ENGINEERING LAB EQUIPMENT
LHP 601
AVIATION &
AERODYNAMICS
The LHP-601 laboratory covers all
areas, theoretical and practical,
concerning the basic principles of
Aviation and Aerodynamics
including Aeronautic products
designed for education and training
AF series. The laboratory consists of a
set of simulators and trainers listed
on the right of this page (any PCs
required are not included - provided
locally by reseller).
The laboratory deals with the AF
series of educational equipment
giving valuable hands-on
experience, whether used by
lecturers to demonstrate
aerodynamic basic principles or
advanced ideas or by students for
project work. AF series offers this
compact lab solution since the
hands-on experience is not always
possible or practical with large-scale
industrial or complex research
facilities. All the Aerodynamics
systems operate with an integrated
data acquisition system connecting
to a personal computer offering
working facilities to the students.
The laboratory’s equipment is
accompanied by the appropriate
software to run interactively with PC
workstations, wherever this is
applicable. When an available
program interfaces the PC with a
simulator, it offers support in all the
above training procedures and
creates realistic simulations.
The Lab consists of 2 sections:
 The Aerodynamics Lab equipment
 The Aviation systems simulators.
The Aerodynamics lab equipment
are custom made based on the
needs of the Institution. It is usually
addressing higher education
laboratory needs and not vocational
schools. You can see here some
applications addressed by our
equipment. For further info on
Aerodynamic laboratory equipment
please contact us with your
requirements.
The Aviation simulators are provided
for training in actual sub-systems of a
standard commercial airplane.
A simulator is an educational system
designed in metal vertical frame or
bench-top block configuration, so
the students have the capability to
watch the theoretical and practical
study of the Aviation systems include
color mimic diagrams that clearly
shows the structure of the system and
allows the location of components
on it. The display of the information
available on the PC monitor allows
the continuous monitoring of the
didactic process. The operational
conditions are entered by the
students. The insertion of faults is
carried out by either the software
application or with switches. A
simulator or a trainer is accompanied
by relevant software to enable the
student to follow step-by-step the
theory and the exercise. The whole
exercise procedure is carried out on
the simulators. The system is
accompanied by technical manuals
for theory and exercises. Each one of
the lab equipment is described
hereinafter. Theory concepts are
presented by the teacher in
presentation slides and the system
also offers a student response system
(optionally) on theoretical and
practical quizzes, tests or exams
which also the teacher can create.
AERODYNAMICS
AF series
AVIATION SYSTEMS
AQ-1
Twin-Engine Aircraft Electrical
System
AQ-2
Twin-Engine Aircraft Hydraulic
System
AQ-3
Twin-Engine Aircraft Air
Conditioning & Pressurization
System
LHP 601 AVIATION & AERODYNAMICS
Aerodynamics
AF Series
AF10
Modular Air Flow Bench
 Air bench with variable air flow
control and a wide range of
optional experiment modules
available for a complete
course in air flow.
 Small-scale wind tunnel, ideal
for student experiments, lecture
theatre demonstrations and
project work.
 Versatile, easy to fit and
change experiment modules.
 Includes a textbook “A First
Course in Airflow” by Professor
E. Markland.
 Compact and mobile, with a
worktop and shelves.
