5000 PSI Hydraulic Test Bench

*Stainless Steel Enclosure if used with Skydrol or Hyjet IV

Key Features & Advantages, Click on JEHA MK IV or HCT-12

Hydraulics International, Inc.*, Chatsworth, Calif., is being awarded a $22,348,042 fixed-price, indefinite-delivery/indefinite-quantity contract for the A/F27T-12 hydraulic component test stand. This contract provides for the procurement of three pilot production units of the main hydraulic console, one pilot production of the pump and motor test console, one pilot production hydraulic fluid cooling system vapor cycle, one pilot production hydraulic fluid cooling system non-vapor cycle and the associated testing, technical and logistics data, and training. Work will be performed in Chatsworth, Calif., and is expected to be completed in August 2018. Contract funds will not expire at the end of the current fiscal year. This contract was competitively procured under an electronic request for proposals as a small business set-aside; two offers were received. The Naval Air Warfare Center Aircraft Division, Lakehurst, N.J., is the contracting activity (N68335-12-D-0023). Date: August 07, 2012 US Department of Defense

(http://www.fbodaily.com/archive/2012/08-August/10-Aug-2012/FBO-02831090.htm)

(http://www.veteranstoday.com/2012/08/07/u-s-department-of-defense-contract-awards-148/)

UNIVERSAL AIRCRAFT COMPONENT TEST STAND for Jumbo Jets including next generation Jumbo, Boeing B787, Airbus A380, A350 and Hydraulic Components fitted on both Military Aircraft & Helicopter.

A/F27T-12 replaces A/F27T-10

The model JEHA MARK IV or HCT-12 (A/F27T-12) is newly designed to perform all functional and operational tests of new generation commercial aircraft hydraulic and pneumatic components including (and not limited to) actuators and control valves, from both large and mid-size body aircrafts. Optional P&MTC (Pump and Motor Test Console ) provides capability of testing pump and motor and can be added to JEHA MARK IV or HCT-12 (A/F27T-12) at any time if required to expand the testing capability.

CONFIGURATION

JEHA MARK IV or HCT-12 (A/F27T-12): Aircraft Component Test Stand
P&MTC: Pump & Motor Test Stand for testing pump and motor tests

Note: As an option P&MTC can be added to JEHA MARK IV or HCT-12 (A/F27T-12) via simple connections.

Capabilities

Manual Control Modes
Human/Machine Interface (HMI) displays flow, pressure, temperature, calibration, diagnostic, & warning signals
Manual Control Panels (MCP)
Programmable Logic Controller (PLC)

Main Hydraulic Circuit

Two independent dynamic hydraulic test circuits, each capable of providing either:
25 GPM up to 5,000 PSIG OR 20 GPM up to 6,000 PSI,
And in combination can provide 50 GPM up to 5,000 PSIG OR 40 GPM up to 6,000 PSI.
Actuator Test Circuit: 1
Supply and Return Ports: 4 each
HP Supply Circuit filtration: 3-Micron Absolute
Return Circuit filtration: 10 micron Absolute
Two Supply Circuit flowmeters: 0.1 – 50 GPM OR 0.1 to 40 GPM
Return Circuit Back-Pressure Controls: 0 – 5,000 PSI OR 0-6,000 PSI

Low Pressure Circuit

Low Flow: Up to 10 GPM & 250 PSI
Supply Circuit flow meter: 0.1 – 15 GPM
Hydrostatic Circuit Up to 10,000 PSI
Pneumatic Circuit (GN2) Up to 6,000 PSI
Option: P&MT Console for Pump and Motor Tests
(with combination of MHC)
AND 20002 Test Pad
High Speed Induction Motor: 250 HP, 2,000 IN-LB torque, 15,000 RPM bi-directional
Regenerative Variable Frequency Drive: Operates and precisely controls the High Speed Motor
Pump Test Circuit: Closed Loop, up to 70 GPM & 5,000 PSI OR 70 GPM & 6,000 PSI
Pump Case Drain Circuit: 0 – 10 GPM
Patch Test Capability
Motor Test Circuit: Open Loop, up to 50 GPM & 5,000 PSI OR 40 GPM & 6,000 PSI

Hydraulic Test Equipment, Aircraft Hydraulic Test Equipment, Hydraulic Equipment Testing, Aircraft Hydraulic Equipment Testing, Hydraulic Test System, Aircraft Hydraulic Test System, Hydraulic Test Bench, Aircraft Hydraulic Test Bench, Hydraulic Test Stand, Aircraft Hydraulic Test Bench, Hydraulic Components Test Equipment, Aircraft Hydraulic Components Test Equipment, Hydraulic Components Testing & Aircraft Hydraulic Components Testing.

JEHA-MKIV Aircraft Component Test Bench

JEHA MKIV is the new generation, state-of-the-art Hydraulic Test Bench. Commercial (JEHA MKIV) and military versions HCT-12 (A/F27T-12) are available for selection. JEHA MKIV is built to meet fully with stringent environment testing like EMI, EMC, shock, vibration, noise etc. HII is building 80 sets and spares support will be guaranteed for the next 25 years.

