FIELD: aviation.
SUBSTANCE: invention relates to the operational manufacturability of a multifunctional single-engine supersonic aircraft. The aircraft includes landing gear located in niches, hydro- and power supply systems, maintenance units located in the niches of supports, on-board equipment located in compartments inside the fuselage. Service assemblies for refuelling and oil charging, connecting a ground source of air conditioning and power supply, ground preparation of weapons, control of cargo compartment doors, grounding and ground intercom are located in the niches of the left and/or right main landing gear with the possibility of human access to them without using additional funds. The avionics units are located in compartments inside the fuselage behind the niche of the right and/or left landing gear supports in the direction of aircraft movement providing human access to them without the use of additional means and are closed by maintenance hatches using quarter-turn cover fasteners. Dismantling the power plant does not require the dismantling of other power elements of the aircraft.
EFFECT: reduced time, increased convenience and safety of operation and maintenance of a light tactical aircraft.
3 cl, 2 dwg
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Authors
Dates
2023-07-18—Published
2022-12-28—Filed