An aircraft canopy comprises first and second canopy portions, wherein the first canopy portion includes a leading edge having a sawtooth shape and wherein the second canopy portion has a trailing edge complementary to the shape of the front bow edge. An interconnect structure is disposed between the leading edge and the trailing edge and maintains the first and second canopy portions in assembled relationship.
AIRCRAFT CANOPY WITH IMPROVED PERFORMANCE AND REDUCED LIFECYCLE COST
01.08.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT CANOPY WITH IMPROVED PERFORMANCE AND REDUCED LIFECYCLE COST
Europäisches Patentamt | 2024
|Improved performance with reduced cost
IuD Bahn | 2001
|NTIS | 1964
|NTRS | 1985
|Lifecycle cost saving benefits
Online Contents | 2012
|