FIELD: aircraft equipment.
SUBSTANCE: invention is related to design of detachable outboard aircraft containers for internal deployment of aircraft weapons. The removable suspension container contains a body with a load-bearing frame, nose and tail aerodynamic fairings, a pylon for suspending container on the aircraft suspension point. Inside the container body, in its upper part, there are communication means for controlling the use of the payload and power units of the frame for securing the payload, including flanged attachment units for aircraft weapons installations, containing studs for attaching air-to-surface missiles, and attachment units of the "lug-fork" type for air-to-air missiles. At the same time, the lower part of the container body is provided with a hatch and powered shutters closing it. The container suspension pylon contains connectors for connecting the container to the aircraft onboard systems. At the same time, all elements of the container design are made with a heat-resistant coating. The outer surface of the container contains a radio-absorbing coating.
EFFECT: expanding the functionality of the aircraft in solving combat missions, increasing the combat effectiveness of the aircraft, reducing radar visibility, as well as increasing the safety of using certain types of aviation weapons.
1 cl, 4 dwg
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Authors
Dates
2023-06-06—Published
2022-12-28—Filed