Electric vertical take-off and landing aircraft with separable lift component

A technology of vertical take-off and landing and aircraft, which is applied in the direction of vertical take-off and landing aircraft, aircraft, parachutes, etc., to achieve high safety margin and realize the effect of safe landing

Inactive Publication Date: 2021-07-09
CHINA HELICOPTER RES & DEV INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

At present, there is no relevant technical solution disclosed in the prior art

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  • Electric vertical take-off and landing aircraft with separable lift component
  • Electric vertical take-off and landing aircraft with separable lift component
  • Electric vertical take-off and landing aircraft with separable lift component

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Embodiment Construction

[0023] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0024] like figure 1 As shown, an electric vertical take-off and landing aircraft with detachable lift components is characterized in that it includes a lift component 100, a suspension cockpit 200, and an undercarriage 300. The lift component 100 is above the suspension cockpit 200, and the The suspended cockpit 200 is connected with a lock; the landing gear 300 is under the suspended cockpit 200 and is fixedly connected with the suspended coc...

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Abstract

The invention belongs to the technical field of vertical take-off and landing aircrafts and relates to an electric vertical take-off and landing aircraft with a separable lift component. The electric vertical take-off and landing aircraft comprises the lift component (100), a hanging cabin (200) and an undercarriage (300); the lift component (100) is arranged above the hanging cabin (200) and is connected with the hanging cabin (200) through a lock; the undercarriage (300) is arranged below the hanging cabin (200) and is fixedly connected with the hanging cabin (200); when the hanging cabin (200) is in a distress emergency state, the lock connection between the hanging cabin (200) and the lift component (100) is disconnected, and meanwhile the hanging cabin (200) is opened through triggering. The electric vertical take-off and landing aircraft with the separable lift component has higher safety margin. the lift component can be separated in the air, and safe landing can be achieved even under the condition of power failure.

Description

technical field [0001] The invention relates to a vertical take-off and landing aircraft, in particular to an electric vertical take-off and landing aircraft with separable lift components. Background technique [0002] In recent years, with the continuous development of urban air vehicle configurations, electric vertical take-off and landing aircraft has received more and more attention. Manned safety is the minimum requirement for urban low-altitude opening, and it is also an important factor that must be considered in the design of electric vertical take-off and landing aircraft. [0003] Even in the case of power failure, traditional helicopters can also manipulate the rotor mechanism to perform autorotation and glide to achieve a safe landing. However, the electric vertical take-off and landing aircraft is driven by pure electricity, and the lift components do not have a control mechanism, and all are controlled by wire. In the air, once their power fails, it is extre...

Claims

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Application Information

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IPC IPC(8): B64C29/00B64C1/32B64D17/72B64D17/78
CPCB64C1/32B64C29/00B64D17/72B64D17/78
Inventor 徐茂陈国军高志武王乐刘威
Owner CHINA HELICOPTER RES & DEV INST
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