IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0955137
(2010-11-29)
|
등록번호 |
US-8528852
(2013-09-10)
|
우선권정보 |
DE-10 2009 056 137 (2009-11-27) |
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
7 인용 특허 :
5 |
초록
A vehicle suitable as both a road vehicle and an aircraft, which includes two units that can be coupled to one another; a first unit embodies a road vehicle with least single-file seating, and a second unit is embodied as a flight unit.
대표청구항
▼
1. A vehicle, suitable as both a road vehicle and an aircraft, comprising two units that can be coupled to one another, in which a first unit is embodied as a road vehicle (1) with at least single-file seating having only two wheels arranged along a single longitudinal axis of the road vehicle, and
1. A vehicle, suitable as both a road vehicle and an aircraft, comprising two units that can be coupled to one another, in which a first unit is embodied as a road vehicle (1) with at least single-file seating having only two wheels arranged along a single longitudinal axis of the road vehicle, and a second unit is embodied as a flight unit (25), wherein road vehicle (1) has a cockpit (2), the cockpit having sides which encloses and surrounds the road vehicle (1), and a floor,wherein the cockpit (2) has a first opening (14) in the floor, a closure flap (13) is disposed so as to be displaceable in the longitudinal direction of the road vehicle (1) to selectively open and close the opening, andwherein in response to the road vehicle dropping below a certain moving speed, the closure flap (13) is movable abruptly under spring load into an open position to permit stabilization of the road vehicle while in a stopped position. 2. The vehicle as defined by claim 1, wherein the road vehicle (1) is assigned its own drive motor (12), and the flight unit (25) is also assigned its own drive motor (35). 3. The vehicle as defined by claim 1, wherein the cockpit (2) has at least one opening (6) for boarding and disembarking, or is to be opened in its entirety. 4. The vehicle as defined by claim 1, wherein the flight unit (25) comprises at least the following parts: a load-bearing surface (30) or rotor, a main landing gear (32), a flight drive mechanism (35), and at least one tail assembly (40, 41). 5. The vehicle as defined by claim 1, wherein the flight unit (25) has a coupling apparatus (26) on a front free end and can be coupled to certain parts of the road vehicle (1). 6. The vehicle as defined by claim 1, wherein the flight unit (25) has a front coupling apparatus (26), which comprises two parallel coupling horns (27), and the coupling horns (27) form coupling faces (18) on the underside of the cockpit (2). 7. The vehicle as defined by claim 1, wherein on the back end of the cockpit (2), a coupling face (19) is embodied with two opposed couplings (43), and one coupling part is disposed on the road vehicle (1) and one coupling part is disposed on a motor part (34). 8. The vehicle as defined by claim 5, wherein the coupling apparatus (26) can be pivoted into the cockpit (2) through a second opening (42) in the floor of the cockpit. 9. The vehicle as defined by claim 1, wherein the flight unit (25) has its own flight drive mechanism (35), such as an internal combustion engine, a rotary piston engine, a jet turbine, or a turboprop drive. 10. The vehicle as defined by claim 9, wherein the flight drive mechanism (35) of the coupled flight unit (25) drives either an airscrew (36), a rotor blade (46, 47), or at least one rotor (48, 49). 11. The vehicle as defined by claim 6, wherein a throttle (29) and a control stick (28) are disposed on the upper side of the coupling apparatus (26), and on coupling to the road vehicle (1), these control elements (28, 29) protrude into the passenger compartment (2). 12. The vehicle as defined by claim 1, wherein the flight unit (25) is capable of flight only in combination with the first unit (1). 13. The vehicle as defined by claim 1, further comprising a sensor operatively connected to the closure flap to automatically move the closure flap into the open position as a function of the travel situation of the road vehicle. 14. The vehicle as defined by claim 1, further comprising a mechanical bracing element configured to be selectively raised and lowered through the opening in the cockpit to protect the road vehicle from tipping over.
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