Sunstar S Im

US Patent:

8439294, May 14, 2013

Filed:

Apr 9, 2009

Appl. No.:

12/384802

Inventors:

Sunstar Im - Lancaster CA, US

International Classification:

B64B 1/06

US Classification:

244 30

Abstract:

The structure provided multi-Levels of the center fuselage, two front wings, Extended mid-two wings and two rear wings with two vertical winglets. The fuselage has a cross section of half circle shaped fuselage. The first level comprises multi-fuel tanks, water tanks, Helium gas tanks, hydraulic, Pneumatic systems and plurality of the multi-landing gear bays and multi-cargo Compartments. The first level comprises a top cockpit and the plurality of the multi-passenger Cabins. The second level is comprises multi-central posts, multi-guy wires on the top center Beams, mid level, lower level center beams, leak proof sealed floor gates for the Multi-gas envelopes structure, under belly multi-pontoon air bags. The first level further comprises multi-jet power plants with multi-chute flaps. The second level may comprises, carbon fiber honey comb sandwich composite Multi-envelopes and multi-level soft gas envelopes.

US Patent:

8459596, Jun 11, 2013

Filed:

Dec 1, 2009

Appl. No.:

12/592655

Inventors:

Sunstar Im - Lancaster CA, US

International Classification:

B64G 1/00
B64G 1/24
B64G 1/26
B64G 1/62

US Classification:

2441581, 2441584, 2441589, 2441724

Abstract:

A sky/space elevator vehicle for going from the surface of a planet or moon up into space and back again. The vehicle has a single fuselage comprising multiple floor sections including a top and bottom cone. The movement of the vehicle is controlled by helium filled envelops as well as a combined jet and rocket propulsion system.

US Patent:

8464979, Jun 18, 2013

Filed:

Jun 2, 2009

Appl. No.:

12/455473

Inventors:

Sunstar Im - Lancaster CA, US

International Classification:

B64C 3/00
B64C 37/00

US Classification:

244 45R, 244 13, 244 2

Abstract:

An aircraft structure is provide, an aircraft structure for an aircraft. including front Wing and rear wing of the Swan-Wing, vertical winglets and the first level Floor body. the fuselage has a cross-section of substantially flat fuselage shape being is Wide enough to provide lifting force. the front wing of the Swan-Wing are Disposed horizontally in front portion of the fuselage. rear wings of the Swan-Wing are disposed horizontally in rear portion of the fuselage. the vertical winglets Are disposed at the top of the rear fuselage. the first level disposed fuel tank storages, a Plurality of landing gear bays, cockpit with control panels, various avionics and Cabin doors. The top of the rear fuselage disposed jet power plants, the fuselage provide lifting force And the wings provides steering force and lifting force the whole structure of an aircraft Comprises carbon fiber honey comb composite molded structure which lighter weight And shear strong structure. the cockpit and cabin disposed. front window, rear Window, side window and doors.

US Patent:

8500070, Aug 6, 2013

Filed:

Jun 10, 2009

Appl. No.:

12/456008

Inventors:

Sunstar Im - Lancaster CA, US

International Classification:

B64G 1/14

US Classification:

2441593, 2441589

Abstract:

The present invention relates to a spacecraft structure that comprises a flat-wide body center fuselage, right and left side arch-wings and rocket propulsion power plant compartments, wherein the arch-wing is anchored to the fuselage via a foldable hinge mechanism. The fuselage structure is constructed as a single solid structure body of the spacecraft. A top portion at the rear of fuselage comprises a jet propulsion power plant to provide thrust during take-off from the airport. Both the left and right side arch-wings are anchored to a front and a rear portion of the center fuselage structure. Both the front and rear wing portions enable spacecraft lift and superior maneuverability during flight. The spacecraft is air tight and water tight and includes floatation devices.