Dual Independent Hydraulic System, each System is capable to deliver at least 25 GPM (or more if required) @ 5,000 PSI. Besides Hydraulic and provisions of AC & DC Power Sources, JEHA IV is equally capable to provide Hydrostatic, Pneumatic, Low Pressure Testing.

The Human Machine Interface (HMI) allows for human monitoring, input, and display of hydraulic fluid temperature and pressure, pneumatic pressures, fluid flow rates, and warning and status indicators. All input from temperature and pressure sensors and HMI inputs are processed by a Programmable Logic Controller (PLC). The PLC receives signal from flowmeters, temperature sensors, pressure transducers and also from HMI inputs and displays the measured valves on the HMI. JEHA MIV is designed with a combination of manual and automated controls. Critical Systems are still using mechanical controls.

No Gauges fitted on JEHA MKIV to be sent for calibration. Its Transducers or flowmeters also do not have to be removed for calibration. Instrument Verification Set (IVS) can be connected to JEHA MKIV to determine if Transducers or Flowmeters are within acceptable accuracy. JEHA MKIV is built with provision for ease of connecting to our Pump and Motor Test Console (P&MTC) if future expansion is required.

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.

Aircraft Components Hydraulic Test Bench

Current Production of Test Benches at Hydraulics International Inc.

Aircraft Components Hydraulic Test Bench

*Stainless Steel Enclosure if used with Skydrol or Hyjet IV

Hydraulic Test Bench for Jumbo Jets including next generation Jumbo, Airbus A350

JEHA MKIII is replaced by JEHA MKIV

37.50 GPM @ 5,000 PSI

55 GPM @ 3,000 PSI

Proof Pressure to 20,000 PSI

Designed and built to include servicing of Jumbo Jets Hydraulic Components including A350.

Large Body Aircraft Accessories Test Bench

JEHA MARK III Hydraulic Test Stand can test all components and hydraulic systems, both rotating and non-rotating, found in today’s new generation of jet aircraft.

TEST CAPABLITY :

• 100 HP Regulated Variable Speed Hydraulic Drive includes a hydraulic motor and gearbox with single output spindle. Driving through a two-range gearbox, the unit provides speed ranges of 100 to 4000 RPM and 600 to 10,000 RPM, bi-directional.

• Hydraulic Circuit, with 150 gallon stainless steel reservoir, in corporates all components necessary to assure circulation of clean (3 micron absolute) hydraulic fluid. all required test unit in let and outlet pressures,test until case pressure and adequate cooling capacity. The hydraulic supply section may be included in the main structure, or may be mounted on a separate base for remote location, with remote elect. Volume and pressure controls (optional).

Main Supply Pump is capable of delivery 55 GPM at 3000 PSI or 37.5 GPM at 5000 PSI. The pressure-compensated pump is a variable displacement type with handwheel volume control.

• A Low Pressure Supercharge Pump is supplied to boost pressure for test pumps operating at high speeds. The 120GPM centrifugal supercharge pump supplies up to 100 PSI boost pressure and can be regulated from 5 to 100 PSIG. Pressure for tests at lower and sub-atmospheric pressures is controlled by a throttle valve. As a safety feature, supercharger pump must be operating at preset pressure before main pump will start.

• 20,000 PSIG Auxiliary Static Proof Pressure Pump is sup plied with the stand.
Fluid Cooling is provided by a water-to-oil heat exchanger, and a self-acting controller maintains fluid at 140° ± 10°.

Aircraft Components Hydraulic Test Bench

Skydrol or Hyjet IV

30 GPM @ 5,000 PSI

Proof Pressure to 20,000 PSI

JEHA MARK II-SS Universal Hydraulic Test Console tests all components and hydraulic systems in today’s jet or piston aircraft.

JEHA MKII (SS) is replaced by JEHA MKIV

TEST CAPABILITY for Non-Rotating Equipment:

Four pressure connections provide flows up to 30 GPM and pressure to 5000 PSI with 60-cycle electrical power source.
Selector valve circuit provides manual flow cycling of components and may also be used as quick open and close valve control.
Three return ports are each capable of throttling return flow up to 5000 PSI. One is a metered circuit, diverting the return flow through flowmeters and measuring fluid flow up to 30 GPM.
- A second metered low flow return circuit measures leakage rates up to 4 GPM. Intended to measure case drain leakage of rotating components, this circuit can also be used as a leakage flowmeter for non-rotating parts.
- Separate low pressure fluid supply provides maximum flow of 30 GPM at 500 PSI.
- Static pressure test circuit provides hydraulic pressures to 20,000 PSI for proof tests.
- *
TEST CAPABILITY for Rotating Equipment:
- Variable Speed drive system permits testing of hydraulic pumps and motors, the drive system may be used to drive a pump under test or, conversely, as a power absorption source to load hydraulic motors being tested.

Aircraft Components Hydraulic Test Bench

30 GPM @ 5,000 PSI

Proof Pressure to 20,000 PSI

JEHA MARK II Universal Hydraulic Test Console tests all components and hydraulic systems in today’s jet or piston aircraft.

