子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | TRANSFORMATION METHOD OF HYBRID TRANSPORTATION VEHICLE FOR GROUND AND AIR, AND HYBRID TRANSPORTATION VEHICLE ITSELF | US14241239 | 2012-08-22 | US20150028150A1 | 2015-01-29 | Stefan Klein |
| Transformation method of hybrid transportation vehicle for ground and air includes the following transformation and reciprocal steps: Tilting the compensation cover (7) on. Expansion of both whole wings (1) from the transportation vehicle longitudinal position around two vertical axes (2) into the flying position. Expansion of rear parts of wings (1) from the top front parts of wings (1) into the spread flying position by tilting the rear of each wing (1) around a horizontal axis (3). The take-off and landing tilting of wings (1) by an angle of attack alpha=0 to 40° of the wings onset. Front wheels track (5) is reduced by axially shifting the front wheels (5) towards the fuselage. Furthermore, a corresponding hybrid transportation vehicle for ground and air is described which contains reciprocal transformation mechanisms for transformation from a sterling double or four-track automobile into a sterling aircraft for take-off and landing on the ground or water, and vice versa. | ||||||
| 42 | AIRCRAFT WITH A PRESSURIZED VESSEL | US12368559 | 2009-02-10 | US20100200689A1 | 2010-08-12 | Robert Erik Grip |
| An aircraft comprising a fuselage, a vessel associated with the fuselage, a propulsion system associated with the fuselage, and a lift system. The vessel is capable of storing a pressurized gas compressed to a density that allows the aircraft to operate under water. The lift system is capable of providing the aircraft lift to fly in air. | ||||||
| 43 | All-terrain amphibious vehicle | US26692 | 1979-04-03 | US4274502A | 1981-06-23 | Michael Somerton-Rayner |
| An automotive vehicle is provided, for use inter alia as a mobile anti-tank guided missile-firing platform, which is sufficiently inexpensive to be expendable in battle and can be readily carried by a helicopter. The vehicle has a main frame comprising a pair of longitudinal closed box section members joined to form a ladder construction by a cross member and having strong points for the mounting of an engine and gearbox. The ground wheels, which lean outwards by about 5 degrees, are mounted on stub axles journalled in the box section members and are all driven by chains housed in oil baths within the box section members. Steering is accomplished by braking the transmission on one side or the other. The wheel tires are low pressure raw hide tires. The closed box section members project below the body of the vehicle and have toboggan-shaped ends to act as runners in snow. The body of the vehicle is constructed as a waterproof box to give buoyancy. The front and back wheels are higher on the frame than the center wheels. | ||||||
| 44 | Small, personal, all terrain vehicle | US686592 | 1976-05-14 | US4072203A | 1978-02-07 | Neil W. Pierson |
| A small, personal, all terrain vehicle is disclosed of the articulated, multi-unit type. A first and second unit, having track members pivotably mounted thereto, are also pivotably and rotatably interconnected to each other. A motor is provided in the second unit for driving the track members of the first and second units. The first unit includes a seat for a driver and a steering mechanism causing the pivoting of the second unit with respect to the first unit. The all terrain vehicle is of a small size, in the preferred embodiment being four feet wide and eight feet long, for the personal transportation of the driver. The all terrain vehicle provides advantageous weight distribution in that the weight of the driver of the all terrain vehicle is located in the first unit to provide substantial traction to the track members of the first unit and the weight of the motor is located in the second unit to provide substantial traction to the track members of the second unit. The interconnection of the first and second units and the pivotable interconnection of the track members to the first and second units assure that all four track members engage the travel surface. | ||||||
| 45 | Rigid chassis for air transportable vehicle | US529510 | 1974-12-04 | US3992027A | 1976-11-16 | Paul Etienne Rene Legueu |
| The main frame rails of an automotive vehicle are offset at the rear spring mount of the front suspension. This divides them into two portions at different levels, the forward portion being higher than the rear portion. | ||||||
| 46 | Foldable transportation device | US3700057D | 1971-05-03 | US3700057A | 1972-10-24 | BOYD LOYCE M; BOYD CLARENCE L |
| A foldable transportation device having the component parts thereof movable between a folded storage position and an extended in-use position for travel is disclosed and includes a center frame having a plurality of telescopeable sections and a body including floor and end and side wall members mounted thereon and movable therewith between respective folded positions and extended in-use positions and a pair of opposed arms for each end of the center frame each having one end thereof pivotally mounted on the respective side of the center frame and each having a wheel rotatably mounted on the other end thereof with each arm being movable between a folded storage position and an in-use position for movably supporting the transportation device. Drive means and steering means are operatively connected to selected wheels for controlling movement and travel of the transportation device.
