LV15738A - Aerodinamiski uzlabots zema ātruma bezpilota gaisa transportlīdzekļa (UAV) spārns - Google Patents
Aerodinamiski uzlabots zema ātruma bezpilota gaisa transportlīdzekļa (UAV) spārnsInfo
- Publication number
- LV15738A LV15738A LVP-21-88A LVP2021000088A LV15738A LV 15738 A LV15738 A LV 15738A LV P2021000088 A LVP2021000088 A LV P2021000088A LV 15738 A LV15738 A LV 15738A
- Authority
- LV
- Latvia
- Prior art keywords
- uav
- aerial vehicle
- unmanned aerial
- wing
- improved low
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
- B64C2003/142—Aerofoil profile with variable camber along the airfoil chord
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Tires In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Izgudrojums attiecas uz lidmašīnas sastāvdaļām, jo īpaši uz spārnu konstrukciju maza ātruma UAV (bezpilota lidaparāta) lietojumiem. Izgudrojuma mērķis ir veidot maza ātruma aerodinamiski uzlabotu spārnu galvenokārt UAV vai vieglo lidmašīnu lietojumam.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LVP-21-88A LV15738A (lv) | 2021-11-17 | 2021-11-17 | Aerodinamiski uzlabots zema ātruma bezpilota gaisa transportlīdzekļa (UAV) spārns |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
LVP-21-88A LV15738A (lv) | 2021-11-17 | 2021-11-17 | Aerodinamiski uzlabots zema ātruma bezpilota gaisa transportlīdzekļa (UAV) spārns |
Publications (1)
Publication Number | Publication Date |
---|---|
LV15738A true LV15738A (lv) | 2023-05-20 |
Family
ID=83193523
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
LVP-21-88A LV15738A (lv) | 2021-11-17 | 2021-11-17 | Aerodinamiski uzlabots zema ātruma bezpilota gaisa transportlīdzekļa (UAV) spārns |
Country Status (1)
Country | Link |
---|---|
LV (1) | LV15738A (lv) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20140098600A (ko) * | 2013-01-31 | 2014-08-08 | 한국항공우주연구원 | 항공기용 익형이 적용된 날개 |
-
2021
- 2021-11-17 LV LVP-21-88A patent/LV15738A/lv unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20140098600A (ko) * | 2013-01-31 | 2014-08-08 | 한국항공우주연구원 | 항공기용 익형이 적용된 날개 |
Non-Patent Citations (5)
Title |
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AEROVIRONMENT: "PUMA AE RQ-20A", 29 April 2016 (2016-04-29), pages 1 - 1, XP055962637, Retrieved from the Internet <URL:https://www.avinc.com/images/uploads/product_docs/PumaAE_Datasheet_Web_v1.2.pdf> [retrieved on 20220920] * |
AEROVIRONMENT: "Raven RQ-11A/B", 2 September 2016 (2016-09-02), pages 1 - 1, XP055962633, Retrieved from the Internet <URL:https://www.avinc.com/images/uploads/product_docs/Raven_Datasheet_v1.1.pdf> [retrieved on 20220920] * |
ARSHAD A ET AL: "Design optimization and investigation of aerodynamic characteristics of low Reynolds number airfoils", vol. 22, no. 4, 1 August 2021 (2021-08-01), pages 751 - 764, XP009539231, ISSN: 2093-274X, Retrieved from the Internet <URL:https://link.springer.com/article/10.1007/s42405-021-00362-2/fulltext.html> [retrieved on 20210223], DOI: 10.1007/S42405-021-00362-2 * |
JIN WONJIN ET AL: "Drag Reduction Design for a Long-endurance Electric Powered UAV", INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, vol. 16, no. 2, 30 June 2015 (2015-06-30), Korea, pages 311 - 324, XP055962258, ISSN: 2093-274X, Retrieved from the Internet <URL:https://www.koreascience.or.kr/article/JAKO201524848648005.pdf> [retrieved on 20220920], DOI: 10.5139/IJASS.2015.16.2.311 * |
MCIVER JOHN ET AL: "Cessna Skyhawk II / 100 Performance Assessment Prepared by Cessna Skyhawk II/100 (172) Performance Assessment", 23 January 2003 (2003-01-23), XP055962247, Retrieved from the Internet <URL:http://www.temporal.com.au/c172.pdf> [retrieved on 20220919] * |
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