CN-116946401-B - Rotary wing cabin and vehicle

CN116946401BCN 116946401 BCN116946401 BCN 116946401BCN-116946401-B

Abstract

The invention provides a rotor wing cabin and a vehicle. The rotor cabin comprises a cabin body, a first cabin door, a second cabin door and a rotor, wherein the cabin body is provided with a first cabin and a second cabin which are communicated. The first cabin door is assembled to the cabin body and can selectively open or close the first cabin, and the second cabin door is assembled to the cabin body and can selectively open or close the second cabin. The rotor is assembled in the cabin body and can be selectively in the storage state or the unfolding state, the rotor is stored in the cabin body from outside the cabin body through the first cabin to be in the storage state, so that the rotor is stored in the cabin body and is beneficial to avoiding interference to other vehicles, pedestrians and the like, and when the rotor is switched to the unfolding state from the storage state, the second cabin is driven to open the second cabin and protrude out of the cabin body from the second cabin, so that a vehicle can fly through the rotor.

Inventors

Ao Shangbing
NI QIANHONG
WU JINGANG
PENG DAN
ZHANG XI
GAO KAI
HUANG JINTENG
HE JINGANG
RAN XIANG
DAI SHILEI
LIU FENG
WU KAIFENG
ZHANG YIFEI
WANG BING

Assignees

广东汇天航空航天科技有限公司

Dates

Publication Date: 20260512
Application Date: 20220701
Priority Date: 20220412

Claims (11)

1. A rotor wing cabin, which comprises a main body, characterized by comprising the following steps: the cabin body is provided with a first cabin and a second cabin which are communicated with each other; a first door fitted to the cabin body and selectively openable or closable by the first cabin, and a second door fitted to the cabin body and selectively openable or closable by the second cabin; a rotor mounted to the housing and selectively in a stowed or deployed state, the rotor stowed in the housing from outside the housing through the first compartment to be in the stowed state, the rotor, when switched from the stowed to the deployed state, driving the second compartment to open and protrude from the second compartment outside the housing, movement of the rotor relative to the housing driving the compartment to selectively open or close the second compartment, and A processor, a hatch driver and a rotor driver, wherein the processor is respectively connected with the hatch driver and the rotor driver in a signal way, the hatch driver is used for driving the first hatch to selectively open or close the first hatch, and the rotor driver is used for driving the rotor to be selectively in the storage state or the unfolding state; The processor is used for outputting a door opening signal, and the door driver responds to the door opening signal and controls the first door to open the first cabin; The processor is further configured to output a rotor control signal, the rotor driver being responsive to the rotor control signal and controlling the rotor to be in a corresponding state, wherein the rotor control signal includes a rotor deployment signal and a rotor stowing signal, the rotor driver controlling the rotor to be in the deployed state according to the rotor deployment signal, the rotor driver controlling the rotor to be in the stowed state according to the rotor stowing signal; The processor is also configured to output a door closing signal, and the door driver is responsive to the door closing signal and controls the first door to close the first compartment.
2. The rotor module of claim 1, wherein the first door is hinged to the body, and the rotor module further comprises a telescoping actuator hinged between the body and the first door, wherein telescoping movement of the telescoping actuator rotates the first door relative to the body and selectively opens and closes the first compartment.
3. The rotor module of claim 1, further comprising a module door lock and a module door lock, the module door lock and the module door lock being selectively lockable and unlockable, one of the module door lock and the module door lock being mounted to the module body and the other being mounted to the first module door.
4. The rotor module of claim 1, wherein the second door is hinged to the module and slidably engages the rotor, and wherein the rotor is configured to move the second door to close the second chamber when the rotor is switched from the extended position to the stowed position.
5. The rotor module according to claim 4, wherein the second door includes a hinge portion and a sliding portion, the hinge portion being opposite the sliding portion, the hinge portion being hinged to the module body, the sliding portion being in sliding engagement with the rotor.
6. The rotor module of claim 5, further comprising a rail mounted to the rotor and a slider hinged to the slider and slidably disposed on the rail.
7. The rotor module of claim 4, further comprising an elastic return member mounted to the second door at the hinge of the second door to the body, the elastic return member adapted to provide the second door with an elastic force that rotates in the direction of the second compartment.
8. The rotor module of claim 7, wherein the rotor includes a wing arm and a propeller blade, the wing arm being hinged to the module, the propeller blade being rotatably mounted to the wing arm, and wherein the second door includes a ball head slidably abutting the wing arm.
9. The rotor module of claim 8, wherein the rotor further comprises a resilient pad coupled to the wing arm and abutting the bulb.
10. The rotor module according to claim 1, wherein the second door has a smaller volume than the first door and/or the second door has a hollowed-out structure.
11. Traffic system the tool is used for the treatment of the surface of the body, characterized by comprising the following steps: Fuselage, and The rotor blade compartment of any one of claims 1 to 10, the compartment body being fitted to the fuselage.

