Structural Life Monitoring Unit TL-5824 is a unique unit for aircraft operational data acquisition or its parts. It enables monitoring and evaluating residual life of several critical places in an aircraft structure. The residual life evaluation process is based on in-time measurement of vertical "G", which is recalculated on the stress spectra in the aircraft structure critical places. The unit offers great benefits for airplane manufacturers, flight schools or other aircraft operators in order to monitor airplane's operation and its structural life. This feature of the Structural Life Monitoring Unit can be useful e.g. for flights schools, where the same type of airplanes is operated in different ways (aerobatics, training, navigation flights etc.). Aircraft manufacturers will appreciate simple monitoring of even a huge number of airplanes.
Price: On Request
- residual life calculation after each flight and display of the value of residual life in %
- measures operational 'g' acceleration on the vertical axis and air speed
- set the limit values at two levels (Warning and Alarm) for 'g' acceleration
- always be informed on the 'g' acceleration reaching the limits, which could result in a damage to the aircraft
- use the complete flight data-log with the date, flight time, GPS position, number of landings, and the maximum and minimum 'g' acceleration reached during each flight
- be informed from the aircraft manufacturer by an SMS message directly on the display on newly-issued bulletins, servicing requirements, etc.
- in case of the manipulation with your aircraft or its parts, the TL-5824 will send you an SMS message and also call to inform you by a voice mail, e.g. "Help! Somebody is stealing me"
- enables downloading of the measured values and flight data-log using a PC or
- wireless downloading of the measured values at any time and anywhere in the world
Basic functions:
- display immediately the maximum 'g' acceleration reached, by pressing the button on the Display unit
- display immediately the Air speed by pressing the button on the Display unit
- display immediately the time to TBO by pressing the button on the Display unit
- display immediately the SMS from the aircraft producer by pressing the button on the Display unit
- using your PC, download at any time the history of the measured 'g' acceleration from the Structural life-monitoring unit
- connect the Display unit to the output of the signalisation unit, which will warn you of the exceeded 'g' acceleration limits
- connect your Structural life-monitoring unit with the Intercom or Voice module using the iFamily® Bus and gain the option of having a voice alert of the exceeded limits
- the latest version of the firmware is automatically downloaded from the server of TL elektronic
Other functions:
- designed for all types of aircraft
- measures the stress in the critical places of the aircraft structure etc.
- incorporates aircraft service records - so-called service book
- enables the wireless remote control of the aircraft starter or the magnetos, e.g. in case of a theft
- enables wireless downloading of the firmware to the instrument according to requirements, e.g. an aircraft manufacturer or an IT office
- record of the whole aircraft operation, 'g' spectra cumulatively written in the 'two-parametric' form
- ability to provide strain-gauge measurements and fatigue evaluation according to the measured stress
- high-precision measurement
- 100 hour memory with 100 SchecK® drawers and 100 Line
Technical parameters:
- voltage: 10.0 to 32.0 Volts
- current consumption: 5 to 1.500 mA @ 14 Volts
- frequency: EUROPE 900/1800MHz or USA 1900 MHz
- alarm signal active to the aircraft ground
- maximal voltage and signal current for locking relay: 30 Volts, 1 Ampere
- measurement: +/-1%
- measuring range: +/- 15g
- resolution: 0.1g
- operating: -20°C to 70°C (-4°F to 158°F) temperature range
- relative humidity: 95% without condensation
- load: +/-20 g
- vibration: 1 to 200 Hz
- weight: 450 grams (0,99 lbs)
- dimensions: 150x100x50 mm (5.905x3.937x1.968 inch)
- internal speed sensor 20 to 350km/h (10 to 189 knots)
- output status signal: grounded, max. 0.5 Amps
- communication line with a PC via standard USB2.0