Digital Stab Trim Update

B727 & B737

 

 

        Present simulation techniques used to model the Boeing 727 and 737 stabilizer trim utilize a maintenance intensive system of hydraulic motors, clutches, limit switches, brakes and other gear driven mechanisms to provide proper operation. By digitizing the stabilizer trim system model, a significant reduction in actual physical linkage and moving components has been realized. We have simplified the mechanical system, provided an easily adjustable detailed mathematical model and added an automatic calibration feature to provide the customer a state of the art system, which requires a minimum of maintenance. A simple chain driven electric motor replaces a pair of complicated hydraulic loader assemblies, and all of the aircraft components are modeled in our high-speed DCL computational system. Our digital stab trim update provides a simple, reliable, virtually maintenance free electromechanical system utilizing state of the art, commercial off the shelf hardware. We have removed the two hydraulic/mechanical loaders, and replaced them with a single main drive electric actuator consisting of a high tech DC motor assembly and a sprocket set connected by a chain. The stabilizer trim indicator on the pedestal has been separated from the main drive to provide ATG and IP enhancements. The indicator is driven by a DC servo motor gearbox in combination with a PWM servo amplifier. All of the aircraft stab trim mechanical components (clutch, manual override, aero force, physical limits and motor operation in main, cruise and auto pilot trim) are modeled digitally at an iteration rate of 2048 Hz using simple straight forward techniques in the 'C' programming language. A Digital Control Loading (DCL) computer designed to our stringent specifications provides an extra measure of reliability when mounting is required onboard the simulator. An Intel Pentium processor insures that we have the computational power required to realistically model the dynamic characteristics of the actual aircraft system being simulated. The only moving parts on this computer are the two air circulation fans, as the hard drive is actually a solid-state flash memory device without any moving parts. Every single component used in this system is a commercially available off the shelf (COTS) item. We have produced a product, which ensures a long service life and provides alternative sources for interchangeable parts replacement.

 

Stab Trim System Description

 

       The electric actuator assembly consists of a high performance DC servo motor fitted with a resolver to provide velocity and position feedback for inner loop control, actuator housing, and a chain and sprocket assembly. This unit does not require any setup or adjustments An 80 VDC power supply assembly houses an isolation transformer, a reservoir capacitor, a full wave rectifier, and a PWM DC servo amplifier. A dual color status lamp on the amplifier indicates the state of readiness; a green light is the normal mode for operation. A red light indicates an amplifier fault or inhibit. A power relay, two 25 amp 250V fuses and a red indicator light are housed in the safety relay assembly, which is a metal box mounted to the frame near the high voltage DC power supply. A watchdog timer in conjunction with the control loading turn on logic actuates this relay and the corresponding red indicator light. If the computer should halt, or if hydraulic power is removed from the control loading system through the pedestal switch or the IOS, this relay will disconnect power to the main drive motor and extinguish the indicator light. An electric DC servo motor with a 12.5:1 gearbox is used to drive the stab trim position indicator. The motor assembly drives the indicator through a set of bevel gears. Position feedback is provided through a 50:1 miniature gearbox attached to a Midori 5Kohm film type potentiometer. No setup is required for the indicator assembly. A PWM DC servo amplifier provides the control current required to drive the indicator motor assembly. This amplifier contains a red fault light which when lit, indicates a problem with the unit. An Isobar premium surge suppresser mounted to the DCL computer provides AC distribution, surge protection and diagnostic indicators which monitor line voltage and polarity of the AC input. The DCL computer and the indicator drive amplifier are connected to this unit The Analog Interface Module (AIM) is mounted on the DCL computer, it provides an expandable interface which is easily modified in the event that any changes are deemed necessary. A 6VDC relay is installed to provide an inhibit signal to the indicator amplifier. The DCL computer is an industrial rack mount computer with a 300 watt power supply, a 14 slot backplane, and two cooling fans. This chassis is specifically designed to endure the rigors of onboard simulator operation. All circuit cards are secured in their respective slots with multiple hold down attachment points. A filter is mounted in front of the intake fan on the front of the computer behind the intake grill. This filter should be checked bi-monthly to insure that there is no significant blockage present A Pentium 850 MHz single board computer (SBC) is utilized for computational processing. Our custom high speed executive provides a 2048 Hz frame rate which allows ample processing time for stab trim modeling and I/O control. Debug and plot routines are provided running as embedded background tasks. A Flash drive hard disk is provided with this system. This flash drive is basically a 16 megabyte solid state EEPROM chip set with no moving parts. The executable program (aastab.exe) resides on this flash ROM which is drive C. The autoexec.bat file has been modified such that the executable program will start immediately after boot up. A high speed PCI video card is used to display debug and plotting information, system status, and timing information via the monochrome monitor provided

 

 

 

 

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