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Hydraulic Power Mule
UNIVERSAL HYDRAULIC CART
UNIVERSAL PORTABLE HYDRAULIC POWER SUPPLY
UNIVERSAL PORTABLE HYDRAULIC TEST STAND
UNIVERSAL PORTABLE HYDRAULIC TEST RIGS
Diesel Engine Driven
A/M27T-15
Test Medium: Hydraulic fluid, MIL-H-83282, MIL-H-5606, or as specified by customer when ordering.
Flow Rate Capacity: 32 GPM at 3000 PSI, 22 GPM at 5000 PSI
Test Medium: Skydrol 500A and B, or as specified by customer when ordering.
Flow Rate Capacity: 32 GPM at 3000 PSI, 22 GPM at 5000 PSI
Electric Motor Driven
A/M27T-14
Test Medium: Hydraulic fluid, MIL-H-83282, MIL-H-5606, or as specified by customer when ordering.
Flow rate Capacity: 40 GPM at 3000 PSI, 25 GPM at 5000 PSI
Test Medium: Skydrol 500A and B, or as specified by customer when ordering.
Flow rate Capacity: 40 GPM at 3000 PSI, 25 GPM at 5000 PSI
Hydraulics International, Inc. (HII) is under Contract in the United States to build these new Units (P/N: 040489-100 & 040499-100) with more modern, reliable, maintainable and supportability for replacing all their existing old Units of different models. These new Units can be used to support military or civil helicopters based ashore or afloat including supporting intermediate activities at the flight line or in hangars, at air stations and air capable ships. These new Units are designed to troubleshoot and functionally check helicopter or any aircraft hydraulic systems. Besides having incorporated the latest state of the art innovations, these Units also come with a much higher capacity (flow rate & pressure). These Units come with NATO or National Stock Numbers and are fully provisioned for spare and replacement parts for more than 20 years. Although specifically designed and built for supporting all military helicopter including those built by other Countries, these Units can also support fixed wing military aircraft including narrow body aircraft such as Boeing B737, B757, AIRBUS A318, A319, A300, A310, A320, A321, MA-60, MA-600, MA-700, C919, C929, C939, LE500, HO300, Primus 100, Primus 150, Starlight 100, Starlight 200, ARJ21, Y-5, Y-6, Y-7, Y-8, Y-9, Y-10, Y-11, Y-12, Y-20, An-26, An-30, An-124, Il-76, Il-476, An-70, Il-86, Tu-134, Tu-154, Yak-40, Yak-42, MiG-21, MiG-23, MiG-25, MiG-27, MiG-29, Su-17 (Su-22), ERJ145, SAAB340, ATR72, Superjet 100, BAE146, BAE HAWK, F28, Falcon Jets, KAI T-50 Golden Eagle etc or as long as the capacity of the hydraulic system is within the range of test stand flow and pressure.
These Units are designed and built for connecting to US Navy Standard Hydraulic Fluid Purifiers (P/N: 040505-100) to provide removal of hydraulic fluid particulates, water, chlorinated solvents, absorbed air & gases, which is common problem with aircraft.
P/N: 040505-100 * NSN: 4920-01-523-0592
A/M37M-11 (US Navy Standard Hydraulic Fluid Purifiers)
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P/N: 040505-100,
NSN: 4920-01-0592
removes:
1) 100% free water .
2) Dissolved water to less than 100 ppm .
3) 100% entrained gases .
4) 98% of dissolved gases
5) Particulate contamination to produce a cleanliness level of NAS1638, Class 2.
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Dual Power Driven:
Diesel Engine Driven
or
Power Supply (3 Phase 115 VAC) can be provided by 040489-100 or 040499-100 .
Towable at 20 mph max. over improved roads.