US Patent:

20100012773, Jan 21, 2010

Filed:

Jul 16, 2008

Appl. No.:

12/174516

Inventors:

Sunstar IM - Lancaster CA, US

International Classification:

B64C 1/00
B64C 39/12
B64D 11/00
B64C 3/22
B64C 1/22
B64C 25/10

US Classification:

244 36, 244 45 A, 244117 R, 2441185, 2441232, 2441181, 244102 R, 244119, 244 90 R

Abstract:

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 of substantially rectangular flat shape, being is wide enough to provide lifting force, and includes three levels separated by multi-partition structure. The front wings are disposed horizontally in front portions of the fuselage. The rear delta wings are disposed horizontally in rear portions of the fuselage. The vertical winglets are disposed at wingtips of the rear delta wings. The first level disposed at a bottom of the three levels includes a cargo bay and a plurality of landing gear bays. The second level disposed at a middle of the three levels includes fuel tank storages. The third level may comprise a top cockpit and a plurality of passenger cabins. The fuselage provides major portion of lifting force and the wings provides steering force.

US Patent:

20100163669, Jul 1, 2010

Filed:

Dec 29, 2008

Appl. No.:

12/317733

Inventors:

Sunstar Im - Lancaster CA, US

International Classification:

B64C 1/00
B64C 3/00
B64D 11/00
B64C 35/00
B64D 11/06
B64C 9/00
B64C 3/14
B64C 1/14
B64C 25/04
B64D 45/00

US Classification:

244 36, 244 45 R, 244119, 2441185, 244106, 2441186, 244 87, 244 35 R, 2441295, 244100 R, 2441292

Abstract:

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 of substantially a half circle fuselage shape. Being is wide enough to provide lifting force, and includes four levels separated by multi partition structure. The front wings are disposed horizontally in front portions of the fuselage. The rear small wings are disposed horizontally in rear portions of the fuselage. The vertical winglets are disposed at the wingtips of the rear small wings. The first level disposed at a bottom of the four levels includes a fuel tank storages and a plurality of landing gear bays. The second level disposed at a middle of the four levels includes cargo bay. The third level may comprise a top cockpit and a plurality of passenger cabins. The fuselage provides major portion of lifting force and the wings provides steering force, and lifting force. The fourth level may comprises a plurality of passenger cabins.

US Patent:

20110114792, May 19, 2011

Filed:

Nov 18, 2009

Appl. No.:

12/592031

Inventors:

Sunstar Im - Lancaster CA, US

International Classification:

B64G 1/00

US Classification:

2441581

Abstract:

Sky station structure comprises circle center core structure and circle outer Ring structure which comprises multi floor section levels.Major center core structure center elevator provide transportations from bottom Cockpit floor levels to top cockpit floor levels.First section levels of multi floors provide cockpit, control office, passenger Compartments, bed rooms, food service compartments, lavatory rooms, landing Pads, rope with winching machines and jet and rocket fuel tanks.Second section levels of multi floors provide center elevators, circle center Hangers, large circle outer ring hangers, jet and rocket power plants at outer Ring structures, inner docking and outer docking bays, multi robotic arms at Outer walls of docking bays,Third section levels of first floor levels provide center elevators, cylindrical Multi soft envelopes from floor levels to top levels of floors, cylindrical carbon Fiber honey comb composite outer envelopes from floor levels to top levels of Floors, multi envelopes of each envelope filled pressurized helium gas which Make it float at atmosphere.Third section levels of outer ring structure provide center post from floor to top Truss structure, cylindrical multi soft envelopes from floor levels to top of Truss structure, large cylindrical carbon fiber honey comb composite outer Envelopes from floor levels to top levels center truss structure, each envelope Floor zone need floor gate for repair and Inspection works.Fourth section levels comprises large circle outer truss structure, top of truss Bridge connected from center core structure to top of outer truss structure.Fifth section levels of top floor structure provide top cockpit and top control Tower.Also guy wire anchor at center of top control tower to top truss of outer Ring structures.