发明名称 RAHMENELEMENT, KLIMAANLAGE FÜR LUFTFAHRZEUG UND VERFAHREN ZUR INSTALLATION EINES RAHMENELEMENTS IN EIN FLUGZEUG
摘要 <p>#CMT# #/CMT# 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. #CMT# : #/CMT# An independent claim is included for method for installing frame element in aircraft. #CMT#USE : #/CMT# Frame element for use in aircraft air-conditioning system (claimed). #CMT#ADVANTAGE : #/CMT# The use of the frame element simplifies the installation of the riser ducts in the aircraft, without reshaping the aircraft interior components. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a perspective view of the frame element. 10 : Frame element 12,14 : Longitudinal Struts 12a,14a : Air-inlet connections of struts 12b,14b : Air-outlet connections of struts 16,18 : Connection struts.</p>
申请公布号 AT476357(T) 申请公布日期 2010.08.15
申请号 AT20070801736T 申请日期 2007.08.17
申请人 AIRBUS DEUTSCHLAND GMBH 发明人 KOEFINGER, CHRISTIAN;METZGER, JOACHIM;AUBURGER, MICHAEL
分类号 B64C1/00;B64C1/06;B64C1/12;B64D13/00 主分类号 B64C1/00
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