APPLICATIONS PW 4050 PW 4052 PW 4056 PW 4060, PW 4060A PW 4060C PW 4152 PW 4156, PW 4156A PW 4158 PW 4460 PW 446211 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 825500 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed6580 RPMI nlet Pressure20 psig (138 kPag)Boost Stage Pressure Rise160 psid (1103 kPad)Discharge Pressure1235 psig (8515 kPag) fuel Flow Rate97 gpm (367 l/min)Main Inlet Filter (Disposable)40 micron nominal/80 micron absoluteCRANKING CHARACTERISTICSS peed (RPM)665 RPMI nlet Pressure20 psig (138 kPag)Discharge Pressure 320 psig (8446 kPag) fuel Flow8 gpm ( l/min)RotationClockwiseWeight 50 pounds ( kg)Model shown 825500 fuel enters the pump at a pressure of approximately 20 psi (138 kPa) from the aircraft booster pump.

10 The centrifugal boost stage raises the fuel pressure and forces heated and fi ltered fuel through the gear housing to the high-pressure gear stage. The high-pressure gear stage discharges fuel to the fuel monitoring unit (FMU). fuel is ported back to the pump through the heat exchanger, re-fi ltered, and returned to the fuel GEAR PUMP 1355 PSIG @ 7145 RPM723300 APPLICATIONS PW4164 PW4168 PW4074 PW4077 PW408412 Eaton CORPORATION Aerospace TF600-52 November 2008 Model shown 723300 PERFORMANCE SPECIFICATIONS OPERATING CHARACTERISTICSS peed7145 RPMI nlet Pressure20 psig (138 kPag)Boost Stage Pressure Rise200 psid (1379 kPad)Discharge Pressure1355 psig (9342 kPag) fuel Flow Rate115 gpm (437 l/min)Main Inlet Filter (Disposable)40 micron nominal/80 micron absolute CRANKING CHARACTERISTICSS peed (RPM)686 RPMI nlet Pressure20 psig (138 kPag)Discharge Pressure 320 psig (2206 kPag) fuel gpm ( l/min)RotationClockwiseWeight 52 pounds ( kg)Model shown 723300 Eaton s 829500 model pump inlet feeds into the centrifugal boost stage, which raises the pressure of the fuel .


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