AIRCRAFT WITH INTEGRAL AERODYNAMIC CONFIGURATION Russian patent published in 2021 - IPC B64C1/36 H01Q1/28 H01Q3/00 

FIELD: aircrafts.

SUBSTANCE: invention relates to a design of multi-modal subsonic and supersonic aircrafts with a low visibility level in the radar range. The aircraft with integral aerodynamic configuration is comprised of a fuselage with strakes, a wing wherein the consoles are smoothly coupled with the fuselage, horizontal and vertical tail, a twin-engine power unit including engines with air intakes, wherein the controlled rotary parts of the fuselage strakes (RPFS) are located above the entrances of the intakes. Each RPFS is made as a removable antenna system including a power frame with paneling and comprised of an antenna section and an instrument section. Antenna arrays are located in the antenna section of the system, and active super high frequency apparatuses, a summation circuit, an antenna system control circuit, air and liquid cooling systems connected with the onboard air and liquid cooling systems are located in the instrument section.

EFFECT: invention is designed to reduce the radar signature characteristics, increase climatic influence resistance of the antenna equipment and improve viewing conditions.

6 cl, 3 dwg