AR126281A1 - LIGHT TACTICAL AIRCRAFT - Google Patents

LIGHT TACTICAL AIRCRAFT

Info

Publication number
AR126281A1
AR126281A1 ARP220101712A ARP220101712A AR126281A1 AR 126281 A1 AR126281 A1 AR 126281A1 AR P220101712 A ARP220101712 A AR P220101712A AR P220101712 A ARP220101712 A AR P220101712A AR 126281 A1 AR126281 A1 AR 126281A1
Authority
AR
Argentina
Prior art keywords
fuselage
empennage
aircraft
elevons
light tactical
Prior art date
Application number
ARP220101712A
Other languages
Spanish (es)
Inventor
Mikhail Yurievich Strelets
Aleksey Sergeevich Bulatov
Artem Alekseevich Nizhenko
Natalia Borisovna Polyakova
Aleksey Kirillovich Shokurov
Mikhail Sergeevich Minkov
Aleksey Zakharovich Tarasov
Original Assignee
Public Joint Stock Company “United Aircraft Corporation”
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Public Joint Stock Company “United Aircraft Corporation” filed Critical Public Joint Stock Company “United Aircraft Corporation”
Publication of AR126281A1 publication Critical patent/AR126281A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

La invención se refiere a la aviación, en particular a una aeronave táctica ligera de firma de radar baja. El resultado técnico es un aumento de la estabilidad y capacidad de control de la aeronave sin deterioro de la firma de radar. La aeronave táctica ligera consta de un fuselaje con largueros de cola laterales avanzados, paneles exteriores de ala, un empenaje, una toma de aire, un sistema motopropulsor y una tobera de propulsión. Los largueros laterales de cola son avanzados y tienen partes finales pivotantes en un eje horizontal. Los paneles exteriores de las alas tienen un diseño muy inclinado y comprenden bordes de ataque articulados, elevones interiores y elevones exteriores. El empenaje está diseñado en forma de V y consta de aletas de movimiento completo que actúan como empenaje tanto horizontal como vertical. La toma de aire está dispuesta en una parte inferior del fuselaje y encierra parcialmente el fuselaje en la parte inferior.The invention relates to aviation, in particular to a low radar signature light tactical aircraft. The technical result is an increase in the stability and controllability of the aircraft without deterioration of the radar signature. The light tactical aircraft consists of a fuselage with advanced lateral tail spars, outer wing panels, an empennage, an air intake, a powertrain and a propulsion nozzle. The tail side spars are advanced and have end parts pivoting on a horizontal axis. The outer wing panels are of a highly raked design and comprise articulated leading edges, inner elevons and outer elevons. The empennage is designed in a V shape and consists of full-motion fins that act as both a horizontal and vertical empennage. The air intake is arranged in a lower part of the fuselage and partially encloses the fuselage in the lower part.

ARP220101712A 2021-07-19 2022-06-30 LIGHT TACTICAL AIRCRAFT AR126281A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2021121249A RU2768101C1 (en) 2021-07-19 2021-07-19 Light tactical plane

Publications (1)

Publication Number Publication Date
AR126281A1 true AR126281A1 (en) 2023-10-04

Family

ID=80820056

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP220101712A AR126281A1 (en) 2021-07-19 2022-06-30 LIGHT TACTICAL AIRCRAFT

Country Status (5)

Country Link
CN (1) CN118043257A (en)
AR (1) AR126281A1 (en)
RS (1) RS20240032A1 (en)
RU (1) RU2768101C1 (en)
WO (1) WO2023003490A1 (en)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2138423C1 (en) * 1998-04-06 1999-09-27 АООТ "ОКБ Сухого" Multimode aircraft of integral aerodynamic configuration
RU2166462C1 (en) * 2000-01-17 2001-05-10 Мухамедов Фатидин Абдурахманович Multi-purpose fighter
RU2605587C1 (en) * 2015-10-30 2016-12-20 Дмитрий Сергеевич Дуров Supersonic convertible aircraft
US10773791B2 (en) * 2018-07-24 2020-09-15 Shih-Ping Lee Aircraft with stealth double wings
CN111516871A (en) * 2020-04-30 2020-08-11 浙江大学 Supersonic stealth unmanned aerial vehicle with pneumatic stealth integrated design

Also Published As

Publication number Publication date
RU2768101C1 (en) 2022-03-23
WO2023003490A1 (en) 2023-01-26
CN118043257A (en) 2024-05-14
RS20240032A1 (en) 2024-03-29

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