The invention relates to a ramp of a catapult and to a catapult. The catapult comprises a carriage (4) for fastening an aircraft (5). The carriage (4) is supported on a ramp (1). The ramp is formed of one or more ramp elements (1a - 1m). The ramp element comprises four frame plates, namely two parallel side plates (20a, 20b), a top plate (21) and a bottom plate (22). The frame plates are separate pieces which are connected at fastening points (25) to each other by means of mechanical fastening elements (26).
Catapult ramp for launching UAVs
2018-05-30
Patent
Electronic Resource
English
Engineering Index Backfile | 1931
|Catapult for launching aeroplanes
Engineering Index Backfile | 1932