JEHA MKII is replaced by JEHA MKIV

TEST CAPABLITY for Non-Rotating Equipment:

Four pressure connections provide flows up to 30 GPM and pressure to 5000 PSI with 60-cycle electrical power source.
Selector valve circuit provides manual flow cycling of components and may also be used as quick open and close valve control.
Three return ports are each capable of throttling return flow up to 5000 PSI. One is a metered circuit, diverting the return flow through flowmeters and measuring fluid flow up to 30 GPM.
A second metered low flow return circuit measures leakage rates up to 4 GPM. Intended to measure case drain leakage of rotating components, this circuit can also be used as a leakage flowmeter for non-rotating parts.
Separate low pressure flu1d supply provides maximum flow of 30 GPM at 500 PSI.
Static pressure test circuit provides hydraulic pressures to 20,000 PSI for proof tests.

Test Capability for Rotating Equipment:

Hydrostatic drive system permits testing of hydraulic pumps and motors. Consisting essentially of a two-speed gear box driven by a hydraulic motor/pump, the drive system may be used to drive a pump under test or, conversely, as a power absorption source to load hydraulic motors being tested.

Aircraft Components Hydraulic Test Bench

HIS-300 is used for functional and operational testing of all types and sizes of aircraft, missiles, ground support and industrial hydraulic components, valves, actuators, pumps, hydraulic motors, systems and sub-systems.

Flow capacities from 5 to 65 GPM.
Constant or infinitely variable flow controls.
Multiple circuits.
Static test circuits to 30,000 PSI.
Automatic Temperature control – Automatic Pressure Control
Constant or infinitely variable pressure controls.
Separate instrumentation for separate circuits.
Pressure capacities from 500 to 5,000 PSI.
Accurate, dependable. Minimum maintenance.
Long trouble-free service.
*

Aircraft Components Hydraulic Test Bench

Hydraulic Component Test Stand, Model: HCT-20

TEST CAPABILITY FOR F-16

The model HCT-20 Hydraulic Component Test Stand has been designed to perform all functional and operational tests on hydraulic components, including (and not limited to) motors, pumps, actuators and control valves, from both rotary and fixed wing aircraft.

Configuration

Type I: Combination of hydraulic component test station and VSD console.

Type II: Hydraulic component test station only. No VSD console

Note: VSD console (for Pump and Motor Tests) can be added to Type II via simple connections.

Aircraft Components Hydraulic Test Bench

*Stainless Steel Enclosure if used with Skydrol or Hyjet IV

High-pressure TUBE & HOSE TEST STAND (HS-3000S) provides versatile service in all static, high pressure testing applications including but not limited to leak check and pressure proof test of metalic tubes, flexible hoses and any other type equipment requiring high-pressure static testing. The test stand may be provided in working pressure ranges from 500 to 30,000 PSI and are safely tested with its compact easy to operate control console design. The protective enclosure can withstand an explosion, such as encountered if a tube or hose fails the hydrostatic test. The test stand is considered to be portable by means of lockable caster wheels. The control console integrates Dual Hydrostatic Air driven pumps to individually control low and high range hydrostatic testing.

HYDRAULICS INTERNATIONAL, INC

Hydraulics International’s Hydrostatic Test System provide versatile service in all static high pressure testing using skydrol fluid of metallic tubes and any other type equipment requiring high-pressure testing. The test stand made our of stainless steel construction may be provided in working pressure ranges from 0-10,000 PSI and are safely tested with its compact easy to operate control console design. Each test hose or tube is enclosed in a chamber. The protective enclosure can withstand an explosion, such as encountered if a tube or hose fails the hydrostatic test. The control console integrates a hydrostatic Air driven pump to fill and control high range testing

Hydraulic Fluid Service Unit

NSN 4920-01-053-2833, NSN 4920-01-061-3819, NSN 4920-01-361-6089

TEST CAPABILITY FOR F-15

Used for functional testing of aircraft Pneumatic / Electro-Pneumatic Components up to 5,000 PSI.

Aircraft 5000 PSI Pneumatic Component Test-Bench

Aircraft 5000 PSI Pneumatic Component Test-Bench

Aircraft Components Hydraulic Test Bench

For functional testing and operational testing of Aircraft Fuel and Booster Pumps. This machine is designed to test electric motor driven submerged fuel booster pumps. The machine incorporates basic features of Model PB-2 Fuel Booster Pump Test Machine. The test machine is available for use with fluids such as gasoline, kerosene, and others. The standard machine is constructed for use JP-8 fluid. (Specify exact fluid designation). The electrical system is designed in conformance with the National Electrical Code requirements for hazardous locations.

OPTIONAL EQUIPMENT

Code 1 – 600 mm flowmeter with an accuracy of 1% of instantaneous reading in lieu of the 250 mm standard.

Code 2 – Fuel accessories test circuit consisting of a hand pump, 60 PSI pressure gauge and control valves for testing fuel relief valves, similar components and external leakage of pumps (static test).

Aircraft Components Hydraulic Test Bench