USD764384S1 - Aircraft delta fin - Google Patents

Aircraft delta fin Download PDF

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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
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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.)
Active
Application number
US29/496,588
Inventor
Dong Tran
Klaus Tritschler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sg Investment America Inc
Icon Aircraft Inc
Original Assignee
Icon Aircraft Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Icon Aircraft Inc filed Critical Icon Aircraft Inc
Priority to US29/496,588 priority Critical patent/USD764384S1/en
Assigned to ICON AIRCRAFT, INC. reassignment ICON AIRCRAFT, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: TRAN, DONG, TRITSCHLER, KLAUS
Application granted granted Critical
Publication of USD764384S1 publication Critical patent/USD764384S1/en
Assigned to SG INVESTMENT AMERICA, INC reassignment SG INVESTMENT AMERICA, INC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SEAPLANE DEBTOR 1, INC., FORMERLY ICON AIRCRAFT, INC.
Assigned to SG Investment America, Inc. reassignment SG Investment America, Inc. CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE PREVIOUSLY RECORDED ON REEL 70512 FRAME 771. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Assignors: SEAPLANE DEBTOR 1, INC., FORMERLY ICON AIRCRAFT, INC.
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

FIG. 1 is a rear, top perspective drawing of an aircraft delta fin showing our new design and its environment.
FIG. 2 is a detailed rear, top perspective view thereof;
FIG. 3 is a right side perspective view thereof;
FIG. 4 is a left side perspective view thereof;
FIG. 5 is a back plan view thereof; and,
FIG. 6 is a bottom plan view of thereof.
The portions of the drawings shown in broken lines indicate surrounding structure and environment that forms no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for an aircraft delta fin, as shown and described.
US29/496,588 2014-07-15 2014-07-15 Aircraft delta fin Active USD764384S1 (en)

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

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US (1) USD764384S1 (en)

Citations (9)

* Cited by examiner, † Cited by third party
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

Patent Citations (9)

* Cited by examiner, † Cited by third party
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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