SECTION DIVIDER ASSEMBLY FOR A VEHICLE

A section divider system is configured to separate sections within an internal cabin (30) of a vehicle (10). The section divider system may include a first rail secured to a fixed panel (302) within the internal cabin (30). A closeout panel (400) may be secured to the fixed panel (302). The closeout...

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Hauptverfasser:	HEROLD, WILLIAM F, NGUYEN, HUNG QUANG, BASS, KEVIN DUANE, SCHWITTERS, CHRISTOPHER L, WALTON, BRENT CLARENCE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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creator	HEROLD, WILLIAM F NGUYEN, HUNG QUANG BASS, KEVIN DUANE SCHWITTERS, CHRISTOPHER L WALTON, BRENT CLARENCE
description	A section divider system is configured to separate sections within an internal cabin (30) of a vehicle (10). The section divider system may include a first rail secured to a fixed panel (302) within the internal cabin (30). A closeout panel (400) may be secured to the fixed panel (302). The closeout panel (400) extends between the fixed panel (302) and a passenger service unit (PSU) (406) within the internal cabin (30). A clearance space (440) is formed between a portion of the closeout panel (400) and the PSU (406). The closeout panel (400) is configured to prevent access to an interior of the PSU (406). A bracket is secured to the first rail. One or more connecting beams extend from the bracket through the clearance space (440). A section divider assembly (130) is connected to the connecting beam(s). (Fig. 9)
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The section divider system may include a first rail secured to a fixed panel (302) within the internal cabin (30). A closeout panel (400) may be secured to the fixed panel (302). The closeout panel (400) extends between the fixed panel (302) and a passenger service unit (PSU) (406) within the internal cabin (30). A clearance space (440) is formed between a portion of the closeout panel (400) and the PSU (406). The closeout panel (400) is configured to prevent access to an interior of the PSU (406). A bracket is secured to the first rail. One or more connecting beams extend from the bracket through the clearance space (440). A section divider assembly (130) is connected to the connecting beam(s). 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subjects	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
title	SECTION DIVIDER ASSEMBLY FOR A VEHICLE
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