US 6,883,503 B2Granted

Engine driven supercharger for aircraft

OwnerErnest A. Carrollinventor

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Abstract

A supercharging system for supplying pressurized combustion air to a piston engine of an aircraft at high altitudes. The engine has an output shaft on which the propeller is supported, together with a small ducted centrifugal fan. The duct leads to the intake side of the engine. A diverter is movable to one position constraining pressurized air to enter the engine through the intake side, and a second position which diverts compressed air away from the intake side. Natural aspiration is employed at low altitudes and supercharging is employed at altitudes wherein there is an oxygen deficiency. Preferably, the centrifugal fan is located between the propeller and the engine block, has blades staggered from those of the propeller so as to be directly exposed to incoming air. The centrifugal fan blades are preferably of different pitch than the propeller blades.

Claims13

Dependent claims

A supercharged reciprocating engine assembly for a miniature, unmanned aircraft, comprising:

an engine sized and configured for powering said miniature, unmanned aircraft and having an engine block defining at least one cylinder, and a piston reciprocatingly and slidably disposed within each cylinder;
a single air intake passage for conducting combustion air into said at least one cylinder;
a rotatable output shaft rotatingly driven by said engine and projecting forward therefrom;
a propeller disposed proximate a forward end of said rotatable output shaft;
a single duct disposed to house an axial flow air pressurization device mounted on said output shaft therein, said single duct having an intake end disposed proximate said propeller, and a discharge end operatively connected to said single air intake passage, said single duct configured to route air pressurized by said axial flow air pressurization device within said single duct to said single air intake passage of said engine;
and
a diverter disposed in said single duct to selectively route pressurized air into said single air intake passage of said engine and to discharge pressurized air away from said single air intake passage of said engine;
both said single duct and said single air intake passage being disposed between said propeller and a forward side of said engine.

5 more elements

A supercharged reciprocating engine assembly for a miniature, unmanned aircraft, comprising:

a) an engine comprising an engine block defining at least one cylinder, a piston reciprocatingly and slidably disposed within said at least one cylinder, a single air intake passage for receiving combustion air and conducting said combustion air to said at least one cylinder;
and a rotatable output shaft projecting forward from a front surface of said engine block;
b) a propeller having blades arranged in a first, predetermined radial arrangement and affixed to said rotatable output shaft proximate a distal end thereof;
c) a single duct having an intake end disposed adjacent to and rearward of said propeller, and a discharge end operably connected to said single air intake passage of said engine to route air from said intake end to said single air intake passage;
d) an axial flow air pressurization device disposed on said output shaft rearward of said propeller and within said single duct, for pressurizing air therein;
e) a diverter disposed within said single duct between said air pressurization device and said single air intake passage to selectively route pressurized air into said single intake passage of said engine and to discharge pressurized air away from said single air intake passage of said engine.

3 more elements

Dependencies are inferred from the claim text.