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Patent No. 5265827

Paddle Wheel Plane

An aircraft having vertical takeoff and landing capability provided with at least first and second laterally extending paddle wheels rotatable on a central axis perpendicular to the longitudinal axis of the aircraft fuselage and between its nose and tail.

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Class 244/89 - Elevators both front and rear


Subclass of Class 244 - Aeronautics and astronautics
Definition: Horizontal rudders arranged at both the front and the rear
No. of patents: 21
Last issue date: 01/17/2012


NumberTitleIssue Date
8096500Mobile surfaces for aircraft with sealed slots
A lifting or stabilising component (11) for an aircraft comprising in the area of its trailing edge a rotary control element (13) rotating around an axis (61) with at least one slot (21) between the tip (15) of the component (11...
01/17/2012
7410133Miniature trailing edge effector for aerodynamic control
Improved miniature trailing edge effectors for aerodynamic control are provided. Three types of devices having aerodynamic housings integrated to the trailing edge of an aerodynamic shape are presented, which vary in details of how the control surface can move. A bu...
08/12/2008
7234667Modular aerospace plane
This invention relates to the design of a Modular Aerospace Plane (MAP) comprising a forward fuselage section, a main wing section, a tail section and wing attachments. Various sections can be integrated to offer a variety of aircraft characteristics, performance an...
06/26/2007
7111810Forward pivoted full flying control tail boom
An aircraft motion control mechanism for regulating aircraft motion from a location remote from an aircraft body portion. The aircraft auxiliary control mechanism has at least one control surface support arm connected to and extending from the aircraft body portion,...
09/26/2006
6986695Method for attaching an empennage assembly to a model airplane
An empennage assembly for a model aircraft. The empennage assembly includes a fuselage having a bottom portion with an opening and a housing positioned in the opening in the bottom portion of the fuselage. The housing has a first end defining an opening and a second...
01/17/2006
6935592Aircraft lift device for low sonic boom
An aircraft lift device comprises a strake capable of coupling to an aircraft fuselage and extending to a leading edge of a wing. The strake has a leading edge. The life device further comprises a leading-edge flap coupled to the strake leading edge. ...
08/30/2005
6804586Arrangement for generating control commands for actuating flaps and slats of an aircraft
An arrangement for generating control commands for controlling the slats and landing flaps of an aircraft includes two manually operable command input levers which are arranged directly side-by-side or as a “rod-within-rod” and are connected respectively by two ...
10/12/2004
6729583Device for articulating a flap to an aircraft aerodynamic surface
An articulation device for articulating a flap to an aircraft aerodynamic surface, the flap having its front edge facing a rear edge of the aerodynamic surface and the articulation device including two fittings bearing the flap. The articulation device pivots about ...
05/04/2004
6698688Apparatus and methods for actuating rotatable members
Apparatus and methods for actuating rotatable members are disclosed. In one embodiment, an assembly for actuating a rotatable member includes an extendible actuator having a first end and a second end, and a drive member having a first portion pivotally c...
03/02/2004
6575406Integrated and/or modular high-speed aircraft
An integrated and/or modular high-speed aircraft and method of design and manufacture. The aircraft can have a supersonic or near-sonic cruise Mach number. In one embodiment, the aircraft can include an aft body integrated with a delta wing and a rearward...
06/10/2003
6543720Directional control and aerofoil system for aircraft
An aircraft is disclosed. The aircraft has a canard control surface 25 and an aft control surface 10. The canard control surface comprises an integral aerofoil which in its entirety pivots about a first axis of rotation 28. The canard control surface has ...
04/08/2003
6220551Flight controls with automatic balance
Flight controls with automatic balance for use in controlling the movement of an aircraft through a fluid system, the control system includes ailerons divided into two parts, which at lower speed adopt the shape of a conventional aileron and rotate in the...
04/24/2001
5722615Transport airplane with front empennage
Airplane (1) including a mainplane (3), elevator aerodynamic surfaces (4) and a front canard empennage adjustable in orientation. This airplane includes: a device for calculating (14) continuously receiving measurements: of the speed (V) of the airplane with r...
03/03/1998
5542625Gull wing aircraft
A vehicle, lacking an empennage, has a gull wing with ailerons movably mounted at the trailing edges of the wing for controlling pitch, yaw and roll, or has a wing and a gull tail with flaps movably mounted at the trailing edges of the tail surface for co...
08/06/1996
5322243Separately banking maneuvering aerodynamic control surfaces, system and method
A maneuvering system for a flight vehicle rotates a lifting aerodynamic surface of the flight vehicle about an axis parallel with a direction of flight of the vehicle in a rotational direction corresponding to the desired change of flight direction to whi...
06/21/1994
5201478Airplane efficiency, safety and utilization
This invention involves a simple but radical approach to airplane design. Many advantages and benefits result therefrom including improved flight efficiency, better handling and control response, less tail area required, increased safety, increased utilit...
04/13/1993
5082204All wing aircraft
An all-wing aircraft is disclosed that has novel foreplane and depending aftplane, a center wing section and outer wing panel flying surfaces which cooperate aerodynamically to eliminate the need for conventional fuselage and tail structures. The foreplan...
01/21/1992
4813634Flying emergency ejection seat
A flying emergency ejection seat for endangered airman to escape from distressed aircraft and to fly cross country in the seat to sanctuary of a more favorable environment for recovery having the following existing state-of-the-art non-flying seat surviva...
03/21/1989
4746081Aircraft
This invention relates to an aircraft having three lift surfaces, and precisely a main wing lift surface located in an intermediate position of the aircraft and two less extended lift surfaces positioned, respectively, in a position ahead of the main wing...
05/24/1988
4037808Travelling tail-unit with circular arc motion
Aircraft having subsonic and supersonic flight capabilities which utilize travelling tail units with circular arc motions, connected with the rear fuselage by means of two arm-frames that swing upward and rearward and vice versa, to generally increase sta...
07/26/1977
4010920Apparatus and method to control forward control surface type aircraft in flight
The control surface-type wing, forward of the center of gravity of the aircraft is placed to be shiftable longitudinally with respect to the center of gravity of the aircraft and also adjustable with respect to a transverse and longitudinal axis of the ai...
03/08/1977
 
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