AF10 Ancillaries
 AF10a Multi-Tube Manometer
 AF11 Bernouli’s Equation
Apparatus
 AF12 Drag Force Apparatus
 AF13 Round Turbulent Jet
Apparatus
 AF14 Boundary Layer
Apparatus
 AF15 Flow Around a Bend
 AF16 Jet Attachment
Apparatus
 AF17 Flow Visualization
Apparatus
 AF18 Tapped Aerofoil
AF41
Flight Demonstration Wind
Tunnel
 Gives students a safe, realistic
introduction to the controls of a
light aircraft
 Aircraft able to move vertically
and pitch about the quarter
chord point independently
 Simulates take off, level flight,
cruise and landing
 Demonstrations include aerofoil
lift, stall, longitudinal stability
and transient motion
 Includes electronic display of
air speed, attitude, altitude,
pressure and lift
 Tufts on the wing clearly
demonstrate the phenomenon
of separation and stall
 Brightly illuminated working
section
 Adjustable centre of gravity of
the model
 Optional smoke generator and
chart recorder (available
separately)
AF41 Ancillaries
 AF41A Two-Pen Chart Recorder
(available separately)
 AFA10 Smoke Generator and
Probe (available separately)
AF100
Sub - sonic Wind Tunnel
 Saves time and money
compared to full-scale windtunnels or airborne laboratories
 Operates at meaningful
Reynolds numbers
 Compact, open-circuit suction
design
 Wide variety of experiments in
aerodynamics
 Comprehensive selection of
optional instrumentation,
models and ancillaries
 High levels of safety
 Controls and instrumentation
conveniently mount on a
separate, free standing frame
AF100 Ancillaries
 VDAS-F VDAS (Frame Mounted
Version)
 AFA1 Multitube Manometer
 AFA2 Basic Lift and Drag
Balance
 AFA3 Three-Component
Balance
 AFA4 Balance Angle
Feedback Unit
 AFA5 Differential Pressure
Transducer
 AFA6 32-Way Pressure Display
Unit
 AFA7 Pitot Static Traverse
(300mm)
 AFA10 Smoke Generator
 AF101 Cylinder Model
 AF102 NACA 0012 Aerofoil with
Tappings
 AF103 NACA 2412 Aerofoil With
Flap
 AF104 Set of two NACA 0012
Aerofoils
 AF105 Flat Plate Drag Model
 AF106 Boundary Layer Model
 AF107 Aircraft Model - Low
Wing
 AF108 Aircraft Model - High
Wing
 AF109 Three-dimensional Drag
Models
AF27
Nozzle Flow Apparatus
If the school does not have one
available, LH can supply the
AF27A air flow pump.
 Floor-standing apparatus that
demonstrates the
thermodynamics and fluid
mechanic of the adiabatic
expansion of air through
subsonic and supersonic
nozzles
 Connects to suitable laboratory
compressed air supply or LAB
HELLAS’s optical Compressor
(AF27A)
 Includes three
interchangeable, profiled and
polishes brass nozzlesconvergent, convergentdivergent and convergentparallel
 Built-in instrument frame and
worktop
 Electronic instruments measure
and display multiple pressure
and temperatures at the same
time, for ease of use and for
connection to LAB HELLAS’s
VDAS®
AF27 Ancillaries
 AF27A Air Comressor And
Receiver
 VDAS-F VDAS (Frame Mounted
Version)
LHP 601 AVIATION & AERODYNAMICS
AVIATION SYSTEMS
AQ-1 Simulator
Twin-engine Aircraft Electrical System
The aircraft electrical system simulator
mod. AQ-1, is included in a complete set of
educational equipment for the basic
training on aircraft systems. The simulator
consists of a computer-assisted panel, with
silk-screen mimic diagram for a clear
location of its components. Various zones
of the mimic diagram are represented with
different colors to emphasize peculiar
aspects of the system. Light and displays
indicators, installed in the mimic diagram
enable to assess the evolutions of the
control. The graphic display of the
information available at the control input,
such as aircraft status (park, APU…) on the
computer screen enables the permanent
monitoring of the system. The operational
conditions are set by students according to
the educational path indicated in the
courseware, carried out by the PC.
TRAINING PROGRAM
POWER GENERATION
DC battery
APU (Auxiliary unit)
Alternator (Integrated Drive Generators)
Transformers-rectifiers (TR)
Electronic inverter DC-AC
External power
Random air turbine (RAT)
Emergency generator
Hydraulic circuits (Green, blue, yellow
POWER NETWORK
DC BAT bus
DC BUS1 – DC BUS2
DC ESS BUS (emergency bus)
AC BUS1
AC ESS bus (emergency bus)
AC BUS2
BUS TIE contactor
AINT bus (Ground handling bus)
SYSTEM SUPERVISION SIMULATIONS
ELECTRICAL PROBLEMS HANDLING
STATUS
Park
Airport service support
APU power supply
APU engine starting
Take off
Landing
TECHNICAL SPECIFICATIONS
The system is arranged on a silk-screen,
panel provided with:
 Color silk screen panel
 Selection of the operational conditions
with switches and pushbuttons
 Displays and LED visualization
 Dynamic display of the parameters, on
the computer screen, with high graphic
performance software (LabVIEW)
 USB connection with the computer
Power supply: 230 Vca 50 Hz single-phase 50 VA (Other voltage & frequency under
request)
LHP 601 AVIATION & AERODYNAMICS
AVIATION SYSTEMS
AQ-2 Simulator
Twin-engine Aircraft Hydraulic System
The aircraft hydraulic system simulator
mod. AQ-2, is included in a complete set of
educational equipment for the basic
training on aircraft systems. The simulator
consists of a computer-assisted panel, with
silk - screen mimic diagram for a clear
location of its components. Various zones
of the mimic diagram are represented
with different colors to emphasize peculiar
aspects of the system. Light and displays
indicators, installed in the mimic diagram
enable to assess the evolutions of the
control.
