| CPC B64C 1/0009 (2013.01) [B62D 35/00 (2013.01); B63H 11/08 (2013.01); B64C 1/16 (2013.01); B64C 15/02 (2013.01); B63H 2011/081 (2013.01); B64C 2001/0045 (2013.01)] | 20 Claims |
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1. Motorized mobile units, other than an airship, comprising of inseparable sub-assemblies:
an outer fuselage envelope with a length greater than a net transverse dimension of the outer fuselage envelope;
at least one motorized internal longitudinal channel and a plurality of motorized internal longitudinal fluidic channels longitudinally crossing the mobile units and incorporated into a volume of the outer fuselage envelope, so as to ensure an internal circulation of a fluid opposing a frontal movement of the mobile units, said at least one motorized internal longitudinal channel or each motorized internal longitudinal fluidic channel being equipped with one or more motorization devices, supplemented by an upstream equipment and a downstream equipment, controlled so that speeds and pressures of an overall flow of the fluid leaving said at least one motorized internal longitudinal channel are greater than speeds and pressures of an incoming flow, each of said plurality of motorized internal longitudinal channels presenting, successively, in a direction of the internal circulation of the fluid;
a set of input portions of convergent sections, a set of intermediate portions of constant section, and a set of final output portions of divergent sections, and an inlet portion of the converging sections in said at least one motorized internal longitudinal channel comprising:
fan-compressors in aeraulic applications or flow accelerators in hydraulic applications; and
differential pressure sensors, between the incoming flow and an external surrounding flow, mounted on a front leading edge separating between the external surrounding flow and a flow admitted into said each motorized internal longitudinal fluidic channel;
each intermediate portion comprising:
propellants from said one or more motorization devices acting directly on a fluid stream channeled by said each motorized internal longitudinal fluidic channel and positioned along an intermediate portion of said each motorized internal longitudinal fluidic channel; and
a longitudinal channeling secondary envelope, which conducts internally, around each motorized fluidic vein, a concentric, damping flow, extending at least over an entire length of said each intermediate portion of said each motorized internal longitudinal fluidic channel;
each final output portion located downstream of said each motorized internal longitudinal fluidic channel of the mobile units, extending from an exit of a corresponding intermediate portion to a rear end of the outer fuselage envelope, and
comprising:
energy sensor devices;
diffusers; and
parallelizers of a flow leaving the corresponding intermediate portion and of a flow channeled by a corresponding longitudinal channeling secondary envelope;
a plurality of non-motorized transverse internal fluidic channels connected at a request of a controller, upstream to said plurality of motorized internal longitudinal fluidic channels at a height of an output of the motorizations devices of said plurality of motorized internal longitudinal fluidic channels or after the energy sensor devices, opening downstream into specific surface areas of the outer fuselage envelope to ensure therein a controlled distribution of flows picked up from said plurality of motorized internal longitudinal fluidic channels and to develop therein controlled lateral thrust forces;
wherein said plurality of non-motorized transverse internal fluidic channels link in a completely internalized manner in the outer fuselage envelope, paths between upstream and downstream ends of said plurality of non-motorized transverse internal fluidic channels comprising variable sections linked to a flow rate of the flows that must be driven by said plurality of non-motorized transverse internal fluidic channels; and
a set of available internal volumes between the outer fuselage envelope and a totality of internal volumes occupied by said plurality of motorized internal longitudinal fluidic channels and said plurality of non-motorized transverse internal fluidic channels, and their associated functional equipment structured in sub-technical sets for operating said mobile units.
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