USD381938S - Tactical aircraft decoy, conjugal tandem design - Google Patents
Tactical aircraft decoy, conjugal tandem design Download PDFInfo
- Publication number
- USD381938S USD381938S US29/043,312 US4331295F USD381938S US D381938 S USD381938 S US D381938S US 4331295 F US4331295 F US 4331295F US D381938 S USD381938 S US D381938S
- Authority
- US
- United States
- Prior art keywords
- conjugal
- tactical aircraft
- tandem design
- aircraft decoy
- decoy
- 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 front perspective view of the invention;
FIG. 2 is a side view of the invention;
FIG. 3 is a top view of the invention;
FIG. 4 is a bottom view of the invention;
FIG. 5 is a front end view of the invention; and,
FIG. 6 is a rear end view of the invention.
Claims (1)
- The ornamental design for a tactical aircraft decoy, conjugal tandem design, as shown and described.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US29/043,312 USD381938S (en) | 1995-08-31 | 1995-08-31 | Tactical aircraft decoy, conjugal tandem design |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US29/043,312 USD381938S (en) | 1995-08-31 | 1995-08-31 | Tactical aircraft decoy, conjugal tandem design |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| USD381938S true USD381938S (en) | 1997-08-05 |
Family
ID=71463995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US29/043,312 Expired - Lifetime USD381938S (en) | 1995-08-31 | 1995-08-31 | Tactical aircraft decoy, conjugal tandem design |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | USD381938S (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6575406B2 (en) | 2001-01-19 | 2003-06-10 | The Boeing Company | Integrated and/or modular high-speed aircraft |
| US6651928B1 (en) | 2002-09-05 | 2003-11-25 | The Boeing Company | Aircraft engine nacelles and methods for their manufacture |
| US20060157613A1 (en) * | 2005-01-19 | 2006-07-20 | Adamson Eric E | Supersonic aircraft with active lift distribution control for reducing sonic boom |
| US7644888B2 (en) | 2002-05-15 | 2010-01-12 | The Boeing Company | High-speed aircraft and methods for their manufacture |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5494239A (en) * | 1994-08-02 | 1996-02-27 | Loral Vought Systems Corporation | Expandable ogive |
-
1995
- 1995-08-31 US US29/043,312 patent/USD381938S/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5494239A (en) * | 1994-08-02 | 1996-02-27 | Loral Vought Systems Corporation | Expandable ogive |
Non-Patent Citations (1)
| Title |
|---|
| Popular Science, Jul. 1986, p. 37, Aerospace plane. |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6575406B2 (en) | 2001-01-19 | 2003-06-10 | The Boeing Company | Integrated and/or modular high-speed aircraft |
| US20040016845A1 (en) * | 2001-01-19 | 2004-01-29 | Nelson Chester P. | Integrated and/or modular high-speed aircraft |
| US6938854B2 (en) | 2001-01-19 | 2005-09-06 | The Boeing Company | Integrated and/or modular high-speed aircraft |
| US7644888B2 (en) | 2002-05-15 | 2010-01-12 | The Boeing Company | High-speed aircraft and methods for their manufacture |
| US6651928B1 (en) | 2002-09-05 | 2003-11-25 | The Boeing Company | Aircraft engine nacelles and methods for their manufacture |
| US20040144889A1 (en) * | 2002-09-05 | 2004-07-29 | Stuhr Victor K. | Aircraft engine nacelles and methods for their manufacture |
| US6966524B2 (en) | 2002-09-05 | 2005-11-22 | The Boeing Company | Aircraft engine nacelles and methods for their manufacture |
| US20060157613A1 (en) * | 2005-01-19 | 2006-07-20 | Adamson Eric E | Supersonic aircraft with active lift distribution control for reducing sonic boom |
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