Matches 1 - 33 out of 33


Match Document Document Title
US20110309187 NESTED CORE GAS TURBINE ENGINE  
An aircraft, with the ability to cruise at supersonic speeds, designed to increase cruise lift/drag ratio, reduce sonic boom and have greater downward visibility by having an ‘inverted’ nose...
US20110121130 BLENDED WING BODY CARGO AIRPLANE  
A blended wing body cargo aircraft is disclosed. A body section defines a cargo volume, where an outer surface of the body section is shaped to provide an aerodynamic lifting surface. A cargo door...
US20130306788 UNMANNED AIR SYSTEM (UAS)  
An unmanned air system and method with blown flaps are presented. Air is guided to a fuel cell carried by the unmanned air system. The fuel cell is ventilated by the guided air such that the air...
US20140103159 Tunnel wing system for lift, altitude flight, and ground effect flight  
Aircraft comprising a single wing suspended under a closed sided chassis. The wing spar is mounted to the sides that enclose and channel the airflow over and under the wing to provide lift....
US20140175215 FLYING WING WITH SIDE CARGO COMPARTMENT  
Optimization of the use of the available volume in a flying wing for commercial passenger transport, in particular for short- or medium-haul routes. A flying wing is provided including a passenger...
US20120091262 FORWARD SWEPT WINGLET  
An aircraft may include a pair of wings. A forward swept winglet may be attached proximate to a wing tip of each wing. The forward swept winglet may include a leading edge and a trailing edge. The...
US20090152392 PARAMETRIC GEOMETRY MODEL FOR A BLENDED WING BODY  
Lofting of a Blended Wing Body air vehicle is accomplished by first determining the required payload volume of the air vehicle. The payload volume is then analyzed to determine a list of corner...
US20130341459 Compression-lift aircraft  
A supersonic aircraft design using compression lift for enhanced cruise performance. Each engine nacelle at mid-span has a vertical wedge at the nose which creates shock waves under the wings. The...
US20100187352 MULTI DECK AIRCRAFT  
The invention relates to multi deck passenger aircraft, having passenger cabins and/or service facilities arranged on the upper and lower deck and inner load bearing cell structure provided within...
US20090230238 Aircraft fuselage structure  
An aircraft fuselage structure is described for a flying-wing aircraft, having a central area of slight curvature and side areas of greater curvature, which forms a pressure body and has an outer...
US20050178884 Flight device with a lift-generating fuselage  
The invention relates to an aircraft comprising a lift-producing fuselage (1) whose largest span (11) lies in the middle third (14) of the total length and whose horizontal projection...
US20140231593 Multi-Role Aircraft With Interchangeable Mission Modules  
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections...
US20120292435 Multi-Role Aircraft with Interchangeable Mission Modules  
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections...
US20100012773 Aircrft Structure  
An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear delta wings, vertical winglets, and three levels. The fuselage has a cross-section...
US20100252674 Reducing runway requirement for aircraft  
Runway length requirement for take-off and landing of an aircraft is reduced by taking advantage of dynamic lift overshoot, and in some cases, dynamic stall. In take-off and landing, the angle of...
US20100102165 Method for Improving the Performance of an Aircraft  
According to the invention, the nose cone (2.I) of the aircraft is modified so as to increase the lifting resultant (R′).
US20070187550 Integrated inward turning inlets and nozzles for hypersonic air vehicles  
A hypersonic waverider aircraft is disclosed that includes a first engine and an inlet including a throat. The inlet is configured to generate three-dimensional flow compression during hypersonic...
US20100163669 Super aircraft structrue  
An aircraft structure is provided. The aircraft structure for an aircraft includes a fuselage, front wings, rear small wings, vertical winglets, and four levels. The fuselage has a cross-section...
US20080277524 METHODS AND APPARATUS FOR AIRCRAFT  
Methods and apparatus for aircraft according to various aspects of the present invention operate in conjunction with a fuselage and a wing. The fuselage may be configured to generate lift in...
US20070170309 Flight device (aircraft) with a lift-generating fuselage  
An aircraft has a lift-generating fuselage (1), the largest span (11) of the fuselage being in the third fifth (15) or the four fifth (17) of the total length thereof. The outline of the fuselage...
US20100163670 DELTOID MAIN WING AERODYNAMIC CONFIGURATIONS  
Deltoid Main Wing idea provides for several innovative aerodynamic configurations for large subsonic and supersonic civil and military aircraft including “T-tailed Deltoid Main Wing” configuration...
US20100213308 POSITIVE-PRESSURE FLYING AIRCRAFT  
Provided is a positive-pressure floating type airplane comprising an airfoil portion, left-right fuselages, a central fuselage, an elevator and a rudder disposed at the back of the airfoil...
US20120256043 ANNULAR AIRBORNE VEHICLE  
An airborne vehicle having a wing-body which defines a wing-body axis and appears substantially annular when viewed along the wing-body axis, the interior of the annulus defining a duct which is...
US20150122942 METHOD FOR GENERATING LIFT AND A DEVICE FOR IMPLEMENTING METHOD  
The object of the invention is a method for generating lift for an airborne flying device, which has a wing part and/or a fuselage part generating lift by means of interactive movement between the...
US20100243795 OBLIQUE BLENDED WING BODY AIRCRAFT  
An oblique wing aircraft (1) designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment (27) on one side of the wing and an aft...
US20170158309 OBLIQUE BLENDED WING BODY AIRCRAFT  
An oblique wing aircraft designed for reduced surface area to volume ratio. The aircraft has an oblique wing comprising a forward swept wing segment and an aft swept wing segment. A center oblique...
US20160368603 Stealth Aerial Vehicle  
An aerial vehicle having a low radar signature includes a first side on which turbine openings, and payload bays or landing gear bays are disposed. A second side of the aerial vehicle is designed...
US20160207630 AIRCRAFT  
An aircraft (2) comprises at least first and second gas turbine engines (10a, 10b) arranged in a line extending generally normally to an aircraft longitudinal axis (A), each engine (10a, 10b)...
US20160137290 RECESSED LIFT SPOILER ASSEMBLY FOR AIRFOILS  
A spoiler assembly is provided that is engageable to a UAV that defines a body, an outer surface and an inner surface. The spoiler assembly comprises a spoiler, translatably connected to the UAV...
US20160075423 Multi-Role Aircraft With Interchangeable Mission Modules  
A flight-operable, truly modular aircraft has an aircraft core to which one or more of outer wings members, fuselage, cockpit, leading and trailing edge couplings, and empennage and tail sections...
US20160052619 SIMPLIFIED INVERTED V-TAIL STABILIZER FOR AIRCRAFT  
The simplified inverted V-tail aircraft comprise of fixed inverted V-tail stabilizers, wing mounted elevons, with no moving control surfaces attached to the fixed inverted V-tail stabilizers....
US20160009391 Stable Low Aspect Ratio Flying Wing  
A low aspect ratio flying wing provides aerodynamic stability throughout the flight envelope with improved aerodynamic efficiency. Insufficient stability and reduced aerodynamic efficiency typical...
US20150375862 Stealth Aerial Vehicle  
An aerial vehicle having a low radar signature includes a first side on which turbine openings, and payload bays or landing gear bays are disposed. A second side of the aerial vehicle is designed...

Matches 1 - 33 out of 33