Class Information
Number: D12/337
Name: Transportation > Aircraft, spacecraft, or fuselage > T-tail empennage, i.e., stabilizer mounted at top of rudder or vertical fin
Description:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| D582832 |
Airplane |
Dec. 16, 2008 |
| D466858 |
Unmanned data gathering aircraft |
Dec. 10, 2002 |
| D431522 |
Airplane |
Oct. 3, 2000 |
| D426804 |
Surface configuration of an airplane |
Jun. 20, 2000 |
| D421955 |
Surface configuration of an airplane |
Mar. 28, 2000 |
| D415993 |
Surface configuration of a vehicle |
Nov. 2, 1999 |
| D394422 |
Tilt rotor aircraft |
May. 19, 1998 |
| D358576 |
Large, single deck airplane |
May. 23, 1995 |
| D358577 |
Large, single deck airplane with elevated flight deck |
May. 23, 1995 |
| D352493 |
Airplane |
Nov. 15, 1994 |
| D349271 |
Airplane |
Aug. 2, 1994 |
| D339319 |
Aircraft |
Sep. 14, 1993 |
| D337095 |
Sporting aeroplane |
Jul. 6, 1993 |
| D332079 |
Dual mode aircraft |
Dec. 29, 1992 |
| 5167383 |
STOL aircraft |
Dec. 1, 1992 |
| 5114097 |
Aircraft |
May. 19, 1992 |
| D325557 |
Airplane |
Apr. 21, 1992 |
| 5096142 |
Folding internal cover |
Mar. 17, 1992 |
| 5072894 |
Apparatus and method for increasing the angle of attack operating range of an aircraft |
Dec. 17, 1991 |
| 5062595 |
Delta wing with lift enhancing flap |
Nov. 5, 1991 |
| D317432 |
Airplane |
Jun. 11, 1991 |
| D311514 |
Light air plane |
Oct. 23, 1990 |
| D308663 |
Airplane |
Jun. 19, 1990 |
| D304924 |
Aircraft |
Dec. 5, 1989 |
| D304925 |
Aircraft |
Dec. 5, 1989 |
| D280892 |
Aircraft |
Oct. 8, 1985 |
| D267794 |
Aircraft design |
Feb. 1, 1983 |
| D264838 |
Aircraft |
Jun. 8, 1982 |
| D258649 |
Airplane |
Mar. 24, 1981 |
| D258648 |
Airplane |
Mar. 24, 1981 |
| D258647 |
Airplane |
Mar. 24, 1981 |
| D256792 |
Aircraft |
Sep. 9, 1980 |
| D244843 |
Airplane |
Jun. 28, 1977 |
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