Flight Mode Transition Guidance for Electric Aircraft Pilots

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Solution Overview

Problem

Modern electric aircraft lack an apparatus to guide the transition between flight modes, making it difficult for pilots to control the aircraft smoothly during mode changes.

Innovation Solution

An apparatus comprising sensors to detect movement data and a flight controller that determines the current flight mode, generates guidance data, and communicates this information to a pilot indicator to assist in smooth transitions between flight modes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If an apparatus for guiding transition between flight modes is added to electric aircraft, then pilot control during mode changes is improved, but device complexity increases

Engineering Contradiction:
Improvepilot control during mode transitionsVSAvoidapparatus complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The flight controller is designed to perform multiple functions: it determines current flight mode based on movement data, generates guidance data for mode transitions, and communicates with the pilot indicator. This multi-functional approach integrates the guidance system into existing flight control infrastructure, providing transition guidance without requiring completely separate dedicated hardware, thereby improving ease of operation while limiting the increase in device complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The pilot indicator serves as an intermediary device that receives guidance data from the flight controller and presents it to the pilot in an understandable format. This intermediary translates complex flight control information into actionable guidance, improving pilot control during transitions without requiring the pilot to directly interface with the complex flight control system, thus resolving the contradiction between ease of operation and device complexity.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Loss of information

If real-time movement data and guidance data are provided to pilots, then flight planning and analytics are improved, but information processing requirements increase

Engineering Contradiction:
Improveflight information availabilityVSAvoidprocessing power requirements
Core Design Contradiction:
Loss of informationVSPower

Solution Approach 1:

The system extracts only the essential and relevant information from the full set of flight data for presentation to the pilot. The flight controller processes movement data to determine flight mode and generates guidance data that highlights critical transition information, rather than presenting all raw data. This extraction approach ensures pilots have access to necessary flight information for planning and analytics while minimizing the processing power required by focusing on key parameters.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The flight controller performs preliminary processing of movement data to determine current flight mode and generate appropriate guidance data before presenting it to the pilot. This preliminary action organizes and pre-processes information in advance, reducing the real-time processing burden during critical transition moments and ensuring that pilots receive pre-analyzed, actionable information rather than raw data requiring immediate processing.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS12332661B2Apparatus for guiding a transition between flight modes of an electric aircraft
Publication Date: 2025.06.17 BETA AIR LLC
  • US12332661B2 patent drawing
  • US12332661B2 patent drawing
  • US12332661B2 patent drawing

AI summary

An apparatus for guiding a transition between flight modes of an electric aircraft is illustrated. The apparatus comprises at least a sensor configured to detect a movement datum of the electric aircraft and a flight controller communicatively connected to the at least sensor, wherein the flight controller is configured to receive the movement datum from the at least a sensor, determine a current flight mode of the electric aircraft as a function of the movement datum, generate a guidance datum as a function of a change in flight mode and the movement datum, communicate the movement datum and the guidance datum to a pilot indicator in communication with the flight controller, and display the movement datum and the guidance datum using the pilot indicator.