Uniflange coupling assembly
Nacelle and mounting arrangement for an aircraft engine
Aircraft propulsive power unit
Aircraft propulsive power unit assembly having a leading edge lipskin and intake barrel Patent #: 5941061
ApplicationNo. 11036075 filed on 01/18/2005
US Classes:60/226.1, Air and diverse fluid discharge from separate discharge outlets (e.g., fan jet, etc.)60/799, Having expansible connection244/53B, Air intakes244/54, Mounting60/802Motor driven accessory
ExaminersPrimary: Koczo, Michael Jr.
Attorney, Agent or Firm
International ClassesB64D 29/06
AbstractA cowl structure (18) for a gas turbine engine (10) comprises an outer skin (26) defining a first path for a load applied to the engine (10). The cowl structure (18) includes an inner skin (24) defining a second path for the load. The inner and outer skins (24, 26) are constructed such that a major proportion of the load is transmitted along the first path.