AR126282A1 - SINGLE ENGINE MULTIFUNCTIONAL SUPERSONIC AIRCRAFT - Google Patents

SINGLE ENGINE MULTIFUNCTIONAL SUPERSONIC AIRCRAFT

Info

Publication number
AR126282A1
AR126282A1 ARP220101713A ARP220101713A AR126282A1 AR 126282 A1 AR126282 A1 AR 126282A1 AR P220101713 A ARP220101713 A AR P220101713A AR P220101713 A ARP220101713 A AR P220101713A AR 126282 A1 AR126282 A1 AR 126282A1
Authority
AR
Argentina
Prior art keywords
aircraft
engine
reduced
fuselage
centerline
Prior art date
Application number
ARP220101713A
Other languages
Spanish (es)
Inventor
Mikhail Yurievich Strelets
Aleksey Sergeevich Bulatov
Mikhail Viktorovich Nikitushkin
Vladimir Dmitrievich Stepanov
Dmitry Germanovich Kononov
Leonid Evgenievich Krylov
Aleksandr Vladimirovish Barabanov
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 AR126282A1 publication Critical patent/AR126282A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C30/00Supersonic type aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tires In General (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Toys (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

La invención se refiere al campo de la aviación. Una aeronave supersónica multifuncional de un solo motor comprende un fuselaje, un ala ahusada, paneles de empenaje vertical en forma de V totalmente móvil, largueros laterales avanzados, toma de aire del motor lateral inferior ubicada debajo de la sección delantera del fuselaje con un conducto que se extiende a lo largo de la línea central de la aeronave, compartimentos de carga centrales y laterales, un sistema motopropulsor de un solo motor que comprende un motor con una tobera de propulsión giratoria dispuesta a lo largo de la línea central de la aeronave. El diseño de la aeronave proporciona dimensiones reducidas de la aeronave y menor peso, resistencia aerodinámica reducida, reducida RCS y firma de radar, alto rendimiento de la aeronave y características de maniobrabilidad, características sobresalientes de estabilidad y control, volumen ampliado de compartimentos de carga, capacidad de cargas de gran tamaño multipropósito, así como capacidad multifuncional de las aeronaves.The invention relates to the field of aviation. A single-engine multifunctional supersonic aircraft comprises a fuselage, a tapered wing, fully movable V-shaped vertical empennage panels, forward side spars, lower lateral engine air intake located below the forward section of the fuselage with a duct that extends along the centerline of the aircraft, center and side cargo compartments, a single-engine propulsion system comprising an engine with a rotating propulsion nozzle arranged along the centerline of the aircraft. The aircraft design provides reduced aircraft dimensions and lower weight, reduced aerodynamic drag, reduced RCS and radar signature, high aircraft performance and maneuverability characteristics, outstanding stability and control characteristics, expanded volume of cargo compartments, multipurpose large cargo capacity, as well as multifunctional capacity of aircraft.

ARP220101713A 2021-07-19 2022-06-30 SINGLE ENGINE MULTIFUNCTIONAL SUPERSONIC AIRCRAFT AR126282A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2021121246A RU2770885C1 (en) 2021-07-19 2021-07-19 Multifunctional supersonic single-engine aircraft

Publications (1)

Publication Number Publication Date
AR126282A1 true AR126282A1 (en) 2023-10-04

Family

ID=81306384

Family Applications (1)

Application Number Title Priority Date Filing Date
ARP220101713A AR126282A1 (en) 2021-07-19 2022-06-30 SINGLE ENGINE MULTIFUNCTIONAL SUPERSONIC AIRCRAFT

Country Status (6)

Country Link
CN (1) CN117769517A (en)
AR (1) AR126282A1 (en)
CU (1) CU20240004A7 (en)
RS (1) RS20240033A1 (en)
RU (1) RU2770885C1 (en)
WO (1) WO2023003491A1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998030444A1 (en) * 1997-01-08 1998-07-16 Yalestown Corporation N.V. Supersonic aircraft
US7762077B2 (en) * 2006-12-05 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Single-stage hypersonic vehicle featuring advanced swirl combustion
CN106494626A (en) * 2016-11-04 2017-03-15 葛明龙 Four kinds of high-speed aircrafts with new work engine
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
CN117769517A (en) 2024-03-26
CU20240004A7 (en) 2024-09-06
RS20240033A1 (en) 2024-03-29
RU2770885C1 (en) 2022-04-25
WO2023003491A1 (en) 2023-01-26

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