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Hydraulic Power Mule
Two System: 106 GPM at 3000 PSI, 80 GPM at 4000 PSI, 64 GPM at 5000 PSI Or combined
UHTS comes with an integral built Hydraulic Purification System (HPS) that provides continuous cooling, filtering moisture and to remove hydraulic fluid particulates, water, chlorinated solvents, absorbed air & gases removal from hydraulic fluid. Keeping hydraulic fluid clean and eliminates the need of changing hydraulic fluid for a long period of time. HPS work in a very cost-effective way to minimize hydraulic fluid usage, minimize hazardous waste disposal needs, reduce deployment foot print and sharply reduce hydraulic maintenance and associated costs.
Purification Performance
1) Contaminant removal: 55 gallon of hydraulic fluid in 5 hours.
2) Water: From 1000 to less than 200 PPM.
3) Chlorinated solvents: From 400 to less than 100 PPM.
4) Air & Gas: 100% dissolved air removal, 98% (by volume) removal.
5) Particulate: Cleanliness level equal to or better than NAS 1638 class 3.
One System: 53 GPM at 3000 PSI, 40 GPM at 4000 PSI, 32 GPM at 5000 PSI per system
Two System: 106 GPM at 3000 PSI, 80 GPM at 4000 PSI, 64 GPM at 5000 PSI Or combined
UHTS comes with an integral built Hydraulic Purification System (HPS) that provides continuous cooling, filtering moisture and to remove hydraulic fluid particulates, water, chlorinated solvents, absorbed air & gases removal from hydraulic fluid. Keeping hydraulic fluid clean and eliminates the need of changing hydraulic fluid for a long period of time. HPS work in a very cost-effective way to minimize hydraulic fluid usage, minimize hazardous waste disposal needs, reduce deployment foot print and sharply reduce hydraulic maintenance and associated costs.
Purification Performance
1) Contaminant removal: 55 gallon of hydraulic fluid in 5 hours.
2) Water: From 1000 to less than 200 PPM.
3) Chlorinated solvents: From 400 to less than 100 PPM.
4) Air & Gas: 100% dissolved air removal, 98% (by volume) removal.
5) Particulate: Cleanliness level equal to or better than NAS 1638 class 3.
UHTS is set-up with Instruments capability to be verified by an inexpensive Instrument Verification Set (IVS) within 15 minutes minimizing UHTS downtime and cost. All readings on UHTS are shown on high resolution LCD Display & Engine Performance Module. NO GAUGES including Transducers or Flowmeters are required to be removed for calibration. IVS can be connected directly to UHTS to verify that Transducers & Flowmeters are within acceptable accuracy. IVS is certified and traceable to NIST.
COMPARISON
(MJ-2A vs UHTS)
|
ITEM |
SPECIFICATIONS |
MJ-2A |
UHTS
|
|
1 |
Design |
30 years old Technology, number of major component are obsolete. |
New generation of Hydraulic Test stands with the latest state-of-the-art features and components. UHTS has also been qualified to the most rigorous military requirement testings such as environmental, Electro Magnetic Interference, Mobility, Reliability, Maintainability, etc. |
|
2 |
Aircraft Application |
Accepted in-service by USAF for their F-16 and some designated aircraft. |
Accepted in-service by USAF for supporting their F-16 and can be used to support any transport or fighter aircraft in their inventory. |
|
3 |
Hydraulic Purification System (HPS) |
Using normal Filter Elements. |
UHTS comes with an AF qualified integral built Hydraulic Purification System (HPS) that provides continuous cooling, filtering to remove hydraulic fluid particulates, water, chlorinated solvents, absorbed air & gases from aircraft hydraulic fluid as well as test stand. This purification process eliminates the need of changing hydraulic fluid for a long period of time. HPS works in a very cost effective way to minimize aircraft hydraulic fluid usage, minimize hazardous waste disposal needs, reduce deployment foot print and sharply reduce aircraft hydraulic components maintenance and associated costs. (See attached article from USAF, which is self-explanatory.) Purification Performance 1) Contaminant removal: 55 gallons of hydraulic fluid in 5 hrs. 2) Water: From 1000 to less than 100 PPM 3) Chlorinated solvents: From 400 to less than 100 PPM 4) Air & Gas: 100% dissolved air removal, 98% (by volume) removal 5) Particulate: Cleanliness level equal to or better than NAS 1638 class 3.
