Selectively actuated flight simulation system for trainer aircra

Aeronautics and astronautics – Retarding and restraining devices – Aerodynamic retarders

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Details

244203, 244213, B64C 932

Patent

active

043725074

ABSTRACT:
This invention generally concerns an aircraft useful for training pilots, and specifically involves providing a trainer aircraft having high to moderate aspect ratio wings with selectively operable design features that impart to the trainer aircraft the handling characteristics of a high performance, swept wing aircraft in an approach and landing configuration. In particular, the high performance swept wing aircraft characteristics are preferably imparted by selectively actuated primary and secondary speed brake mechanisms. Optimally, the primary speed brake mechanism is positioned as a function of angle of attack of the aircraft.

REFERENCES:
patent: 2005965 (1935-06-01), Barnhardt
patent: 2239854 (1941-04-01), McCormick
patent: 2344945 (1944-03-01), Knox et al.
patent: 2381957 (1945-08-01), Ibarra
patent: 2744173 (1956-05-01), Grosse-Lohmann
patent: 2943823 (1960-07-01), Mullins et al.
patent: 3480040 (1949-08-01), Mitchell
patent: 3589648 (1971-06-01), Gorham et al.
patent: 3945593 (1976-03-01), Schanzer

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