A collapsible stabilizer assembly to provide directional stability to a windmill or an aircraft is disclosed. The collapsible stabilizer assembly comprises at least one fin 200 having a leading member 202 and a trailing member 204 respectively coupled with a first tube 104 and a second tube 106 that are pivotally fixed to frame 102 of the aircraft. The leading member 202 includes a first hole 208 for engaging a fastening member 302 when the first hole 208 is in alignment with a second hole 108 that is configured in the first tube 104 so as to couple the leading member 202 and the first tube 104. Coupling of the leading member 202 and the trailing member 204 with the first tube 104 and the second tube 106 respectively allows quick installation as well as removal of the at least one fin 200 from the frame 102.
COLLAPSIBLE STABILIZER ASSEMBLY FOR AN AIRCRAFT
2021-04-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |