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1.发明公开TRIEBWERKS-EINLAUFKLAPPE ZUR ANBRINGUNG AN DEM GEHÄUSE EINES LUFTEINLASSES EINES FLUGZEUG-TRIEBWERKS SOWIE TRIEBWERK MIT EINER SOLCHEN TRIEBWERKS-EINLAUFKLAPPE UND FLUGZEUGSYSTEM 有权发动机进气口FLAP用于连接到飞机发动机和发动机这样的发动机吸气瓣和飞机系统的外壳进气口
公开(公告)号：EP2254795A1
公开(公告)日：2010-12-01
申请号：EP09708711.8
申请日：2009-02-04
发明人： BOLENDER, Lars , WAGNON, Sébastian
CPC分类号： B64D15/16 , B64D33/02 , B64D2033/0213 , B64D2033/0233 , F02C7/047 , F02C7/055 , Y02T50/672
摘要： Engine inlet flap (K) for mounting on the housing of an air inlet or air inlet duct of an engine of an aircraft, having a first end (E1) and a second end (E2) arranged in opposition thereto at a distance therefrom in the longitudinal direction (L) of the inlet flap, wherein the longitudinal direction (L) in the given installation is aligned against the flow direction (S) of the air flowing into the engine. The inlet flap (K) comprises an inlet flap base body (1) with a connector device for a jointed connector for jointed connection of the inlet flap base body (1) to the housing of the air inlet or air inlet duct, with a rotational axis (A) running along the second end (E2), an inlet flap extension piece (2) structurally integrated with the inlet flap base body (1), with a first and a second lateral piece (5, 6), which extends from the inlet flap base body (1) on the two opposed lateral edges (5, 6) of the inlet flap (K) running in the longitudinal direction (L) with a number of transverse struts (11) or longitudinal struts, arranged in the leading region of the engine inlet flap (K).
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2.发明授权TRIEBWERKS-EINLAUFKLAPPE ZUR ANBRINGUNG AN DEM GEHÄUSE EINES LUFTEINLASSES EINES FLUGZEUG-TRIEBWERKS SOWIE TRIEBWERK MIT EINER SOLCHEN TRIEBWERKS-EINLAUFKLAPPE UND FLUGZEUGSYSTEM 有权发动机进气口FLAP用于连接到飞机发动机和发动机这样的发动机吸气瓣和飞机系统的外壳进气口
公开(公告)号：EP2254795B1
公开(公告)日：2011-10-26
申请号：EP09708711.8
申请日：2009-02-04
发明人： BOLENDER, Lars , WAGNON, Sébastien
CPC分类号： B64D15/16 , B64D33/02 , B64D2033/0213 , B64D2033/0233 , F02C7/047 , F02C7/055 , Y02T50/672
摘要： Engine inlet flap (K) for mounting on the housing of an air inlet or air inlet duct of an engine of an aircraft, having a first end (E1) and a second end (E2) arranged in opposition thereto at a distance therefrom in the longitudinal direction (L) of the inlet flap, wherein the longitudinal direction (L) in the given installation is aligned against the flow direction (S) of the air flowing into the engine. The inlet flap (K) comprises an inlet flap base body (1) with a connector device for a jointed connector for jointed connection of the inlet flap base body (1) to the housing of the air inlet or air inlet duct, with a rotational axis (A) running along the second end (E2), an inlet flap extension piece (2) structurally integrated with the inlet flap base body (1), with a first and a second lateral piece (5, 6), which extends from the inlet flap base body (1) on the two opposed lateral edges (5, 6) of the inlet flap (K) running in the longitudinal direction (L) with a number of transverse struts (11) or longitudinal struts, arranged in the leading region of the engine inlet flap (K).
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