AR126282A1 - SINGLE ENGINE MULTIFUNCTIONAL SUPERSONIC AIRCRAFT - Google Patents
SINGLE ENGINE MULTIFUNCTIONAL SUPERSONIC AIRCRAFTInfo
- 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
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)
- 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.
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)
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 |
-
2021
- 2021-07-19 RU RU2021121246A patent/RU2770885C1/en active
-
2022
- 2022-06-29 CN CN202280050997.4A patent/CN117769517A/en active Pending
- 2022-06-29 RS RS20240033A patent/RS20240033A1/en unknown
- 2022-06-29 WO PCT/RU2022/000206 patent/WO2023003491A1/en active Application Filing
- 2022-06-29 CU CU2024000004A patent/CU20240004A7/en unknown
- 2022-06-30 AR ARP220101713A patent/AR126282A1/en unknown
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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