Temporarily-installed aircraft observer door plug, chair, sonotube ejection and control system
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United States of America Patent
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Oct 10, 2017
Issued Date -
N/A
app pub date -
Feb 13, 2017
filing date -
Oct 15, 2007
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
In one embodiment, a temporarily-mounted control system is installed in an aircraft. The temporarily-mounted control system includes a temporary door plug assembly that is adapted to in an opening in a fuselage of the aircraft, such as an opening created by removing a door in the fuselage. The temporary door plug is connected to a retraction rail assembly that connects the temporary door plug and the fuselage. One or more workstation assemblies is mounted to the floor of the aircraft using mounting plates that are attached to adaptive floor plates connected to the floor of the aircraft. An observer chair assembly is connected to the floor of the aircraft and to the workstation assemblies.
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