Nacelle with thrust reverser

A nacelle for an aircraft, comprising:

• an outer casing having a longitudinal axis;
• a translating cowl cooperating with the outer casing to define an outer boundary of a bypass passage configured to surround an engine, the translating cowl movable relative to the outer casing along the longitudinal axis;
• a blocking panel connected to the outer casing by a pivot connection and connected to the translating cowl by a sliding connection, the sliding connection including an engagement member slidingly engaged in a track, the track having a first portion parallel to the longitudinal axis and a second portion non-parallel to the longitudinal axis and extending from the first portion toward the longitudinal axis, the track being connected to the blocking panel, the engagement member protruding from the translating cowl;
• wherein the translating cowl and the blocking panel define at least part of a thrust reverser selectively configurable between:
• a closed configuration where the translating cowl abuts the outer casing, the blocking panel has a stowed position radially outwardly of the bypass passage, and the engagement member is located in the first portion of the track,
• a deployed configuration where the translating cowl is spaced a first distance from the outer casing so as to define an opening therebetween, the blocking panel has a pivoted position within the bypass passage adjacent the opening to direct a flow toward the opening, and the engagement member is located in the second portion of the track, the blocking panel pivoting about the pivot connection to move between the stowed and pivoted positions, and
• an intermediate configuration between the closed and deployed configurations, wherein in the intermediate configuration, the translating cowl is spaced a second distance smaller than the first distance from the outer casing, the blocking panel is in the stowed position, and the engagement member is located at a junction between the first and second portions of the track.

A nacelle for an aircraft, comprising:

• an outer casing having a longitudinal axis;
• a thrust reverser including:
• a translating cowl, the outer casing and translating cowl cooperating to define an outer boundary of a bypass passage configured to surround an engine, the translating cowl movable relative to the outer casing along the longitudinal axis between a closed position and an open position, the translating cowl in the open position being axially spaced from the outer casing so as to define an opening between the translating cowl and the outer casing;
• and
• a blocking panel pivotable about a pivot connection between a stowed position and a pivoted position, the blocking panel in the pivoted position extending within the bypass passage adjacent the opening to direct a flow toward the opening;
• wherein the blocking panel is connected to the translating cowl by a sliding connection including an engagement member slidingly engaged in a track, the track having a first portion parallel to the longitudinal axis and a second portion non-parallel to the longitudinal axis and extending from the first portion away from the longitudinal axis, the track being connected to the translating cowl, the engagement member protruding from the blocking panel;
• wherein motion of the translating cowl along the longitudinal axis slides the engagement member within the track, the motion of the translating cowl being performed without moving the blocking panel when the engagement member is within the first portion of the track, the motion of the translating cowl causing the blocking panel to pivot about the pivot connection when the engagement member is within the second portion of the track.

A nacelle for an aircraft, comprising:

• an outer casing having a longitudinal axis;
• a translating cowl cooperating with the outer casing to define an outer boundary of a bypass passage configured to surround an engine, the translating cowl movable relative to the outer casing along the longitudinal axis;
• a blocking panel connected to the outer casing by a pivot connection and connected to the translating cowl by a sliding connection, the sliding connection including an engagement member slidingly engaged in a track, the track having a first portion parallel to the longitudinal axis and a second portion non-parallel to the longitudinal axis and extending from the first portion away from the longitudinal axis, the track being connected to the translating cowl, the engagement member protruding from the blocking panel;
• wherein the translating cowl and the blocking panel define at least part of a thrust reverser selectively configurable between:
• a closed configuration where the translating cowl abuts the outer casing, the blocking panel has a stowed position radially outwardly of the bypass passage, and the engagement member is located in the first portion of the track,
• a deployed configuration where the translating cowl is spaced a first distance from the outer casing so as to define an opening therebetween, the blocking panel has a pivoted position within the bypass passage adjacent the opening to direct a flow toward the opening, and the engagement member is located in the second portion of the track, the blocking panel pivoting about the pivot connection to move between the stowed and pivoted positions, and
• an intermediate configuration between the closed and deployed configurations, wherein in the intermediate configuration, the translating cowl is spaced a second distance smaller than the first distance from the outer casing, the blocking panel is in the stowed position, and the engagement member is located at a junction between the first and second portions of the track.