Abstract: An aircraft passenger restraint and protection system including an aircraft seat mounted at an oblique angle to a direction of forward travel, a multi-point seat belt associated with the aircraft seat, and a structural mounted airbag located forward of the aircraft seat.

Abstract: An aircraft passenger seat comprises a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary, seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) so as to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4) and the secondary support surface (5) form a substantially flat and continuous surface wherein the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, said axis being translated between the reclined and subs

Abstract: An aircraft passenger seat comprises a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary, seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) so as to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4) and the secondary support surface (5) form a substantially flat and continuous surface wherein the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, said axis being translated between the reclined and subs

Abstract: An aircraft passenger seat having a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4), and the secondary support surface (5) form a substantially flat and continuous surface where the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, the axis being translated between the reclined and substantially fl

Abstract: An aircraft passenger seat having a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4), and the secondary support surface (5) form a substantially flat and continuous surface where the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, the axis being translated between the reclined and substantially fl

Abstract: An aircraft passenger seat comprises a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) so as to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4) and the secondary support surface (5) form a substantially flat and continuous surface wherein the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, said axis being translated between the reclined and subst

Abstract: An electrical connector, including a first electrically-conductive connector element, a second electrically-conductive connector element for being mated with the first connector element for allowing electrical current to flow through the electrical connector from an upstream to a downstream side, and a retainer for receiving and carrying the first connector element. The retainer includes locking anchors for mounting the retainer into complementary locking ports in a mounting bracket whereby the electrical connector is releasably carried on the mounting bracket. The retainer includes a retainer flange on which the locking anchors are mounted. The second connector element includes a connector flange for being mounted on an opposite side of the mounting bracket from the retainer. The connector flange has holes therein for receiving the locking anchors.

Abstract: An electrical connector, including a first electrically-conductive connector element, a second electrically-conductive connector element for being mated with the first connector element for allowing electrical current to flow through the electrical connector from an upstream to a downstream side, and a retainer for receiving and carrying the first connector element. The retainer includes locking anchors for mounting the retainer into complementary locking ports in a mounting bracket whereby the electrical connector is releasably carried on the mounting bracket. The retainer includes a retainer flange on which the locking anchors are mounted. The second connector element includes a connector flange for being mounted on an opposite side of the mounting bracket from the retainer. The connector flange has holes therein for receiving the locking anchors.