The graphic display of the information
available at the control input, such as
aircraft status (park, APU…) on the
computer screen enables the permanent
monitoring of the system. The operational
conditions are set by students according to
the educational path indicated in the
courseware, carried out by the PC.
TRAINING PROGRAM
PRESSURE GENERATION
Engine
Driven Pump (green hydraulic
circuit)
Engine Driven Pump (yellow hydraulic
circuit)
Electric pump (blue hydraulic circuit)
Power Transfer Unit (PTU)
HYDRAULIC ACTUATORS
Green
circuit: Flaps, Rudder, Spoilers,
Nose wheel steering
Blue circuit: Spoilers, Rudder, Elevator
Yellow circuit: Elevator, Spoiler, Landing
gear
PRESSURE ACCUMULATOR
Circuit 1 accumulator
Circuit 2 accumulator
Circuit 3 accumulator
SYSTEM SUPERVISION SIMULATIONS
STATUS
Park
Airport service support
APU engine starting
HYDRAULIC PROBLEMS HANDLING
TECHNICAL SPECIFICATIONS
The system is arranged on a silk-screen,
panel provided with:
 Color silk screen panel
 Selection of the operational conditions
with switches and pushbuttons
 Displays and LED visualization
 Dynamic display of the parameters, on
the computer screen, with high graphic
performance software (LabVIEW)
 USB connection with the computer
Power supply: 230VAC, 50Hz single-phase 50VA (Other voltage and frequency under
request)
LHP 601 AVIATION & AERODYNAMICS
AVIATION SYSTEMS
AQ-3 Simulator
Twin-engine Aircraft Air Conditioning
And Pressurization System
The aircraft air conditioning and
pressurization simulator mod. AQ-3, is
included in a complete set of educational
equipment for the basic training on aircraft
systems. The simulator consists of a
computer-assisted panel, with silk - screen
mimic diagram for a clear location of its
components. Various zones of the mimic
diagram are represented with different
colors to emphasize peculiar aspects of
the system. Light and displays indicators,
installed in the mimic diagram enable to
assess the evolutions of the control. The
graphic display of the information
available at the control input, such as
aircraft status (park, APU…) on the
computer screen enables the permanent
monitoring of the system.
The operational conditions are set by
students according to the educational
path indicated in the courseware, carried
out by the PC.
TRAINING PROGRAM
 AIR INTAKE
BLEED valve 1 and 2
FAN AIR VALVE 1 AND 2
APU BLEED valve
External group
Cross BLEED valve
 AIR CONDITIONING CIRCUIT
PACK 1 and 2
HEAT EXCHANGER 1 and 2
COMPRESSOR 1 and 2
AIR distribution
 AIR PRESSURIZATION
OUTFLOW valve
Pressurization profile
 SYSTEM SUPERVISION SIMULATIONS
 STATUS
Park
Airport service support
APU bleed
PACK 1 and 2
Engine starting
Pressurization cycle
 AIR MANAGEMENT PROBLEMS HANDLING
TECHNICAL SPECIFICATIONS
The system is arranged on a silk-screen,
panel provided with:
 Color silk screen panel
 Selection of the operational conditions
with switches and pushbuttons
 Displays and LED visualization
 Dynamic display of the parameters, on
the computer screen, with high graphic
performance software (LabVIEW)
 USB connection with the computer
Power supply: 230VAC, 50Hz single-phase 50VA (Other voltage and frequency under
request)