CU20240003A7 - LIGHT TACTICAL AIRCRAFT - Google Patents
LIGHT TACTICAL AIRCRAFTInfo
- Publication number
- CU20240003A7 CU20240003A7 CU2024000003A CU20240003A CU20240003A7 CU 20240003 A7 CU20240003 A7 CU 20240003A7 CU 2024000003 A CU2024000003 A CU 2024000003A CU 20240003 A CU20240003 A CU 20240003A CU 20240003 A7 CU20240003 A7 CU 20240003A7
- Authority
- CU
- Cuba
- Prior art keywords
- fuselage
- empennage
- aircraft
- elevons
- light tactical
- 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)
- Radar Systems Or Details Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
<p>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 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.</p><p>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 forward-facing side tail spars, outer wing panels, an empennage, an air intake, a propulsion system and a propulsion nozzle. The side tail spars are forward-facing and have end portions pivoting on a horizontal axis. The outer wing panels have 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-moving fins acting as both a horizontal and vertical empennage. The air intake is arranged in a lower part of the fuselage and partially encloses the fuselage at the bottom.</p>
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2021121249A RU2768101C1 (en) | 2021-07-19 | 2021-07-19 | Light tactical plane |
| PCT/RU2022/000205 WO2023003490A1 (en) | 2021-07-19 | 2022-06-29 | Tactical light aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CU20240003A7 true CU20240003A7 (en) | 2024-09-06 |
| CU24779B1 CU24779B1 (en) | 2026-02-09 |
Family
ID=80820056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CU2024000003A CU24779B1 (en) | 2021-07-19 | 2022-06-29 | LIGHT TACTICAL AIRCRAFT |
Country Status (7)
| Country | Link |
|---|---|
| CN (1) | CN118043257A (en) |
| AR (1) | AR126281A1 (en) |
| CU (1) | CU24779B1 (en) |
| PE (1) | PE20241023A1 (en) |
| RS (1) | RS20240032A1 (en) |
| RU (1) | RU2768101C1 (en) |
| WO (1) | WO2023003490A1 (en) |
Family Cites Families (5)
| 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 | A supersonic stealth UAV with integrated design of aerodynamic stealth |
-
2021
- 2021-07-19 RU RU2021121249A patent/RU2768101C1/en active
-
2022
- 2022-06-29 CU CU2024000003A patent/CU24779B1/en unknown
- 2022-06-29 RS RS20240032A patent/RS20240032A1/en unknown
- 2022-06-29 CN CN202280051011.5A patent/CN118043257A/en active Pending
- 2022-06-29 PE PE2024000109A patent/PE20241023A1/en unknown
- 2022-06-29 WO PCT/RU2022/000205 patent/WO2023003490A1/en not_active Ceased
- 2022-06-30 AR ARP220101712A patent/AR126281A1/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| RU2768101C1 (en) | 2022-03-23 |
| PE20241023A1 (en) | 2024-05-08 |
| RS20240032A1 (en) | 2024-03-29 |
| WO2023003490A1 (en) | 2023-01-26 |
| CN118043257A (en) | 2024-05-14 |
| CU24779B1 (en) | 2026-02-09 |
| AR126281A1 (en) | 2023-10-04 |
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