Aircraft capture systems

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

Patent

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Details

244110R, B64C 2568

Patent

active

050547178

ABSTRACT:
An aircraft capture system, e.g. for a radio-controlled pilotless aircraft (19), having at the homing station a boom arrangement (13) mounted for rotation about a vertical hinge axis (A--A) and having appreciable flexibility under forces acting perpendicular to the hinge axis while being substantially inflexible under forces acting parallel to the hinge axis. The flexibility of the boom arrangement cushions the aircraft against shock when an arrester hook (33) deployed from the aircraft engages the boom arrangement via an arrester wire (15) attached to the boom arrangement.

REFERENCES:
patent: 584152 (1897-06-01), Campbell
patent: 614756 (1898-11-01), Perkins
patent: 835404 (1906-11-01), Cramer
patent: 880609 (1908-03-01), Watts
patent: 991838 (1911-05-01), Feist
patent: 1056449 (1913-03-01), Ponton
patent: 1084579 (1914-01-01), Jenkins
patent: 1224433 (1917-05-01), West
patent: 4311290 (1982-01-01), Koper

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