CA174562S - Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors - Google Patents

Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors

Info

Publication number
CA174562S
CA174562S CA174562F CA174562F CA174562S CA 174562 S CA174562 S CA 174562S CA 174562 F CA174562 F CA 174562F CA 174562 F CA174562 F CA 174562F CA 174562 S CA174562 S CA 174562S
Authority
CA
Canada
Prior art keywords
vtol
landing
view
air vehicle
vertical take
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
CA174562F
Other versions
CA958048A (en
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.)
Aerovironment Inc
Original Assignee
Aerovironment 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 Aerovironment Inc filed Critical Aerovironment Inc
Application granted granted Critical
Publication of CA174562S publication Critical patent/CA174562S/en
Active legal-status Critical Current
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Links

Abstract

The design is the visual features of the VERTICAL TAKE-OFF AND LANDING (VTOL) WINGED AIR VEHICLE WITH COMPLEMENTARY ANGLED ROTORS shown in solid lines in the drawings, whether those features are of shape, configuration, ornament, or pattern, or are a combination of any of these features. Shading is used in the drawings to better illustrate the design.Drawings of the design are included.FIG. 1 is a front perspective view of the vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors;FIG. 2 is a rear perspective view of FIG. 1;FIG. 3 is a front elevational view of FIG. 1;FIG. 4 is a rear elevational view of FIG. 1;FIG. 5 is a right side elevational view of FIG. 1;FIG. 6 is a left side elevational view of FIG. 1;FIG. 7 is top plan view of FIG. 1; andFIG. 8 is a bottom plan view of FIG. 1.
CA174562F 2016-11-04 2017-05-03 Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors Active CA174562S (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/583,481 USD813143S1 (en) 2016-11-04 2016-11-04 Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors

Publications (1)

Publication Number Publication Date
CA174562S true CA174562S (en) 2018-05-31

Family

ID=61008531

Family Applications (1)

Application Number Title Priority Date Filing Date
CA174562F Active CA174562S (en) 2016-11-04 2017-05-03 Vertical take-off and landing (vtol) winged air vehicle with complementary angled rotors

Country Status (4)

Country Link
US (1) USD813143S1 (en)
JP (1) JP1596010S (en)
AU (1) AU201712218S (en)
CA (1) CA174562S (en)

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Also Published As

Publication number Publication date
JP1596010S (en) 2018-01-29
AU201712218S (en) 2017-05-15
USD813143S1 (en) 2018-03-20

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