RU2013103508A - Aircraft wing end - Google Patents
Aircraft wing end Download PDFInfo
- Publication number
- RU2013103508A RU2013103508A RU2013103508/11A RU2013103508A RU2013103508A RU 2013103508 A RU2013103508 A RU 2013103508A RU 2013103508/11 A RU2013103508/11 A RU 2013103508/11A RU 2013103508 A RU2013103508 A RU 2013103508A RU 2013103508 A RU2013103508 A RU 2013103508A
- Authority
- RU
- Russia
- Prior art keywords
- trailing edge
- end washer
- edge
- washer
- additional aerodynamic
- Prior art date
Links
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Landscapes
- Tires In General (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Законцовка крыла летательного аппарата, имеющая концевую шайбу, снабженную дополнительной аэродинамической стреловидной поверхностью малого удлинения с острой передней кромкой, смонтированной с внешней стороны концевой шайбы на ее конце, при этом задняя кромка дополнительной аэродинамической поверхности совмещена с задней кромкой концевой шайбы, носок расположен на передней кромке концевой шайбы ниже уровня задней кромки, а стреловидность составляет 60-85°, отличающаяся тем, что дополнительная аэродинамическая стреловидная поверхностью малого удлинения с острой передней кромкой, смонтирована не только с внешней, но и внутренней стороны концевой шайбы на конце законцовки крыла, при этом ее задняя кромка совмещена с задней кромкой концевой шайбы, а образованная стреловидность составляет 76-87°.The wing tip of an aircraft with an end washer equipped with an additional aerodynamic swept surface of small elongation with a sharp leading edge mounted on the outside of the end washer at its end, while the trailing edge of the additional aerodynamic surface is aligned with the trailing edge of the end washer, the nose is located on the leading edge the end washer is below the level of the trailing edge, and the sweep is 60-85 °, characterized in that the additional aerodynamic swept surface of small elongation with a sharp leading edge is mounted not only on the outer, but also on the inner side of the end washer at the end of the wingtip, while it the trailing edge is aligned with the trailing edge of the end washer, and the sweep formed is 76-87 °.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2013103508/11A RU2525335C1 (en) | 2013-01-25 | 2013-01-25 | Aircraft wing tip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2013103508/11A RU2525335C1 (en) | 2013-01-25 | 2013-01-25 | Aircraft wing tip |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2013103508A true RU2013103508A (en) | 2014-07-27 |
| RU2525335C1 RU2525335C1 (en) | 2014-08-10 |
Family
ID=51264754
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2013103508/11A RU2525335C1 (en) | 2013-01-25 | 2013-01-25 | Aircraft wing tip |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2525335C1 (en) |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2783885B1 (en) * | 1998-09-25 | 2001-07-27 | Geco As | SUPPORTING STRUCTURE WITH REDUCED MARGINAL TOURBILLON |
| RU2264328C1 (en) * | 2004-04-27 | 2005-11-20 | Открытое акционерное общество "Туполев" (ОАО "Туполев") | Flying vehicle wing tip |
| FR2954275B1 (en) * | 2009-12-22 | 2012-01-13 | Astrium Sas | ULTRA-RAPID AIR VEHICLE AND ASSOCIATED AIR LOCOMOTION METHOD |
-
2013
- 2013-01-25 RU RU2013103508/11A patent/RU2525335C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2525335C1 (en) | 2014-08-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20150126 |