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Patent No. 6125480

Vehicle mounted toilet seat

An extension member is attachable to a trailer hitch and extends away from the vehicle and is connected to a seating frame supporting a toilet seat.

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Class 244/99.1 - Fuselage


Subclass of Class 244 - Aeronautics and astronautics
Definition: Subject matter in which the device or arrangement includes
No. of patents: 9
Last issue date: 05/06/2008


NumberTitleIssue Date
7367530Aerospace vehicle yaw generating systems and associated methods
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system...
05/06/2008
7278609Movable nose cap and control strut assembly for supersonic aircraft
A nose cap and control strut assembly for supersonic aircraft is disclosed. In one embodiment, the nose cap extends forward from the nose of the aircraft to deflect shock waves and decrease draft during supersonic flight. In another embodiment, control struts extend...
10/09/2007
7275722Wing tip device
An aircraft comprises a wing tip device, for example a winglet, a raked-tip device, a wing tip fence or a planar wing extension, mounted in the region of the tip of a wing on the aircraft. The wing tip device is rotatably moveable between a first position and a seco...
10/02/2007
7185859Aerospace vehicle yaw generating systems and associated methods
Aerospace vehicle yaw generating systems and associated methods are disclosed herein. One aspect of the invention is directed toward a yaw generating system that can include an aerospace vehicle having a fuselage with a first portion and a second portion. The system...
03/06/2007
7070144Aircraft and missile afterbody flow control device and method of controlling flow
The present invention relates to an afterbody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization. The present invention further relates to a method of operating the flow control system....
07/04/2006
7048234Adaptive flap and slat drive system for aircraft
A drive station includes two drives connected via drive transmissions to one or more flaps or slats of a flap/slat group. The drives may be mechanically coupled to a rotational shaft, with a shaft brake arranged thereon. Guide transmissions are connected to the shaf...
05/23/2006
4869443Method of extending the performance of a specific jet aircraft
A method of extending the maneuver, performance and flight safety of a specific fighter aircraft, namely, the F-16, is disclosed. In accordance with the method, a portion of the forebody strakes on the original aircraft which extend along each side of the...
09/26/1989
4786009Yaw and pitch control of air vehicles at high angles of attack
Method and apparatus for controlling the yaw and pitch of air vehicles at high angles of attack by controlling the vortex pattern around the forebodies of the air vehicles by means of deflecting strakes 11 and 16....
11/22/1988
4501397Method of stabilizing flight of a flying body and flight-stabilized flying body
A method of stabilizing flight of a flying body having a circular cross-section by the use of a plurality of tripping wires, when the flying body flies in an air current at a high angle of attack with respect to the air current. And also a flight-stabiliz...
02/26/1985
 
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