Analogue Computers For Vehicles TRIZ Cases

Segmented hysteresis points define dynamic buffer zones around operating points, preventing rapid mode switching and inaccurate data extrapolation.

A control method monitors supercapacitor cell temperature and voltage to limit function availability when thresholds are exceeded.

A sliding mode control system adjusts fuel injection quantity and gas flow rates through a microcomputer-controlled engine unit.

Alphanumeric and graphical displays on flight control computers show real-time engine thrust levels during automated quiet climb operations.

A control unit switches intake air amounts to stabilize engine speed during idle operation.

A control system switches between multiple torque power curves based on detected engine load to optimize fuel economy and performance.

Roadside laser systems analyze weight, vibration, and noise data to distinguish accident jams from congestion, enabling accurate distance alerts for drivers.

A voltage setting module adjusts alternator output based on brake pedal position during deceleration fuel cutoff events.

A vehicle control device calculates necessary heat and estimates supply to optimize engine operation.

A driving assist device uses received signal strength thresholds to notify drivers of nearby vehicles.

A vehicle communication system broadcasts personal data via direct short-range links to enable user profile matching.

A fuel economy mode module selectively triggers cylinder deactivation based on manifold absolute pressure thresholds.

A trajectory generation device shapes airport reference points into geometric turns and straight segments for automated aircraft guidance.

Aircraft sensors detect runway surface conditions using imaging and radar data, replacing delayed manual pilot reports with real-time automated updates.

Direct current measurement via a sensor replaces estimation models, resolving inaccuracies in power distribution.

A firing control unit alters engine firing sequences to reduce undesirable vibrations in skip fire internal combustion engines.

An avionic system uses a hash table to store airport operational parameters and links ground stations via a communication network.

Continuous crankshaft rotation maintains a hydrodynamic oil film during non-fueled engine modes to prevent metal-to-metal contact wear.

A vehicle occupant information controller calculates distance-to-empty readings using dynamic fuel economy baselines.

A hybrid vehicle control device calculates friction torque using generator power output in series mode to enable precise engine torque correction.

Performance simulator estimates total effective grade to identify haul route deficiencies and optimize productivity.

A taxiway collision alerting system calculates dynamic protection zones around aircraft using ADS-B data to predict potential ground conflicts.

Temperature sensors detect thermal anomalies in combustion zones, enabling fuel flexibility by preventing component damage from flashback events.

Internal exhaust gas recirculation traps exhaust gases to maintain intake manifold pressure and temperature.

A computer model adjusts engine performance parameters using core and bypass pressure ratios to determine specific fuel consumption.

Acoustic drivers perturb purge-air flow to eliminate pressure fluctuations and prevent hardware damage in pre-mixed combustors.

Processor translates verbal taxi instructions into graphical airport maps to resolve pilot confusion and runway incursions.

Inverting the conventional valve deactivation sequence minimizes trapped charge mass and pressure, reducing noise and vibration at low engine speeds.

A diesel throttle valve device adjusts air supply via EGR and throttle control to maintain desired airflow during idle operation.

A UAS guidance system fuses radar, TCAS, and electro-optical sensors to detect obstacles and generate autonomous 4D flight paths for safe navigation.

An intersection visibility determination device calculates conflict points to set specific assessment areas for approaching objects.

A signal control unit adjusts engine power output based on detected vehicle load mass to improve fuel economy.

Calculates predictive braking power and turnaround times for thrust reversers to assist pilot decision-making during landing.

A variable turbine geometry system closes to maximize exhaust pressure and decelerate engine speed during gear shifts.

An engine control unit dynamically tests and sets a mechanical-electrical confidence bit to optimize airflow modeling accuracy.

Controllers rotate turret assemblies to protect cameras from damage during unmanned aircraft belly landings.

An engine torque control device increases output torque during automatic transmission downshifting to synchronize engine speed with target values.

Dynamic variable extraction orifices reduce excessive cooling air usage, resolving the trade-off between turbine blade reliability and compressor efficiency.

A vehicle radar system estimates object size by calculating the collision angle from reflected electromagnetic waves.

Mobile devices mediate between sensors and processors, correcting errors to resolve accuracy-reliability contradictions.

A hydraulic control system modulates solenoid valve duty values to manage gear shift operations.

A diagnostic module requests minimum air per cylinder to control mass airflow for post converter oxygen sensor evaluation.

A processor converts 4D point cloud data into height maps to visualize safe landing zones in real time.

A navigation system creates blend meshes to interpolate traffic data between areas with and without real-time flow information.

Calibrates descent trajectory calculations with actual engine performance data to reduce fuel consumption caused by degradation.

A control valve balances pressure between series hydromotors, ensuring equal traction levels and automatic drive mode switching without manual intervention.

A control module manages engine speed using hand and foot throttle inputs.

A portable navigation apparatus integrates a fuel recording unit and refueling prompt unit to calculate forecasting fuel consumption.