Aeronautics and astronautics – Aircraft structure – Fuselage and body construction
Patent
1988-10-11
1990-01-09
Basinger, Sherman D.
Aeronautics and astronautics
Aircraft structure
Fuselage and body construction
1562726, 427 39, B64C 114
Patent
active
048922714
ABSTRACT:
Apparatus for and a method of rendering selected areas 17, 18 of an aircraft canopy 2 receptive to an adhesive by means of which a detonating cord 7 is attached in loop form to the canopy, to facilitate fracture of the canopy for pilot ejection in an emergency, comprises pretreating those areas 17, 18 by corona discharge. The canopy 2 is mounted in a jig 10 shaped to conform with the canopy and having rebates 11 for accommodating discharge electrodes 12 located at a distance from the canopy 2. A pump 16 is provided to remove ozone formed due to the discharge and trapped between the canopy 2 and the jig 10.
REFERENCES:
patent: 2876358 (1959-03-01), Root
Basinger Sherman D.
British Aerospace PLC
Corl Rodney
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