Invention Grant
US09097209B2 Gas turbine engine thrust reverser system 有权
燃气轮机反推系统

Gas turbine engine thrust reverser system
Abstract:
A gas turbine engine thrust reverser system includes a fan nacelle having a fixed portion and a movable portion configured to move relative to the fixed portion between opened and closed positions in response to a command to selectively provide an opening between the fixed and movable portions. A fan case is arranged within the fan nacelle. The fan case includes an integral bull nose adjacent to the opening in the open position and to the movable portion in the closed position. The bull nose has a curved wall sloping radially outward.
Public/Granted literature
Information query
Patent Agency Ranking
0/0