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Display and control system for cockpit of electric vertical take-off and landing aircraft

A vertical take-off and landing aircraft, control system technology, applied to aircraft parts, transportation and packaging, etc., to achieve the effect of convenient manipulation

Pending Publication Date: 2022-07-29
上海沃兰特航空技术有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, current aircraft mainly include helicopters and fixed-wing aircraft, and the existing cockpit display and control systems are also aimed at helicopters and fixed-wing aircraft. Cockpit display and control system

Method used

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  • Display and control system for cockpit of electric vertical take-off and landing aircraft
  • Display and control system for cockpit of electric vertical take-off and landing aircraft
  • Display and control system for cockpit of electric vertical take-off and landing aircraft

Examples

Experimental program
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Embodiment

[0027] The electric vertical take-off and landing aircraft includes an electric rotor motor, an electric thrust motor and a fixed-wing aerodynamic shape. The electric rotor motor provides the aircraft with vertical lift for vertical take-off and landing, and the electric thrust motor provides the aircraft with forward flying power in the fixed-wing flight mode, such as Figure 1-Figure 3 As shown, the present invention provides an electric vertical take-off and landing aircraft cockpit display and control system, which provides a man-machine interface for the pilot and the aircraft, and specifically includes a front instrument panel area, a side console area, a central console area and a seat;

[0028] The front instrument area includes integrated integrated display module, communication / audio control panel, spare instrumentation, cockpit recorder panel, AP control panel, key system control panel and cabin integrated management display panel, communication / audio control panel, s...

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PUM

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Abstract

The invention discloses an electric vertical take-off and landing aircraft cockpit display and control system which comprises a front instrument desk area, a side console area, a central console area and seats. The front instrument area comprises an integrated comprehensive display module, a communication / audio control panel, a standby instrument, a cockpit recorder panel, an AP control panel, a key system control panel and a passenger cabin comprehensive management display panel. The communication / audio control panel, the standby instrument, the cockpit recorder panel, the AP control panel, the key system control panel and the passenger cabin comprehensive management display panel are connected with the integrated comprehensive display module and distributed around the integrated comprehensive display module, and the integrated comprehensive display module is connected into the triple-redundancy aircraft computer FCC through three buses in a redundancy mode. According to the cockpit display and control system, manipulation and display are designed for the electric vertical take-off and landing aircraft, the space position of cockpit equipment is arranged according to the characteristics of a single pilot, and manipulation of the electric vertical take-off and landing aircraft by a flight crew is facilitated.

Description

technical field [0001] The invention relates to the technical field of aviation equipment, in particular to a cockpit display and control system for an electric vertical take-off and landing aircraft. Background technique [0002] Electric vertical take-off and landing aircraft are expected to be used in urban air traffic to solve the problem of increasingly serious urban traffic congestion in the future. The electric vertical take-off and landing aircraft is driven by pure electric power, and realizes vertical take-off and landing through a lifting rotor motor, and has both fixed wings and thrust. achieve long-distance flight. The cockpit display and control system, as the man-machine interface between the pilot and the aircraft, generally includes the main flight display, multi-function display, joystick and control panel, etc., and is the basis for the use of electric vertical take-off and landing aircraft. However, the current aircraft mainly include helicopters and fix...

Claims

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Application Information

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IPC IPC(8): B64D43/00
CPCB64D43/00
Inventor 高小龙何皇冕党铁红董明
Owner 上海沃兰特航空技术有限责任公司
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