Abstract: An apparatus (102) for applying a viscous material (162) to a surface (182) of a workpiece (180) is disclosed. The apparatus (102) comprises a channel (104) comprising an inlet (106) and an outlet (108). The channel (104) has a width CW that increases from the inlet (106) to the outlet (108). The apparatus (102) also comprises dividers (110) inside the channel (104). The channel (104) further comprises subdivisions (112) formed by the dividers (110). The subdivisions (112) of the channel (104) are in communication with the inlet (106) and the outlet (108) of the channel (104). At least one of the subdivisions (112) of the channel (104) has a width SW that increases from the inlet (106) of the channel (104) to the outlet (108) of the channel (104).

Abstract: An apparatus for applying a viscous material to a surface of a workpiece is disclosed. The apparatus comprises a channel comprising an inlet and an outlet. The channel has a width CW that increases from the inlet to the outlet. The apparatus also comprises dividers inside the channel. The channel further comprises subdivisions formed by the dividers. The subdivisions of the channel are in communication with the inlet and the outlet of the channel. At least one of the subdivisions of the channel has a width SW that increases from the inlet of the channel to the outlet of the channel.

Abstract: Systems and methods are provided for a thrust reverser. The thrust reverser may include one or more flapper doors. The flapper doors may be stored in a stored position within a housing portion of a nacelle of an aircraft propulsor. The flapper doors may then move to a deployed position (e.g., through rotation of the flapper doors or through other movements) when thrust reversing is desired. The aircraft propulsor may further include a thrust reverser door that covers an aperture within the nacelle. When the thrust reverser door is in an open position and the flapper doors are in the deployed position, airflow within the aircraft propulsor may be deflected by the flapper doors and out of the aircraft propulsor through the aperture.

Abstract: An apparatus (102) for applying a viscous material (162) to a surface (182) of a workpiece (180) is disclosed. The apparatus (102) comprises a channel (104) comprising an inlet (106) and an outlet (108). The channel (104) has a width CW that increases from the inlet (106) to the outlet (108). The apparatus (102) also comprises dividers (110) inside the channel (104). The channel (104) further comprises subdivisions (112) formed by the dividers (110). The subdivisions (112) of the channel (104) are in communication with the inlet (106) and the outlet (108) of the channel (104). At least one of the subdivisions (112) of the channel (104) has a width SW that increases from the inlet (106) of the channel (104) to the outlet (108) of the channel (104).