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US 11,691,715 B2Granted
Aircraft system for reduced observer visibility
AssigneeAeroVironment, Inc.
InventorsChristopher Eugene Fisher, Steven Bradley Chambers, Pavil Belik, Austin Craig Gunder, John Peter Zwaan
Life of this patent
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Abstract
An aircraft apparatus is disclosed that has a fuselage boom having proximal and distal ends, a wing coupled to a proximal end of the fuselage boom and at least one transparent stabilizer coupled to a distal end of the fuselage boom.
Claims15
An aircraft apparatus, comprising:
- a tubular fuselage boom having a proximal end and a distal end;
- a wing coupled to the fuselage boom at a proximal end of the fuselage boom, wherein the wing comprises a port outboard wing section and a starboard outboard wing section;
- a stabilizer coupled to the distal end of the fuselage boom;
- a servo having a servo arm;
- and
- a servo horn slidably coupled to the stabilizer to slidably receive and detachably couple the servo arm to the stabilizer;
- wherein each of the port outboard wing section and the starboard outboard wing section comprise curved leading edges of varying radii;
- and
- wherein each of the port outboard wing section and the starboard outboard wing section comprise curved trailing edges of varying radii.
6 more elements
Dependencies are inferred from the claim text.