Adaptable Automatic Nacelle Conversion for Tilt Rotor Aircraft
Adaptable Automatic Nacelle Conversion for Tilt Rotor Aircraft
- Neue Suche nach: KOWALSKI JACOB
- Neue Suche nach: GRILL IVAN
- Neue Suche nach: SEMINOLE ROBERT T
- Neue Suche nach: KOWALSKI JACOB
- Neue Suche nach: GRILL IVAN
- Neue Suche nach: SEMINOLE ROBERT T
Systems and methods for displaying to a tilt rotor aircraft pilot an optimum nacelle position and/or automatically controlling movement of the nacelles for the pilot. An automatic nacelle conversion function employs an active flight director speed mode to provide a current desired speed and a final speed. When the automatic nacelle conversion function is in a passive (uncoupled) mode of operation, the pilot follows visual cues, manually achieving the commanded nacelle position by rotating a thumbwheel. When in an active (coupled) mode of operation, the automatic nacelle conversion function provides a fully automatic nacelle controller requiring no pilot input. This automatic nacelle controller provides a variable nacelle rate along with several angle versus speed schedules tailored for different guidance speed modes and a wide range of aircraft configurations. The automatic nacelle conversion function is improved though the inclusion of altitude, rate of climb, and deceleration rate commands.
Dokumentinformationen
Adaptable Automatic Nacelle Conversion for Tilt Rotor Aircraft
2016-01-28
Patent
Elektronische Ressource
Englisch
| IPC: | G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes |
Ähnliche Titel
Adaptable automatic nacelle conversion for tilt rotor aircraft
| Europäisches Patentamt | 2016
Twin tilt nacelle V/STOL aircraft
| NTRS | 1984
Twin Tilt Nacelle V/STOL Aircraft
| SAE Technical Papers | 1984