Carburetor for model jet power plant

Claim 2

A carburetor for a model jet engine aircraft power plant, the power plant having a generally cylindrical duct, a single cylinder model aircraft engine having said cylinder oriented vertically immediately aft of said duct and a fan enclosed in said duct and driven by said engine, said engine having its fuel mixture inlet port forward of said cylinder, comprising: an essentially cylindrical body having a lower end forming a throat section for insertion into said engine fuel mixture inlet port, and an upper section relieved to form a web having a leading edge thereof tapering to a sharp edge for directing airflow from said fan around said body toward said engine cylinder, said body having a lower portion with a carburetor air opening in the forward portion thereof for receiving pressurized air from said fan; and a fuel feed control disposed at the top of said body and external to said duct, said control including a needle valve for adjusting maximum fuel input, a throttle for varying the volume of fuel-air mixture to said engine, and a fuel-air ratio mixture control wherein all adjustments of said control are external to the airstream from said fan.

Claim 3

The carburetor as defined in claim 1 in which said cylindrical body has a lower portion thereof having a cylindrical concentric inlet chamber therein, said chamber having said forwardly oriented carburetor air opening therein, said lower portion having said throat section communicating with said chamber by being inserted into said fuel mixture port of said engine.

Claim 4

The carburetor as defined in claim 2 in which said throttle includes: a throttle tube extending from the top of said body into said chamber, said throttle tube concentric to said body and having a closed lower end and a first fuel outlet slot adjacent said lower end, said throttle tube having an inverted air control cup concentric with said chamber and said throttle tube, said cup having a cup opening therethrough matching said chamber opening, said throttle tube externally rotatable with respect to said body to cause said cup opening to move relative to said chamber opening to thereby vary the amount of incoming air into said chamber; and a throttle arm connected to the upper end of said throttle tube to rotate said throttle tube changing said incoming airflow through said chamber opening and said cup opening.

Claim 5

The carburetor as defined in claim 3 in which said fuel-air ratio mixture control includes a fuel supply tube disposed concentrically within said throttle tube to fit snugly therein, said fuel supply tube having a closed lower end and a second fuel outlet slot adjacent said lower end and aligned with said first fuel outlet slot in said throttle tube wherein rotation of said throttle tube changes the fuel flow through said second fuel outlet slot and said first fuel outlet slot, said fuel supply tube communicating with an external fuel inlet, said fuel supply tube rotatable within said throttle tube for adjusting the fuel-air ratio.

Claim 6

The carburetor as defined in claim 4 in which said second fuel outlet slot has a non-linear opening to thereby provide a more linear throttle adjustment.

Claim 7

The carburetor as defined in claim 4 in which said needle valve is disposed between said fuel inlet and said fuel supply tube, said needle valve means externally adjustable to control the maximum fuel flow into said fuel supply tube.

Claim 8

In a model aircraft engine having a single vertically oriented cylinder, and a fuel mixture port forward of said cylinder, a carburetor connected to said port and extending upwardly therefrom comprising: an essentially cylindrical body having an upper portion thereof relieved to form a web having a leading edge thereof tapering to a sharp edge, and a lower portion of said body having a cylindrical concentric inlet chamber therein, said chamber having a forwardly oriented opening, said lower portion having a rearwardly angling throat section communicating with said chamber and adapted to be inserted into said fuel mixture port of said engine; a throttle tube extending from the top of said body into said chamber, said throttle tube concentric to said body and having a closed lower end and a first fuel outlet slot adjacent said lower end, said throttle tube having an inverted air control cup concentric with said chamber and said throttle tube, said cup having a cup opening therethrough matching said chamber opening, said throttle tube externally rotatable with respect to said body to cause said cup opening to move relative to said chamber opening to thereby vary the amount of incoming air into said chamber; a fuel supply tube disposed concentrically within said throttle tube to fit snugly therein, said fuel supply tube having a closed lower end and a second fuel outlet slot adjacent said lower end and aligned with said first fuel outlet slot in said throttle tube, said fuel supply tube integral with an external fuel feed control portion having a fuel inlet, said external fuel feed control portion rotatable to adjust the fuel-air ratio; needle valve means disposed in said fuel feed control portion between said fuel inlet and said fuel supply tube, said needle valve means externally adjustable to control fuel flow into said fuel supply tube; and a throttle arm connected to the upper end of said throttle tube to rotate said throttle tube thereby changing fuel flow through said second fuel outlet slot and said first fuel outlet slot and changing said incoming airflow through said chamber opening and said cup opening.

Claim 9

In a model aircraft engine having a single vertically oriented cylinder, and a fuel mixture port forward of said cylinder, a carburetor connected to said port and extending upwardly therefrom comprising: an essentially cylindrical body having an upper portion thereof relieved to form a web having a leading edge thereof tapering to a sharp edge, and a lower portion of said body having a cylindrical concentric inlet chamber therein, said chamber having a forwardly oriented opening, said lower portion having a rearwardly angling throat section communicating with said chamber and adapted to be inserted into said fuel mixture port of said engine; a throttle tube extending from the top of said body into said chamber, said throttle tube concentric to said body and having a closed lower end and a first fuel outlet slot adjacent said lower end, said throttle tube having an inverted air control cup concentric with said chamber and said throttle tube, said cup having a cup opening therethrough matching said chamber opening, said throttle tube externally rotatable with respect to said body to cause said cup opening to move relative to said chamber opening to thereby vary the amount of incoming air into said chamber; a fuel supply tube disposed concentrically within said throttle tube to fit snugly therein, said fuel supply tube having a closed lower end and a second fuel outlet slot adjacent said lower end and aligned with said first fuel outlet slot in said throttle tube, said fuel supply tube integral with an external fuel feed control portion having a fuel inlet, said external fuel feed control portion rotatable to adjust the fuel-air ratio; needle valve means disposed in said fuel feed control portion between said fuel inlet and said fuel supply tube, said needle valve means externally adjustable to control fuel flow into said fuel supply tube; and a throttle arm connected to the upper end of said throttle tube to rotate said throttle tube thereby changing fuel flow through said second fuel outlet slot and said first fuel outlet slot and changing said incoming airflow through said chamber opening and said cup opening.

Claim 10

The carburetor as defined in claim 7 in which said fuel feed control portion of said fuel supply tube is externally adjustable to thereby vary the fuel-air ratio from said carburetor.

Claim 11

The carburetor as defined in claim 7 in which said second fuel outlet slot has a non-linear opening to thereby provide a more linear throttle adjustment.