A cup holder retainer is provided. The cup holder retainer includes a support frame and a preloaded retainer clip. The preloaded retainer clip is connected to the support frame by a living hinge and an integral biasing element that biases the preloaded retainer clip into a cup-engaging position.

A storage cubby for an aircraft including a housing having a front opening and an interior space accessible through the front opening, a fixed retention bar extending across the front opening, and a beverage container holder positioned in the interior space. In embodiments, the beverage container holder includes a bearing block having a bearing surface, a positioning magnet mounted to the bearing block, a catch mounted to the bearing block, and a strap having a first end mounted to the housing and a second end carrying a magnetic latch. During a first use condition of the strap, the magnetic latch is retained by the positioning magnet disengaged from the catch. During a second use condition of the strap, the magnetic latch is engaged with the catch. In embodiments, the first and second use conditions correspond to routine and high g-force events of the aircraft, respectively.

A cup holder includes a holder main body having a retaining portion, the retaining portion being configured to receive and hold a beverage container on a bottom wall. The retaining portion includes an upper opening for receiving the beverage container, the bottom wall for supporting a bottom of the beverage container, and a side wall formed between the upper opening and the bottom wall, and has a cylindrical shape. An inner diameter at the upper opening is substantially the same as an inner diameter of the bottom wall.

A beverage holder (1) for a motor vehicle has a receptacle (2) with a side wall (5) extending from a bottom wall (3) to an open top (4) that is farther upward. At least one elastic compensation element (7) is provided for holding differently sized drinking vessels (6). The side wall (5) has at least one opening (8), and an elastic covering (10) penetrates the opening (8) due to its biasing to form the elastic compensation element (7).

The present invention in one or more embodiments provides a console support panel which includes a first portion defining a cavity to receive therein a pivot shaft of an inertia block; and a second portion positioned next to the first portion and to support a movable cover, wherein the first portion further includes a lead-in rib extending into the cavity to restrain translational movement of the pivot shaft. In certain embodiments, the lead-in rib includes first and second lead-in ribs to restrain translational movement of first and second ends of the pivot shaft, respectively.

A hinge mechanism includes a resin base member, and a support rotatably and pivotally mounted to the base member. The base member is formed by blow molding so as to be hollowed. The base member integrally includes a hinge member for rotatably and pivotally mounting the support to the base member. The hinge member is set in a molding die for clamping at the time of the blow molding of the base member, so as to be molded integrally with the base member.

According to one aspect of the present invention, an illuminated cupholder assembly is disclosed. The assembly comprises an upper portion comprising a lower mating portion forming a first diameter and a base portion comprising an upper mating portion forming a second diameter. A light ring is disposed substantially between the lower mating portion and the upper mating portion in an assembled configuration. The cupholder assembly comprises a photoluminescent portion configured to convert a first wavelength to a second wavelength to illuminate at least a portion of the cupholder assembly.

A storage cubby for an aircraft including a housing having a front opening and an interior space accessible through the front opening, a fixed retention bar extending across the front opening, and a beverage container holder positioned in the interior space. In embodiments, the beverage container holder includes a bearing block having a bearing surface, a positioning magnet mounted to the bearing block, a catch mounted to the bearing block, and a strap having a first end mounted to the housing and a second end carrying a magnetic latch. During a first use condition of the strap, the magnetic latch is retained by the positioning magnet disengaged from the catch. During a second use condition of the strap, the magnetic latch is engaged with the catch. In embodiments, the first and second use conditions correspond to routine and high g-force events of the aircraft, respectively.

A vehicle feature includes a wall having a wall surface formed from a first material and an opening extending through the wall surface. An insert is mounted to the wall surface. The insert is formed from a second material. The insert includes a wall member having a first side facing the wall surface and a second side facing away from the wall surface. The first side includes at least one connector element that engages with the wall surface through the opening. The insert is covered in a third material that is distinct from the first material and the second material.