Abstract: An aircraft flooring system for an aircraft fuselage adapted to secure a payload component may include first and second seat tracks extending longitudinally with respect to the aircraft fuselage, the first and second seat tracks being spaced from one another; and an intercostal assembly extending between the first and second seat tracks. The intercostal assembly can include a first intercostal having a center member having a first end and a second end and a top flange including a mounting region between the first and second ends; and at least first and second tab members. The first tab member can be coupled to the top flange toward the first end of the center member and the second tab member can be coupled to the top flange toward the second end of the center member. The first and second tab members can extend beyond the first and second ends of the center member, respectively, and be configured to be coupled to the first and second seat tracks.

Abstract: An aircraft flooring system for an aircraft fuselage adapted to secure a payload component may include first and second seat tracks extending longitudinally with respect to the aircraft fuselage, the first and second seat tracks being spaced from one another; and an intercostal assembly extending between the first and second seat tracks. The intercostal assembly can include a first intercostal having a center member having a first end and a second end and a top flange including a mounting region between the first and second ends; and at least first and second tab members. The first tab member can be coupled to the top flange toward the first end of the center member and the second tab member can be coupled to the top flange toward the second end of the center member. The first and second tab members can extend beyond the first and second ends of the center member, respectively, and be configured to be coupled to the first and second seat tracks.

Abstract: A door apparatus includes a door, actuating mechanism, and tie rod mechanism, the actuating mechanism actuating the tie rod mechanism to impart a substantially translating motion to the door. The actuating mechanism can include a drive yoke coupled to the tie rod mechanism with a one-way coupling. The tie rod mechanism can include a primary tie rod coupled to a secondary tie rod coupled to a latch. In another aspect a door apparatus includes an actuator, a first door, a second door, a first linkage assembly coupling the actuator to the first door, and a second linkage assembly coupling the first door to the second door, the actuator configured to activate the first linkage assembly to move the first door, the first door imparting motion to the second linkage assembly to move the second door in a synchronous and opposite motion with respect to the motion of the first door.

Abstract: An aircraft elevator system includes a fixed frame, a floating frame coupled to the fixed frame, and a cabin coupled to the floating frame. The floating frame can move with respect to the fixed frame and the cabin can move with respect to the floating frame. The system can include an actuating system operating at least one pulley system to move the cabin between upper and lower positions, which respectively can be inside and outside the aircraft. In some embodiments, the system includes a support assembly that moderates or eliminates load transfer between the system and an aircraft upper deck floor structure. In some embodiments, the cabin includes a ramp configured to deploy when approaching the lower position and to retract to a stowed position when the cabin moves from the lower position toward the upper position. The ramp can include a sensor to control cabin movement.

Abstract: One particular overhead space utilization device, adapted for installation in a hull structure, incorporates at least one berth module with first and second berth portions, first and second intermediate support members, and first and second coupling members. Each berth module has two opposing berth members with a walkway therebetween. The first and second intermediate support members each has a first end pivotably coupled to the corresponding one of the first and second berth portions, and a second end configured to be pivotably coupled to the hull structure. The first and second coupling members are configured to pivotably couple the second berth portions to the hull structure. The first and second coupling members and the second berth portions are configured to be positioned outboard of the first berth portion.

Abstract: An aircraft elevator system includes a fixed frame, a floating frame coupled to the fixed frame, and a cabin coupled to the floating frame. The floating frame can move with respect to the fixed frame and the cabin can move with respect to the floating frame. The system can include an actuating system operating at least one pulley system to move the cabin between upper and lower positions, which respectively can be inside and outside the aircraft. In some embodiments, the system includes a support assembly that moderates or eliminates load transfer between the system and an aircraft upper deck floor structure. In some embodiments, the cabin includes a ramp configured to deploy when approaching the lower position and to retract to a stowed position when the cabin moves from the lower position toward the upper position. The ramp can include a sensor to control cabin movement.

Abstract: A door apparatus includes a door, actuating mechanism, and tie rod mechanism, the actuating mechanism actuating the tie rod mechanism to impart a substantially translating motion to the door. The actuating mechanism can include a drive yoke coupled to the tie rod mechanism with a one-way coupling. The tie rod mechanism can include a primary tie rod coupled to a secondary tie rod coupled to a latch. In another aspect a door apparatus includes an actuator, a first door, a second door, a first linkage assembly coupling the actuator to the first door, and a second linkage assembly coupling the first door to the second door, the actuator configured to activate the first linkage assembly to move the first door, the first door imparting motion to the second linkage assembly to move the second door in a synchronous and opposite motion with respect to the motion of the first door.

Abstract: An aircraft elevator system includes a fixed frame, a floating frame coupled to the fixed frame, and a cabin coupled to the floating frame. The floating frame can move with respect to the fixed frame and the cabin can move with respect to the floating frame. The system can include an actuating system operating at least one pulley system to move the cabin between upper and lower positions, which respectively can be inside and outside the aircraft. In some embodiments, the system includes a support assembly that moderates or eliminates load transfer between the system and an aircraft upper deck floor structure. In some embodiments, the cabin includes a ramp configured to deploy when approaching the lower position and to retract to a stowed position when the cabin moves from the lower position toward the upper position. The ramp can include a sensor to control cabin movement.

Abstract: A door apparatus includes a door, actuating mechanism, and tie rod mechanism, the actuating mechanism actuating the tie rod mechanism to impart a substantially translating motion to the door. The actuating mechanism can include a drive yoke coupled to the tie rod mechanism with a one-way coupling. The tie rod mechanism can include a primary tie rod coupled to a secondary tie rod coupled to a latch. In another aspect a door apparatus includes an actuator, a first door, a second door, a first linkage assembly coupling the actuator to the first door, and a second linkage assembly coupling the first door to the second door, the actuator configured to activate the first linkage assembly to move the first door, the first door imparting motion to the second linkage assembly to move the second door in a synchronous and opposite motion with respect to the motion of the first door.