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Aircraft including a powerplant mounted on an airframe and a rotor/wing rotatably mounted on the airframe. The rotor/wing has multiple blades extending outward from roots adjacent the airframe to tips opposite the roots and having internal conduits extending between inlets adjacent the roots and dow

Aircraft including a powerplant mounted on an airframe and a rotor/wing rotatably mounted on the airframe. The rotor/wing has multiple blades extending outward from roots adjacent the airframe to tips opposite the roots and having internal conduits extending between inlets adjacent the roots and downstream outlets. The aircraft also includes multiple intermediate ducts having upstream ends including flanges and downstream ends slidably and pivotally connected to corresponding blade inlets. Moreover, the aircraft includes a manifold having an upstream end in fluid communication with the powerplant and multiple downstream ends including flanges connected to upstream ends of corresponding intermediate ducts. The aircraft further includes multiple covers connected to corresponding manifold flanges and covering corresponding intermediate duct flanges. The aircraft also includes multiple absorbers positioned between corresponding intermediate duct flanges and manifold flanges and between the intermediate duct flanges and corresponding cover to control movement of the intermediate duct flanges.

대표청구항 ▼

1. An assembly comprising: a first duct terminating in a first annular flange;a second duct terminating in a second annular flange; andan articulable sealed joint including: a cover covering said second flange of the second duct, the cover terminating in a third flange that extends outwards and oppo

1. An assembly comprising: a first duct terminating in a first annular flange;a second duct terminating in a second annular flange; andan articulable sealed joint including: a cover covering said second flange of the second duct, the cover terminating in a third flange that extends outwards and opposes the first flange of the first duct;a first absorber positioned between said second flange and said cover;a second absorber positioned on an opposite side of the second flange; anda gasket between the first flange and the second absorber;the first and second absorbers allowing limited movement of said second flange with respect to the first flange and the cover. 2. An assembly as set forth in claim 1 wherein the second absorber includes a wave spring positioned between said gasket and said second flange and wherein the first absorber includes a wave spring positioned between said second flange and said cover. 3. An assembly as set forth in claim 1 wherein the gasket has a lateral surface and the second duct has an inner surface opposite said lateral surface and the gasket includes a protrusion extending from its lateral surface, the protrusion between the first and third flange. 4. The assembly of claim 1, wherein each absorber is made of an elastomeric material. 5. The assembly of claim 1, wherein a downstream end of the second duct includes a toroidal or spherical portion. 6. The assembly of claim 1, further comprising a clamp for connecting the cover to the first flange. 7. An assembly including an articulable sealed joint connecting a first duct having a first flange extending outward adjacent an edge thereof and a second duct having a second flange extending outward therefrom, the assembly comprising a cover connected to said first flange of the first duct and covering said second flange of the second duct;an absorber positioned between said first flange and said second flange and between said second flange and said cover allowing limited movement of said second flange with respect to the first flange and the cover; anda gasket positioned between said first flange and said absorber and between said first flange and said second flange;wherein said second flange is spaced from said edge of the second duct, the second duct includes a longitudinal rib positioned between said second flange and said edge, and the gasket includes a slot in which the longitudinal rib is positioned to pilot the second duct in the sealed joint. 8. An assembly as set forth in claim 7 wherein the second duct is pivotable between a default position and a plurality of pivoted positions and said longitudinal rib is spaced from a bottom of said slot when the second duct is in its default position. 9. An assembly comprising: a manifold having an upstream end and a plurality of downstream ends, each downstream end having a first annular flange;a plurality of ducts, each duct having upstream end with a second annular flange;and a plurality of articulable joints, each jointing connecting an upstream end of a corresponding duct to a corresponding downstream end of the manifold, each joint having a first side that contracts and an opposing second side that expands to allow the corresponding duct to assume a fully pivoted position; each articulable joint including: a cover terminating in a third annular flange that extends outwards and opposes the first flange of the corresponding manifold downstream end, the cover covering the second flange of the corresponding duct;a first absorber positioned between the second flange and the cover; anda second absorber positioned between the corresponding first and second flanges to cushion movement between the corresponding duct upstream end and manifold downstream end. 10. The assembly of claim 9 wherein each articulable joint further includes a gasket having a first portion between the corresponding first flange and the second absorber, and a second portion between the first and third flanges. 11. The assembly of claim 9, wherein each first absorber includes an inboard wave spring positioned between the corresponding first and second flanges; and each second absorber includes an outboard wave spring positioned between the cover and the corresponding second flange.