USD764384S1 - Aircraft delta fin - Google Patents
Aircraft delta fin Download PDFInfo
- Publication number
- USD764384S1 USD764384S1 US29/496,588 US201429496588F USD764384S US D764384 S1 USD764384 S1 US D764384S1 US 201429496588 F US201429496588 F US 201429496588F US D764384 S USD764384 S US D764384S
- Authority
- US
- United States
- Prior art keywords
- aircraft
- delta
- fin
- delta fin
- view
- Prior art date
- Legal status (The legal status 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 status listed.)
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Description
The portions of the drawings shown in broken lines indicate surrounding structure and environment that forms no part of the claimed design.
Claims (1)
- The ornamental design for an aircraft delta fin, as shown and described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/496,588 USD764384S1 (en) | 2014-07-15 | 2014-07-15 | Aircraft delta fin |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/496,588 USD764384S1 (en) | 2014-07-15 | 2014-07-15 | Aircraft delta fin |
Publications (1)
Publication Number | Publication Date |
---|---|
USD764384S1 true USD764384S1 (en) | 2016-08-23 |
Family
ID=56683343
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29/496,588 Active USD764384S1 (en) | 2014-07-15 | 2014-07-15 | Aircraft delta fin |
Country Status (1)
Country | Link |
---|---|
US (1) | USD764384S1 (en) |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2960286A (en) * | 1955-10-07 | 1960-11-15 | Chance Vought Aircraft Inc | Means for providing directional stability |
US3738595A (en) * | 1969-10-14 | 1973-06-12 | J Bouchnik | Delta-wing aircraft |
US4291853A (en) * | 1978-12-26 | 1981-09-29 | The Boeing Company | Airplane all-moving airfoil with moment reducing apex |
US6202959B1 (en) * | 1998-08-05 | 2001-03-20 | Bae Systems Plc | Aircraft fin and rudder |
US20040056150A1 (en) * | 2000-12-08 | 2004-03-25 | Morgenstern John M. | Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom |
US7070144B1 (en) * | 2003-01-03 | 2006-07-04 | Orbital Research Inc. | Aircraft and missile afterbody flow control device and method of controlling flow |
USD620876S1 (en) * | 2008-06-11 | 2010-08-03 | Icon Aircraft, Inc. | Aircraft delta fin |
US20120091266A1 (en) * | 2010-10-13 | 2012-04-19 | Whalen Edward A | Active Flow Control on a Vertical Stabilizer and Rudder |
USD739807S1 (en) * | 2013-07-15 | 2015-09-29 | Icon Aircraft, Inc. | Amphibious sport aircraft |
-
2014
- 2014-07-15 US US29/496,588 patent/USD764384S1/en active Active
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2960286A (en) * | 1955-10-07 | 1960-11-15 | Chance Vought Aircraft Inc | Means for providing directional stability |
US3738595A (en) * | 1969-10-14 | 1973-06-12 | J Bouchnik | Delta-wing aircraft |
US4291853A (en) * | 1978-12-26 | 1981-09-29 | The Boeing Company | Airplane all-moving airfoil with moment reducing apex |
US6202959B1 (en) * | 1998-08-05 | 2001-03-20 | Bae Systems Plc | Aircraft fin and rudder |
US20040056150A1 (en) * | 2000-12-08 | 2004-03-25 | Morgenstern John M. | Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom |
US7070144B1 (en) * | 2003-01-03 | 2006-07-04 | Orbital Research Inc. | Aircraft and missile afterbody flow control device and method of controlling flow |
USD620876S1 (en) * | 2008-06-11 | 2010-08-03 | Icon Aircraft, Inc. | Aircraft delta fin |
US20120091266A1 (en) * | 2010-10-13 | 2012-04-19 | Whalen Edward A | Active Flow Control on a Vertical Stabilizer and Rudder |
USD739807S1 (en) * | 2013-07-15 | 2015-09-29 | Icon Aircraft, Inc. | Amphibious sport aircraft |
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