The reinforcement sash should be integrally formed.

Since the reinforcing frame (3) is fit in a fitting cutout (1d) formed in the rear surface of the rim-like frame (10), the reinforcing frame can be easily mounted.

A reinforcement frame (20) is then disposed between the two articles.

The reinforcing frame (3) is not embedded in the buffer material.

The reinforcement frame may be a honeycomb plastic frame and enclosed by a fabric material.

Disclosed is a reinforcement frame (38) fixed to an outer package (37) of a heated component unit in a display (69), wherein a first heat dissipation fin is included in the reinforcement frame (38).

The handle is configured by having at least a part of a rear section reinforcing frame (21) and a front section reinforcing frame (22) protruding to the inside, said frames configuring the edges of the opening (17).

The invention relates to an aircraft fuselage structure comprising a circumferential reinforcing frame (2) and a plurality of stringers (3) substantially perpendicular to the frame.

The reinforcing frame (32) is affixed to the main frame (10) by means of fasteners (108, 109).

Further, the buffer material does not come into contact with the reinforcing frame (3) to remain unworn.

The sealing resin (4) and the reinforcing frame (5) are formed by transfer molding a synthetic resin.

The reinforcing frame (31) has a recessed portion (31d) in a region which corresponds to the touch sensor electrode (47) and the connector (67).

The invention relates to a system for transmitting stresses at the intersection between a reinforcing frame and a stiffener in a fuselage and to a method for producing one such system.

This allows for longer lasting performance, elimination of frame reinforcement members, more glass area with larger window openings and a slimmer frame.

The round reinforcement frame is integrated with the frame.