USD926665S1 - Set of aircraft canards - Google Patents

Set of aircraft canards Download PDF

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Publication number
USD926665S1
USD926665S1 US29/692,499 US201929692499F USD926665S US D926665 S1 USD926665 S1 US D926665S1 US 201929692499 F US201929692499 F US 201929692499F US D926665 S USD926665 S US D926665S
Authority
US
United States
Prior art keywords
aircraft
canards
view
plan
ornamental design
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
US29/692,499
Inventor
Brian D. Morrison
Andre H. De Salis
Martti J. Lampela
Adil M. Ali
Peter F. Falt
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.)
Alakai Technologies Corp
Original Assignee
Alakai Technologies Corp
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 Alakai Technologies Corp filed Critical Alakai Technologies Corp
Priority to US29/692,499 priority Critical patent/USD926665S1/en
Assigned to ALAKAI TECHNOLOGIES CORPORATION reassignment ALAKAI TECHNOLOGIES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ALI, ADIL M., DE SALIS, ANDRE H., FALT, PETER F., LAMPELA, MARTTI J., MORRISON, BRIAN D.
Application granted granted Critical
Publication of USD926665S1 publication Critical patent/USD926665S1/en
Active legal-status Critical Current
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Description

FIG. 1 is a left side plan view of the set of aircraft canards;
FIG. 2 is a right side plan view of the set of aircraft canards;
FIG. 3 is a front plan view of the set of aircraft canards;
FIG. 4 is a right front elevated isometric view of the set of aircraft canards; and,
FIG. 5 is a top plan view of the set of aircraft canards.
The broken line showing of the aircraft is for the purpose of illustrating the environmental structure in which the claimed elements are found and forms no part of the claimed design.
In addition, thick lines are used to outline objects, while thin lines show contours.

Claims (1)

    CLAIM
  1. The ornamental design for a set of aircraft canards, as shown and described.
US29/692,499 2019-05-24 2019-05-24 Set of aircraft canards Active USD926665S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/692,499 USD926665S1 (en) 2019-05-24 2019-05-24 Set of aircraft canards

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/692,499 USD926665S1 (en) 2019-05-24 2019-05-24 Set of aircraft canards

Publications (1)

Publication Number Publication Date
USD926665S1 true USD926665S1 (en) 2021-08-03

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ID=77040179

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/692,499 Active USD926665S1 (en) 2019-05-24 2019-05-24 Set of aircraft canards

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US (1) USD926665S1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD978768S1 (en) * 2021-05-13 2023-02-21 Alakai Technologies Corporation Aircraft airframe

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848700A (en) * 1987-04-16 1989-07-18 Lockheed John A Canard control system for aircraft
US5454530A (en) * 1993-05-28 1995-10-03 Mcdonnell Douglas Helicopter Company Canard rotor/wing
US20040262450A1 (en) * 2002-09-30 2004-12-30 Cordy Clifford B Better balanced canard airplane with forward engine
US20140339354A1 (en) * 2013-03-15 2014-11-20 Ian Todd Gaillimore Vertical Takeoff and Landing ("VTOL") Aircraft
US20160200436A1 (en) * 2013-08-13 2016-07-14 U.S.A. As Represented By The Administrator Of The National Aeronautics And Space Administration Tri-Rotor Aircraft Capable of Vertical Takeoff and Landing and Transitioning to Forward Flight
US20170137122A1 (en) * 2013-08-14 2017-05-18 Bell Helicopter Textron Inc. Maintaining Drive System Alignment in Tiltrotor Aircraft
USD814972S1 (en) * 2016-08-05 2018-04-10 Samsung Electronics Co., Ltd. Drone
US9981734B2 (en) * 2016-09-19 2018-05-29 Bell Helicopter Textron Inc. Cross-wing driveshaft channel
US20180257764A1 (en) * 2017-03-08 2018-09-13 Toyota Motor Engineering & Manufacturing North America, Inc. Suspension for landing condition
US20180297695A1 (en) * 2015-10-16 2018-10-18 4Front Robotics Ltd. Rotary wing aircraft
USD858420S1 (en) * 2015-12-18 2019-09-03 Leonardo S.P.A. Combined airplane and scale model
US20200086971A1 (en) * 2018-09-14 2020-03-19 Bell Helicopter Textron Inc. Tiltrotor Free-Pivot Wing Extension

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4848700A (en) * 1987-04-16 1989-07-18 Lockheed John A Canard control system for aircraft
US5454530A (en) * 1993-05-28 1995-10-03 Mcdonnell Douglas Helicopter Company Canard rotor/wing
US20040262450A1 (en) * 2002-09-30 2004-12-30 Cordy Clifford B Better balanced canard airplane with forward engine
US20140339354A1 (en) * 2013-03-15 2014-11-20 Ian Todd Gaillimore Vertical Takeoff and Landing ("VTOL") Aircraft
US20160200436A1 (en) * 2013-08-13 2016-07-14 U.S.A. As Represented By The Administrator Of The National Aeronautics And Space Administration Tri-Rotor Aircraft Capable of Vertical Takeoff and Landing and Transitioning to Forward Flight
US20170137122A1 (en) * 2013-08-14 2017-05-18 Bell Helicopter Textron Inc. Maintaining Drive System Alignment in Tiltrotor Aircraft
US20180297695A1 (en) * 2015-10-16 2018-10-18 4Front Robotics Ltd. Rotary wing aircraft
USD858420S1 (en) * 2015-12-18 2019-09-03 Leonardo S.P.A. Combined airplane and scale model
USD814972S1 (en) * 2016-08-05 2018-04-10 Samsung Electronics Co., Ltd. Drone
US9981734B2 (en) * 2016-09-19 2018-05-29 Bell Helicopter Textron Inc. Cross-wing driveshaft channel
US20180257764A1 (en) * 2017-03-08 2018-09-13 Toyota Motor Engineering & Manufacturing North America, Inc. Suspension for landing condition
US20200086971A1 (en) * 2018-09-14 2020-03-19 Bell Helicopter Textron Inc. Tiltrotor Free-Pivot Wing Extension

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD978768S1 (en) * 2021-05-13 2023-02-21 Alakai Technologies Corporation Aircraft airframe

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