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USD919547S1 - Aircraft fuselage - Google Patents

Aircraft fuselage Download PDF

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Publication number
USD919547S1
USD919547S1 US29/719,438 US202029719438F USD919547S US D919547 S1 USD919547 S1 US D919547S1 US 202029719438 F US202029719438 F US 202029719438F US D919547 S USD919547 S US D919547S
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US
United States
Prior art keywords
aircraft fuselage
fuselage
aircraft
view
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
US29/719,438
Inventor
Joseph Richard Carpenter
Timothy Carr
Matthew E. Louis
Steve Michael Loveland
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.)
Bell Textron Rhode Island Inc
Original Assignee
Bell Textron 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 Bell Textron Inc filed Critical Bell Textron Inc
Priority to US29/719,438 priority Critical patent/USD919547S1/en
Assigned to Bell Textron Inc. reassignment Bell Textron Inc. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: LOUIS, MATTHEW E., LOVELAND, Steve Michael, CARR, TIMOTHY, CARPENTER, Joseph Richard
Application granted granted Critical
Publication of USD919547S1 publication Critical patent/USD919547S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

FIG. 1 is a perspective view of our new design for an aircraft fuselage;
FIG. 2 is a side view in elevation of the aircraft fuselage as shown in FIG. 1;
FIG. 3 is a top plan view of the aircraft fuselage as shown in FIG. 1;
FIG. 4 is a front elevational view of the aircraft fuselage as shown in FIG. 1;
FIG. 5 is a bottom plan view of the aircraft fuselage as shown in FIG. 1; and,
FIG. 6 is a rear elevational view of the aircraft fuselage as shown in FIG. 1.
The broken lines in the drawings are for the purpose of illustrating environmental structure and form no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for an aircraft fuselage, substantially as shown and described.
US29/719,438 2020-01-03 2020-01-03 Aircraft fuselage Active USD919547S1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/719,438 USD919547S1 (en) 2020-01-03 2020-01-03 Aircraft fuselage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/719,438 USD919547S1 (en) 2020-01-03 2020-01-03 Aircraft fuselage

Publications (1)

Publication Number Publication Date
USD919547S1 true USD919547S1 (en) 2021-05-18

Family

ID=75865997

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/719,438 Active USD919547S1 (en) 2020-01-03 2020-01-03 Aircraft fuselage

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US (1) USD919547S1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD1045752S1 (en) * 2021-09-27 2024-10-08 Honda Motor Co., Ltd. Manned aircraft

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120043413A1 (en) * 2005-10-18 2012-02-23 Smith Frick A Apparatus and method for vertical take-off and landing aircraft
US20120234968A1 (en) * 2005-10-18 2012-09-20 Smith Frick A Aircraft with freewheeling engine
US20180057157A1 (en) * 2016-08-31 2018-03-01 Bell Helicopter Textron Inc. Tilting Ducted Fan Aircraft Generating a Pitch Control Moment
US20190291860A1 (en) * 2016-10-27 2019-09-26 Mono Aerospace Ip Ltd Vertical take-off and landing aircraft and control method
US10562620B2 (en) * 2016-09-28 2020-02-18 Wisk Aero Llc Tilt-wing aircraft
USD887948S1 (en) * 2019-01-03 2020-06-23 Bell Helicopter Textron Inc. Aircraft
US20200223530A1 (en) * 2019-01-15 2020-07-16 Bell Helicopter Textron Inc. Ducted fan assembly with curved stators
US20200239134A1 (en) * 2019-01-25 2020-07-30 Bell Helicopter Textron Inc. Hybrid-electric ducted fan transport
US20200255135A1 (en) * 2017-09-28 2020-08-13 Seung il HONG Vertical takeoff and landing aircraft
US20200262553A1 (en) * 2019-02-18 2020-08-20 Roberto Gomez Hybrid electric-jet powered

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120043413A1 (en) * 2005-10-18 2012-02-23 Smith Frick A Apparatus and method for vertical take-off and landing aircraft
US20120234968A1 (en) * 2005-10-18 2012-09-20 Smith Frick A Aircraft with freewheeling engine
US20180057157A1 (en) * 2016-08-31 2018-03-01 Bell Helicopter Textron Inc. Tilting Ducted Fan Aircraft Generating a Pitch Control Moment
US10562620B2 (en) * 2016-09-28 2020-02-18 Wisk Aero Llc Tilt-wing aircraft
US20190291860A1 (en) * 2016-10-27 2019-09-26 Mono Aerospace Ip Ltd Vertical take-off and landing aircraft and control method
US20200255135A1 (en) * 2017-09-28 2020-08-13 Seung il HONG Vertical takeoff and landing aircraft
USD887948S1 (en) * 2019-01-03 2020-06-23 Bell Helicopter Textron Inc. Aircraft
US20200223530A1 (en) * 2019-01-15 2020-07-16 Bell Helicopter Textron Inc. Ducted fan assembly with curved stators
US20200239134A1 (en) * 2019-01-25 2020-07-30 Bell Helicopter Textron Inc. Hybrid-electric ducted fan transport
US20200262553A1 (en) * 2019-02-18 2020-08-20 Roberto Gomez Hybrid electric-jet powered

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Bell Reveals the City of the Future at CES 2020 (article) [Jan. 6, 2020] found online [Nov. 30, 2020]—https://news.bellflight.com/en-US/184550-bell-reveals-the-city-of-the-future-at-ces-2020. *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD1045752S1 (en) * 2021-09-27 2024-10-08 Honda Motor Co., Ltd. Manned aircraft

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