Wing for an aircraft and method of connection of a connection assembly

A wing for an aircraft, comprising:

• a main wing;
• and
• a high lift assembly comprising:
• a high lift body comprising a high lift structure;
• and
• a connection assembly comprising a slat track and a roller bearing that movably connects the high lift body to the main wing, such that the high lift body is movable between a retracted position and at least one extended position, and the connection assembly comprises a primary connector and a secondary connector,
• wherein the primary connector is mounted to the main wing via a primary mount profile and the secondary connector is mounted to the main wing via a secondary mount profile,
• wherein the primary connector is configurable to engage the primary mount profile, and the secondary connector is configurable to engage the secondary mount profile,
• wherein the primary connector is rotatable relative to the primary mount profile and at least one of the connection assembly and the main wing so as to configure the primary connector and mount profile between a decoupled configuration in which the primary connector may be moved into so as to be engaged with, and removed from so as to be disengaged from, the primary mount profile, and a locked configuration in which movement between the primary connector and the primary mount profile is restricted,
• wherein the primary mount profile is defined by a mounting sleeve with a circumferentially extending opening therein, and the primary connector comprises an elongate connector, and
• wherein the primary connector is positionable in the primary mount profile via the circumferential opening to engage with the primary mount profile.

A wing for an aircraft, comprising:

• a main wing;
• and
• a high lift assembly comprising:
• a high lift body comprising a high lift structure;
• and
• a connection assembly comprising a slat track and a roller bearing that movably connects the high lift body to the main wing, such that the high lift body is movable between a retracted position and at least one extended position, and the connection assembly comprises a primary connector and a secondary connector,
• wherein the primary connector is mounted to the main wing via a primary mount profile and the secondary connector is mounted to the main wing via a secondary mount profile,
• wherein the primary connector is configurable to engage the primary mount profile, and the secondary connector is configurable to engage the secondary mount profile,
• wherein the primary connector is rotatable relative to the primary mount profile and at least one of the connection assembly and the main wing so as to configure the primary connector and mount profile between a decoupled configuration in which the primary connector may be moved into so as to be engaged with, and removed from so as to be disengaged from, the primary mount profile, and a locked configuration in which movement between the primary connector and the primary mount profile is restricted,
• wherein the primary connector comprises a longitudinal axis, and the primary mount profile comprises a longitudinal axis, wherein the primary connector is configurable to engage with the primary mount profile such that the longitudinal axis of the primary mount profile is coincident with the longitudinal axis of the primary connector, and at least one of the primary mount profile and the primary connector is configurable to rotate about its longitudinal axis.