Equipment for the reduction of the radar marking for aircrafts
First Claim
1. Equipment for reduction of radar marking of an aircraft, which can be applied to at least one hot portion of the aircraft chosen from the following:
- a piloting cabin or cockpit, comprising at least one transparent portion;
a first frame of the fuselage;
a plurality of junction edges of components, including wings, tail veilings and engine air intakes;
at least one motor face;
said equipment comprising;
at least one removable device for dissipating incident radar waves, which is applied to at least one hot portion of the aircraft without affecting aerodynamic characteristics of the aircraft;
at least one grid to reduce the radar marking from hot portions of the aircraft including at least one motor face;
the grid comprising;
an inner structure with a plurality of openings;
a support structure for securing the grid to the aircraft;
wherein said openings are sized to act like a flat surface for lower frequencies of a frequency spectrum commonly used by low-frequency radar recognition systems;
each of said openings comprising an inner surface coated with a thin radar absorbing material adapted to absorb electromagnetic waves at high frequency;
said grid being adapted to allow air flow to the engine and to reduce visibility of the motor face of the aircraft to radar systems.
1 Assignment
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Accused Products
Abstract
Equipment for the reduction of the radar marking of an aircraft V, can be applied to at least one hot portion H of the aircraft, chosen from the following: a piloting cabin or cockpit, including at least one transparent portion; a first frame of the fuselage; a plurality of junction edges of components, including wings, tail veilings and engine air intakes; at least one motor face. Said equipment comprises at least one device for dissipating incident radar waves, which can be removably applied to at least one hot portion H of the aircraft without affecting the aerodynamic characteristics of the aircraft V.
28 Citations
9 Claims
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1. Equipment for reduction of radar marking of an aircraft, which can be applied to at least one hot portion of the aircraft chosen from the following:
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a piloting cabin or cockpit, comprising at least one transparent portion; a first frame of the fuselage; a plurality of junction edges of components, including wings, tail veilings and engine air intakes; at least one motor face; said equipment comprising; at least one removable device for dissipating incident radar waves, which is applied to at least one hot portion of the aircraft without affecting aerodynamic characteristics of the aircraft; at least one grid to reduce the radar marking from hot portions of the aircraft including at least one motor face;
the grid comprising;an inner structure with a plurality of openings; a support structure for securing the grid to the aircraft; wherein said openings are sized to act like a flat surface for lower frequencies of a frequency spectrum commonly used by low-frequency radar recognition systems; each of said openings comprising an inner surface coated with a thin radar absorbing material adapted to absorb electromagnetic waves at high frequency; said grid being adapted to allow air flow to the engine and to reduce visibility of the motor face of the aircraft to radar systems. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9)
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Specification