Aeronautical Lab Equipment

Composite Structures lab

Modular 2S Vacuum assisted resin transfer molding system.

Description:

The MODULAR 2S is a single pump / single resin trap mobile vacuum system for manufacturing composites using processes such as resin infusion and vacuum bagging.

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Thin Cylinder Apparatus

Description:

Is to investigate stresses and strains in a thin-walled cylinder under internal pressure. Steel cylinder working to 70 bar. Cylinder fitted with 6 strain gauges wired to a selector switch. Self-contained hydraulic pump and flow control valve and bourdon tube pressure gauge.

Product Code : SAMS - 0777

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Supersonic Wind Tunnel

Specifications:

Operational stagnation pressure = 8 bar

Volume of storage tank = 3 ft dia X 7 ft length X 2 no

Steady state run time = 30 seconds

Compressor of suitable of 20HP capacity

Suitable air drier

Instrumentation consisting of PC board

Air receiver tank 1500 ltr (vertical) 2.NO

Air receiver tank 2500 ltr (vertical)

Air dryer

Air cooled air cooler

Product Code : SAMS-AE-0777

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Supersonic Wind Tunnel

Specifications:

Operational stagnation pressure = 8 bar

Volume of storage tank = 3 ft dia X 7 ft length X 2 no

Steady state run time = 30 seconds

Compressor of suitable of 20HP capacity

Suitable air drier

Instrumentation consisting of PC board

Air receiver tank 1500 ltr (vertical) 2.NO

Air receiver tank 2500 ltr (vertical)

Air dryer

Air cooled air cooler

Product Code : SAMS-AE-0777

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Wind Tunnel

This is an open circuit Wind Tunnel which provides a region of controlled airflow into which models can be inserted. The propulsion is provided by a fan at downstream of working section. The tunnel consists of bell mouth shaped entry to guide the air smoothly into settling chamber consisting of honeycomb and nylon mesh screens which filters and stabilizes the air flow. This follows working section or test section where various models can be tested.

Product Code : SAMS AE - 001

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Sub Sonic Wind Tunnel

This is an open circuit Wind Tunnel which provides a region of controlled airflow into which models can be inserted. The propulsion is provided by a fan at downstream of working section. The tunnel consists of bell mouth shaped entry to guide the air smoothly into settling chamber consisting of honeycomb and nylon mesh screens which filters and stabilizes the air flow. This follows working section or test section where various models can be tested.

Product Code : SAMS AE - 001

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RADIAL 14 CYLINDER PISTON ENGINE (PROPULSION- LAB) (PROPULSION- LAB)

We are leading of doing cut works in Aircraft Piston Engine Cut-section for easily understanding the working principles

The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders point outward from a central crankshaft like the spokes of a wheel. It resembles a stylized star when viewed from the front, and is called a "star engine" (German Sternmotor) in some languages. The radial configuration was very commonly used in aircraft engines before turbine engines became predominant.

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Centrifugal Blower Test Rig

The Centrifugal Compressor Test Rig consists of a centrifugal blower driven by a variable speed electric motor. A motor controller is used to regulate the blower speed. Ducts are fitted to inlet & outlet of the blower. A damper in inlet duct is provided to regulate the intake air flow of the blower. A Pitot tube with differential manometer is used to measure the air flow rate. Two manometers are provided to measure intake & discharge pressure of air.

Product Code : SAMS AE - 002

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Beam Test Setup

A bench mounted beam apparatus to allow students to investigate the deflections and reactions in simply supported and cantilevered beams

Product Code : SAMS AE - 003

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Forced Convection Apparatus

Average surface heat transfer coefficient for a pipe losing heat by forced convection to air flowing through it can be obtained for different air flow and heat flow rates. The unit consists of a circular pipe, loosing heat by forced convection to air, being forced through it. Constant heat flux is added to pipe by an electrical heater, provided with input control. The pipe surface temperature is measured at various points along length of pipe using thermocouples. Temperature of air at inlet and outlet of test section is measured using temperature indicator.

Product Code : SAMS AE - 004

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Propeller Test Rig

In this test rig, performance of a Propeller can be investigated. The propeller is mounted on a shaft of DC motor. The load cell arrangement is used to measure the thrust force produced by the propeller.

Product Code : SAMS AE - 005

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hele shaw apparatus

Working Section : Made of two laminated glass / acrylic sheets which are closely spaced and fixed in a leak proof moulding

Flow table : Width = minimum 300mm,Length = minimum 500mm,

Dye Tank With Flow Control : Stainless steel tank with minimum 1L capacity Dye injection facility

Sump Tank : Stainless steel tank with minimum 40L capacity

Water circulation : Suitable capacity pumpProduct Code : SAMS DYN - 002

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Flow Visualization Apparatus

The unit uses water as the flow medium. A contrast medium (dye) is injected through small needles into the flow area. Various drag bodies (included) can be placed in the area of flow. In addition, sources and sinks can be simulated and illustrated using eight additional openings in the flow area.

Product Code : SAMS AE - 006

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