Avitech.docx
DOCX document 211 KB Posted
- Attached to
- Hydraulic Test Stand Federal contract opportunity
- Solicitation number
- W912KN-17-T-0047
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Additional information for the Hydraulic Test Stand
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| 17-T-0047.docx | DOCX document | |
| 17-T-0061.docx | DOCX document | |
| 17-T-0047.docx | DOCX document |
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Text version
HYDRAULIC PUMP AND ACCESSORI ES TEST STAND MODEL AV843
NSN 4920-01-074-7836
HYDRAUL
I C
PUMP
AND
ACCESSORI
ES
TEST
S T
AND
MODEL
A V843
NSN
4920-01-074-7836
PURPOSE
The Avitech AV843 Hydraulic Pump and Accessories Test Stand is designed to accurately perform overhaul and post overhaul acceptance tests on
| hydraulic |
| and |
| pneumatic |
| components | |
| such | |
| as | valves, |
actuating cylinders, solenoid valves, reservoirs, accumulators, pumps, and other components .
Capabilities of the AV843 Test Stand include producing and maintaining drive speeds, flow rates, temperatures, and pressures, as required when testing components.
and faci lities for mounting and driving hydraulic pumps The )The Test Stand consists of a drive console and a control console. The drive console encloses a reversible, variable speed drive, an electric motor, control console contains the instrumentation, electrical control circuits, storage compartment and writing surface.
The Test Stand utilizes a low pressure boost pump, high pressure hydraulic pump and an air-operated hydraulic booster.
All required instrumentation to perform tests on the necessary components has been provided with accuracies meeting or exceeding specifications in the applicable Technical Orders.
APPLICA BILITY
AIRCRAFT:
Many different military aircraft systems including the F-4, F-5, F-15, F-18, F-16, F-111, 818, 852, C130, KC135, and others.
COMPO ENTS TESTED
Hydraulic valves, linear and rotary actuating cylinders, solenoid valves, relief valves, selector valves, shuttle valves, pressure switches, pistons, reservoirs, accumulators, pumps, and other associated components .
HYDRAUL
I C
PUMP
AND
ACCESSORI
ES
TEST
S T
AND
MODEL
A V843
NSN
4920-01-074-7836
DESIGN PARAMETERS
1. One man operation
2. Stainless Steel Reservoir 3. MIL-H-5606 or MIL-H-6083
4. Drive Motor:
60 hp reversible, variable-speed drive system, 0 to 5000 RPM.
5. Pump Motors:
High Pressure: 60hp, 1775 rpm, 460v, 60Hz, 3-phase AC Boost Pump: 5hp, 1740 rpm, 460v, 60Hz, 3-phase AC.
6. Pump Capabilities:
High Pressure: 30 GPM at 3750 psi, reduce flow to 5000 psi Low Pressure: 40 GPM at 150 psi
7. Static Pressure Test: 0 to 25,000psi
8. Fluid Operating Temperature: 100°F tO 160°F
9. Supply and Return Filtration: High Pressure: 3 micron Boost Low Pressure: 10 micron Reservoir Return: 10 micron Uses replaceable elements.
10. UUT Mounting Adapters
OVERALL DIMENSIONS
132" wide by 78" high by 72" deep
WEIGHT
4500 pounds
SERVICES REQUIRED
Electrical Power Input:
460 volts, 3-phase, 60 Hz AC, 160kW, 200 amps Note: Other Electrical Voltages are Available - Please Specify Water: 15 to 20 gpm, 80° F Shop Air: 80 psi Nitrogen : 2630 cu in. nitrogen cylinder, rechargeable, supplied with test stand.
OPTIONS
See Separate Option details.
MANUALS
Three sets of Operation and Maintenance Manuals are shipped with each Stand. Included are schematics, installation wiring diagrams, bill of material, vendors' literature, spare parts list, and operation and maintenance instructions.
WARRANTY
AVIATION TECHNOLOGY , INC.
guarantees Equipment against defects in design, material, or workmanship for a period of 18 months after shipment or one year after start-up.
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