video corpo

39-0001-1100
2Pages

{{requestButtons}}

Catalog excerpts

39-0001-1100 - 1

Part No. 39-0001-1100 — Pump Part No. 39-0004-1100 — Canister The Eaton designed 39-0001 boost pump is mounted within a 39-0004 canister installed in the aircraft fuel tanks. The pump incorporates a mixed flow impeller driven by an internal, fuel flooded, variable frequency 3 phase induction motor and provides fuel supply to the engines. The pump is capable of operation directly from a 200V L-L 360Hz to 800Hz three phase supply. Pump performance is maintained at altitude over a range of fuel temperatures. The unit has excellent thermal performance mounted to composite structure and includes both motor thermal protection devices and a thermal sensor to indicate composite structure interface temperature. Design Features • The canister incorporates inlet and outlet valves to allow the pump to be removed from the tank without needing to drain the fuel tanks. • The reliability and long life of the unit are enhanced by the fully flooded operation of the AC motor which facilitates cooling and lubrication.

Open the catalog to page 1
39-0001-1100 - 2

Specification Pump . . . . . . . . . . . . . . . . . . . . . . . . Part No. 39-0001-1100 Canister . . . . . . . . . . . . . . . . . . . . . . Part No. 39-0004-1100 Power Supply . . . . . . . . . . . . . . . . . . 200V 3 Phase . . . . . . . . . . . . . . . . . . . . . . . . . . . . Variable Frequency 360 - 800Hz Flow Rate . . . . . . . . . . . . . . . . . . . . 3.78kg/sec (30,000 lb/hr) Delivery Pressure . . . . . . . . . . . . . . min 48 / max 413kPa (7/60psig) Motor Speed . . . . . . . . . . . . . . . . . . Variable (5300 - 8500rpm) Current Consumption . . . . . . . . . . . 8.4A at 400Hz ....

Open the catalog to page 2

All EATON SAS catalogs and technical brochures

  1. Boeing CH-47

    8 Pages

  2. Aerospace

    8 Pages

  3. 7202

    2 Pages

  4. 7100

    2 Pages

  5. 9121

    2 Pages

  6. 20026

    2 Pages