Elemento de armação, sistema de condicionamento de ar da aeronave, e, método para a instalação de um elemento de armação em uma aeronave

The frame element (10) has a pair of longitudinal hollow struts (12,14) that are connected together using connection struts (16,18). Each longitudinal strut has air inlet connection (12a,14a) connected to the air outlet duct of the aircraft air-conditioning unit and air outlet connection (12b,14b) c...

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Bibliographic Details
Main Authors MICHAEL AUBURGER, CHRISTIAN KÖFINGER, JOACHIM METZGER
Format Patent
LanguagePortuguese
Published 07.04.2015
Subjects
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The frame element (10) has a pair of longitudinal hollow struts (12,14) that are connected together using connection struts (16,18). Each longitudinal strut has air inlet connection (12a,14a) connected to the air outlet duct of the aircraft air-conditioning unit and air outlet connection (12b,14b) connected to the air outlet opening termination in the cabin region of the aircraft. An independent claim is included for method for installing frame element in aircraft.
Bibliography:Application Number: BR2007PI15708