|
|
4 |
Test Medium |
Hydraulic fluid, MIL-H-5606, MIL-H-83282 |
Hydraulic fluid, MIL-PRF-5606, MIL-PRF-83282, and MIL-PRF-87257. |
| 5 |
Flow Rate Capacity |
One system 35 GPM at 3000 PSI 15 GPM at 5000 PSI Two system 70 GPM (35 GPM/system at 3000 PSI) 30 GPM (15 GPM/system at 5000 PSI) or combined |
One system 53 GPM at 3000 PSI 40 GPM at 4000 PSI 32 GPM at 5000 PSI per system Two system 106 GPM at 3000 PSI 80 GPM at 4000 PSI 64 GPM at 5000 PSI Or combined
|
|
6 |
Operating Conditions
|
Ambient Temperature Range -40ºF to +125ºF Altitude: Sea level to 6000 feet Relative Humidity: 0% to 100% Test Stand Position: Up to 8 1/2° from horizontal |
Ambient Temperature Range -40ºF to +125ºF Altitude: Sea level to 7000 feet Relative Humidity: 0% to 100% Test Stand Position: Up to 8 1/2° from horizontal |
|
7 |
Hydraulic Reservoir
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60 U.S. Gallon capacity vented to atmosphere and fluid is subject to ambient |
90 U.S. Gallon capacity Is completely sealed to atmosphere. This feature prevents airborne particulate, moisture and air to enter hydraulic fluid, maintaining purity of hydraulic fluid all the time.
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8
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Control Panel |
Conventional Control and Analog Instrumentation |
Combination of manual and automated controls. Fully military qualified with System Diagnostic, Built-in Test System and Human Machine Interface Touch Screen Operator Panel enabling ease of Operator Operation, Troubleshooting and ease of Calibration. |
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9
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Drive Unit |
Diesel Engine, 210 HP, naturally aspirated, non-EPA certified, obsolete |
Diesel Engine, 300 HP, turbo-turbo charged, EPA certified to TIER III, Multi Fuel. |
|
10 |
Engine Diagnostic System |
No |
Cummins engine QSB6.7 is an electronic fuel and Governor controlled via Electronic Control Module (ECM) and full diagnostic control feature facilitating safety and troubleshooting features. |
|
11 |
Fuel tank capacity |
42 US gallons |
60 US gallon |
|
12
|
External Fill and Purification Ports |
No |
External Reservoir Fill and Discharge Ports enables the Operator to fill the Hydraulic Reservoir from an outside source, or to remove clean filtered hydraulic fluid from the Reservoir also External Purification Ports allow purification of external fluid source. |
|
13 |
Back Pressure Regulator |
No |
Back Pressure Regulator allows operation in both aircraft (Closed Loop) or test Stand Reservoir (Open Loop) operation with pressurized or non-pressurized aircraft reservoir systems. |
|
14 |
Instrument Calibration/Verification |
All Instruments require removal and verified calibration by third party, these results in equipment downtime and excessive cost. |
UHTS is set-up with Instruments capability to be verified by an inexpensive Instrument Verification Set (IVS) within 15 minutes minimizing Equipment downtime and cost. |
|
15 |
Fault Diagnostic System |
No |
If a fault exists before system operation or a fault occurs during system operation, fault conditions will immediately report to HMI message field and warning horn is activated. Any fault condition will be permanently stored to retentive memory of HMI computer. Up to 200 fault conditions can be stored in retentive memory If a critical fault occurs during system operation, engine will be automatically shut down in 10 seconds. Each fault condition has a corresponding fault diagnostics page at HMI. Fault diagnostics page provides detail fault information and recommend corrective actions. |
|
16 |
115 VAC Utility Power |
No |
UHTS incorporates Invertor to provide 115 VAC, Single Phase Electrical Power for Utilities. |
|
17 |
Wet Weight |
6,3000 Lbs |
7,800 Lbs |