Description

Rotary wing cabin and vehicle Technical Field The invention relates to the technical field of vehicles, in particular to a rotor wing cabin and a vehicle. Background In related art vehicles, such as a aerocar, a flying structure is directly externally arranged outside a fuselage, so that the aerocar is easy to interfere with other vehicles, pedestrians and the like on a road surface in a land traveling process. Disclosure of Invention Embodiments of the present invention provide a rotor wing tank or vehicle to ameliorate at least one of the above problems. The embodiments of the present invention achieve the above object by the following technical means. In a first aspect, an embodiment of the present invention provides a rotor nacelle, where the rotor nacelle includes a nacelle body, a first door, a second door, and a rotor, and the nacelle body is provided with a first nacelle and a second nacelle that are in communication. The first cabin door is assembled to the cabin body and can selectively open or close the first cabin, and the second cabin door is assembled to the cabin body and can selectively open or close the second cabin. The rotor is assembled in the cabin body and can be selectively in a storage state or a unfolding state, the rotor is stored in the cabin body from outside the cabin body through the first cabin to be in the storage state, and when the rotor is switched from the storage state to the unfolding state, the rotor drives the second cabin door to open the second cabin and protrudes out of the cabin body from the second cabin. In some embodiments, the first door is hinged to the body, and the rotor wing cabin further comprises a telescopic actuator hinged between the body and the first door, wherein telescopic movement of the telescopic actuator drives the first door to rotate relative to the body and enables the first door to selectively open or close the first compartment. In some embodiments, the rotor wing nacelle further includes a nacelle door lock and a nacelle door lock, the nacelle door lock and the nacelle door lock being selectively lockable and unlockable, one of the nacelle door lock and the nacelle door lock being mounted to the nacelle body and the other being mounted to the first nacelle door. In some embodiments, the second door is hinged to the cabin and slidably cooperates with the rotor, and when the rotor is switched from the deployed state to the stowed state, the second door is brought to close the second cabin. In some embodiments, the second door includes a hinge portion opposite the slide portion, the hinge portion being hinged to the body and the slide portion being in sliding engagement with the rotor. In some embodiments, the rotor nacelle further includes a guide rail mounted to the rotor, and a slider hinged to the slider and slidably disposed on the guide rail. In some embodiments, the rotor nacelle further comprises an elastic return member mounted at the hinge of the second nacelle door and the nacelle body, the elastic return member being adapted to provide the second nacelle door with an elastic force that rotates in the direction of the second nacelle. In some embodiments, the rotor includes a wing arm hinged to the nacelle and a propeller blade rotatably mounted to the wing arm, and the second door includes a ball head slidably abutting the wing arm. In some embodiments, the rotor further comprises an elastic pad connected to the wing arm and abutting the ball head. In some embodiments, the second door has a smaller volume than the first door and/or the second door is hollow. In some embodiments, movement of the rotor relative to the nacelle causes the second door to selectively open or close the second compartment. The rotary wing cabin further comprises a processor, a cabin door driver and a rotor driver, wherein the processor is respectively connected with the cabin door driver and the rotor driver in a signal mode, the cabin door driver is used for driving the first cabin door to selectively open or close the first cabin, and the rotor driver is used for driving the rotor to be selectively in a storage state or an unfolding state. The processor is used for outputting a door opening signal, and the door driver responds to the door opening signal and controls the first door to open the first cabin. The processor is further configured to output a rotor control signal, the rotor driver is responsive to the rotor control signal and controls the rotor to be in a corresponding state, wherein the rotor control signal includes a rotor deployment signal and a rotor stowing signal, the rotor driver controls the rotor to be in a deployed state according to the rotor deployment signal, and the rotor driver controls the rotor to be in a stowed state according to the rotor stowing signal. The processor is also configured to output a door closing signal, and the door driver is responsive to the door closing signal and controls the first door to close the firs