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| 47 | Collapsible automotive vehicle | US28100363 | 1963-05-16 | US3254734A | 1966-06-07 | GEORG BEHRMANN |
| 48 | Automatic clutch with speed responsive pilot clutch | US7425160 | 1960-12-07 | US3160252A | 1964-12-08 | GUSTAV STEINLEIN |
| 49 | Collapsible road vehicle | US75665858 | 1958-08-22 | US2975850A | 1961-03-21 | VERNON DOLPHIN JOHN ROBERT |
| 50 | Folding motor vehicle for aircraft | US77619647 | 1947-09-26 | US2536749A | 1951-01-02 | RICHARD JENNER RAY; MITCHELL DONALD H |
| 51 | Military vehicle body | US41412341 | 1941-10-08 | US2278450A | 1942-04-07 | JONES BYRON Q |
| 52 | 다축 다단계 틸트 멀티 로터 플라잉 카 | KR1020120134690 | 2012-11-26 | KR101386959B1 | 2014-04-29 | 윤광준 |
| The flying car according to the present invention includes a main frame having a square shape outside and a grid structure inside; a main body mounted at the center of the main frame with regard to balance; multiple rotors on the upper part of the main frame; multiple wheels on the lower part of the main frame, main body wings on the two side of the main body; and an auto driving control unit on the main body to control the rotors and wheels. The flying car according to the present invention is three times faster, flies three times longer, and flies five times farther than a rotor flying body such as a helicopter when the flying car does only necessary vertical taking off and landing with limited space and switches to the fixed wing mode for normal flying. | ||||||
| 53 | 공기역학 및 운송 특징들을 완전하게 증가시키기 위한 방법, 상기 방법（변형들)을 실행하기 위한 위그선 및 비행을 실현하기 위한 방법 | KR1020117018172 | 2010-01-05 | KR1020110112402A | 2011-10-12 | 노비코브-코프,이반 |
| 발명들의 그룹은 (정적 및 동적) 공기 배출을 갖는 항공기 및 운송 수단에 관한 것이며, 특히 타입들 A, B 및 C의 자체 안정화 위그선에 관한 것이다. 이하의 기술적인 결과들이 얻어진다 : 증가된 비행 안전성 및 조종 안전성, 증가된 로드-베어링 능력 및 지면 효과 모드에서의 비행 높이 증가, 감소된 치수들, 개선된 이륙 및 랜딩 특징들, 수륙 양용 특성 및 경제적 효율성, 증가된 기능성 및 넓은 범위의 작동 배열들, 및 사용 및 정비의 커다란 용이성이 얻어진다. 이 결과는 공기력의 시스템을 발생시키기 위한 방법들, 구조적 해결책들 및 "비행 날개" 또는 "합성 날개" 설계 레이아웃들에 대해 발명들의 현 그룹에서 제안한 것과 개념적으로 링크된 조종 방법들을 동시에 적용함에 의해 얻어지게 된다.
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| 54 | 지상 및 공중에서 사용하기 위한 하이브리드 수송용 운송 수단의 변형 방법 및 하이브리드 수송용 운송 수단 | KR1020147008064 | 2012-08-22 | KR1020140077157A | 2014-06-23 | 클라인스테판 |
| 지상 및 공중에서 사용하기 위한 하이브리드 수송용 운송 수단의 변형 방법은 이하의 변형 및 상호 단계를 포함한다. 보상 커버(7)를 틸팅 온(tilting on)하는 단계. 수송용 운송 수단의 종방향 위치로부터 2개의 수직방향 축선을 중심으로 비행 위치로 양 날개(1) 전체를 확장하는 단계. 수평방향 축선(3)을 중심으로 한 각각의 날개(1)의 후방부의 틸팅에 의해 날개(1)의 후방부를 날개(1)의 상부 전방 부분으로부터 전개된 비행 위치로 확장하는 단계. 날개 시작부의 0 내지 40 도의 영각(α)만큼 날개(1)의 이륙 틸팅 및 착륙 틸딩을 행하는 단계. 동체를 향해 전방 휠(5)을 축방향으로 시프트함으로써 전방 휠(5) 트랙을 축소시키는 단계. 더욱이, 지상 및 공중에서 사용하기 위한 대응하는 하이브리드 수송용 운송 수단으로서, 지상 또는 물에서의 이륙 및 착륙을 위해 스털링 이중 트랙 또는 포 트랙 자동차로부터 스털링 항공기로 변형하기 위한 그리고 이와 반대로 변형하기 위한 상호 변형 메커니즘들을 포함하는 하이브리드 수송용 운송 수단이 설명된다.
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| 55 | 지면 및 공중과 수면을 기동하는 방법 및 그 장치 | KR1020110058763 | 2011-06-16 | KR1020120139139A | 2012-12-27 | 김준규 |
| PURPOSE: A method and a device of driving on surface, air and under water are provided to freely driving in air space and under water. CONSTITUTION: A device of driving on surface, air and under water comprises a center car body(10), a front wing frame(20), a rear wing frame(30), and a rudder unit(40). The center car body comprises a streamline frame unit, a power unit(12), and a propeller(14). The power unit is coupled at the upper end on the front surface of a wire frame. The propeller is connected to a rotation center shaft(13) of the power unit. The rear wing frame includes a rear wheel shaft and a rear wheel device(32). | ||||||
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