USD479501S1 - High-speed aircraft - Google Patents
High-speed aircraft Download PDFInfo
- Publication number
- USD479501S1 USD479501S1 US29/168,026 US16802602F USD479501S US D479501 S1 USD479501 S1 US D479501S1 US 16802602 F US16802602 F US 16802602F US D479501 S USD479501 S US D479501S
- Authority
- US
- United States
- Prior art keywords
- speed aircraft
- view
- elevational view
- side elevational
- speed
- 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.)
- Expired - Lifetime
Links
Images
Description
FIG. 1 is a top, left, isometric view of a first embodiment of a high-speed aircraft showing my new design.
FIG. 2 is a top plan view thereof.
FIG. 3 is a bottom plan view thereof.
FIG. 4 is left-side elevational view thereof; the right-side elevational view is a mirror image thereof.
FIG. 5 is a front elevational view thereof.
FIG. 6 is a rear elevational view thereof.
FIG. 7 is a top, left, isometric view of a second embodiment of a high-speed aircraft showing my new design.
FIG. 8 is a top plan view thereof.
FIG. 9 is a bottom plan view thereof.
FIG. 10 is left-side elevational view thereof; the right-side elevational view is a mirror image thereof.
FIG. 11 is a front elevational view thereof.
FIG. 12 is a rear elevational view thereof.
FIG. 13 is a top, left, isometric view of a third embodiment of a high-speed aircraft showing my new design.
FIG. 14 is a top plan view thereof.
FIG. 15 is a bottom plan view thereof.
FIG. 16 is left-side elevational view thereof; the right-side elevational view is a mirror image thereof.
FIG. 17 is a front elevational view thereof.
FIG. 18 is a rear elevational view thereof.
FIG. 19 is a top, left, isometric view of a fourth embodiment of a high-speed aircraft showing my new design.
FIG. 20 is a top plan view thereof.
FIG. 21 is a bottom plan view thereof.
FIG. 22 is left-side elevational view thereof; the right-side elevational view is a mirror image thereof.
FIG. 23 is a front elevational view thereof; and,
FIG. 24 is a rear elevational view thereof.
Elements identified by broken lines in the accompanying drawings form no part of the claimed invention.
Claims (1)
- The ornamental design for a high-speed aircraft, as shown and described.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US29/168,026 USD479501S1 (en) | 2001-03-22 | 2002-09-24 | High-speed aircraft |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US29138990 | 2001-03-22 | ||
| US29152202 | 2001-10-30 | ||
| US29/168,026 USD479501S1 (en) | 2001-03-22 | 2002-09-24 | High-speed aircraft |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US29152202 Continuation | 2001-03-22 | 2001-10-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USD479501S1 true USD479501S1 (en) | 2003-09-09 |
Family
ID=27791269
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US29/168,026 Expired - Lifetime USD479501S1 (en) | 2001-03-22 | 2002-09-24 | High-speed aircraft |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | USD479501S1 (en) |
| AU (3) | AU148312S (en) |
| CA (4) | CA99703S (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060157613A1 (en) * | 2005-01-19 | 2006-07-20 | Adamson Eric E | Supersonic aircraft with active lift distribution control for reducing sonic boom |
| USD809993S1 (en) * | 2016-12-22 | 2018-02-13 | Toshikazu Tsukii | Jet airplane |
| US9950800B2 (en) * | 2014-11-26 | 2018-04-24 | The Boeing Company | Integrated pusher turbofan for aircraft |
-
2001
- 2001-07-19 CA CA 99703 patent/CA99703S/en not_active Expired - Lifetime
- 2001-07-19 CA CA 97203 patent/CA97203S/en not_active Expired - Lifetime
- 2001-07-19 AU AU200102258F patent/AU148312S/en active Active
- 2001-07-19 CA CA 99704 patent/CA99704S/en not_active Expired - Lifetime
- 2001-07-19 CA CA 99702 patent/CA99702S/en not_active Expired - Lifetime
-
2002
- 2002-06-07 AU AU200201717F patent/AU153283S/en active Active
