发明名称 Earthbound landing gear for aircraft take=off and landing - has carriage on rails with hydraulic capture-release elements, speed matching controllers
摘要 The earthbound landing gear arrangement has a carriage (2) which bears the aircraft (1) during take-off and landing and whose speed is matched to that of the aircraft via an inductive electrical linear drive. The carriage is guided on a rail (4) forming a take-off and landing strip and carries hydraulic capture (3) devices with latching elements which can be coupled with and released from the aircraft during the landing and launch phases. The aircraft and carriage contain controllers for speed matching, buffers in the capture devices and the latching elements during each phase. USE/ADVANTAGE - Esp. for launching and landing large aircraft. Enables maximum safety to be achieved with very small landing strip area.
申请公布号 DE4102271(A1) 申请公布日期 1992.07.30
申请号 DE19914102271 申请日期 1991.01.26
申请人 DEUTSCHE AIRBUS GMBH, 2000 HAMBURG, DE 发明人 MUELLER, HANS-JUERGEN, 2359 HENSTEDT-ULZBURG, DE;GROSSE-PLANKERMANN, 2153 NEU WULMSTORF, DE
分类号 B64F1/10 主分类号 B64F1/10
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