- 2002-09-24 US US29/168,026 patent/USD479501S1/en not_active Expired - Lifetime
-
2003
- 2003-09-12 AU AU200303120F patent/AU156952S/en active Active
Non-Patent Citations (23)
| Title |
|---|
| "Dan Raymer" http://www.aircraftdesign.com/raymer.html [Accessed Oct. 29, 2001]. |
| "Photos Show Key Features of YF-23A ATF," Aviation Week & Space Technology, Jul. 9, 1990. |
| "Prototypes: Comparative Design Analysis," Aviation Week & Space Technology, Sep. 17, 1990. |
| "Rockwell/MBB X-31 Makes Second Flight, Reaching 20,000-Ft. Altitude, Mach 0.6," Aviation Week & Space Techn., p. 117, Oct. 22, 1990. |
| Aircraft Conceptual Design Drawings & Pictures http://www.aircraftdesign.com/acpix.html [Accessed Oct. 30, 2001]. |
| Angelucci, Enzo, "World Encyclopedia of Civil Aircraft, from Leonardo da Vinci to the Present," Crown Publishers, Inc., New York, 1981 (p. 364.). |
| Brennan, Heather, "Spotlight on . . . Daniel Raymer," AIAA Editorial Echoes Interview with Daniel Raymer, Spring 2000 http://www.aircraftdesign.com/sportlighton.html [Accessed Oct. 29, 2001]. |
| Capone, Francis J. and Reubush, David E., "Effects of Varying Podded Nacelle-Nozzle Installations on Transonic Aeropropulsive Characteristics of a Supersonic Fighter Aircraft," NASA Technical Paper 2120, 1983 (pp. 83 and 99). |
| Dryden Flight Research Center, Feb. 1998. |
| International Search Report for International Application No. PCT/US01/02368, Aug. 28, 2001. |
| International Search Report for International Application No. PCT/US02/01567, Dec. 12, 2002 (5 pages). |
| Liebeck, R.H. et al., AIAA 98-0438, Blended-Wing-Body Subsonic Commercial Transport, 36th Aerospace Sciences, Meeting & Exhibit, Jan. 12-15, 1998, Reno, Nevada (pp. 1 and 4). |
| NASA Contractor Report 165934, "Large Payload Capacity SST Concepts—Technical and Economic Feasibility," Contract NAS1-16150, Jul. 1982. |
| NASA Technical Memorandum, "Proceedings of NASA Conference on Supersonic Transport Feasibility Studies and Supporting Research," Sep. 17, 1963 (Figure 45 only). |
| Poisson-Quinton, Philippe, "Slender Wings for Civil and Military Aircraft," Twentieth Israel Annual Conference on Aviation and Astronautics, Feb. 22-23, 1978 (Title Page, p. 57, Figure 5). |
| Rockwell/MBB X31. |
| Roskam, Jan, Dr., "Airplane Design Part II: Preliminary Configuration Design and Integration of the Propulsion System," Roskam Aviation and Engineering Corporation, Ottawa, Kansas, 1985 (pp. 76-78, 81). |
| Scott, William, B., "YF-23A Previews Design Features of Future Fighters," Avaiation Week & Space Technology, Jul. 2, 1990. |
| Stinton, Darrol, "The Anatomy of the Aeroplane," Granada Publishing Limited, 1966 (p. 27, 276, 274, 162). |
| Taylor, Michael J.H., "Jane's Pocket Book of Research and Experimental Aircraft," North American XB-70A Valkyrie, Collier Books, New York, 1976. |
| U.S. patent application Ser. No. 09/671,870, Clark, filed Sep. 27, 2000. |
| U.S. patent application Ser. No. 09/816,985, Seidel, filed Mar. 23, 2001. |
| U.S. patent application Ser. No. 09/822,862, Balzer, filed Mar. 30, 2001. |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060157613A1 (en) * | 2005-01-19 | 2006-07-20 | Adamson Eric E | Supersonic aircraft with active lift distribution control for reducing sonic boom |
| US9950800B2 (en) * | 2014-11-26 | 2018-04-24 | The Boeing Company | Integrated pusher turbofan for aircraft |
| USD809993S1 (en) * | 2016-12-22 | 2018-02-13 | Toshikazu Tsukii | Jet airplane |
Also Published As
| Publication number | Publication date |
|---|---|
| AU148312S (en) | 2002-07-01 |
| CA99704S (en) | 2002-10-10 |
| CA99702S (en) | 2002-10-10 |
| CA99703S (en) | 2002-10-10 |
| AU153283S (en) | 2003-10-14 |
| AU156952S (en) | 2004-11-29 |
| CA97203S (en) | 2002-10-10 |
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