Aircraft Information Transmission System Using Vibration Feedback

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Solution Overview

Problem

Pilots face a high workload due to the need to rapidly process and react to various changing information inputs while operating an aircraft, which can lead to increased stress and decreased efficiency in decision-making.

Innovation Solution

An information transmission system that determines relevant information for pilots using a combination of visual, auditory, and vibrational outputs, categorizing messages as emergency, caution, or report to prioritize and simplify information delivery, utilizing vibrating devices strategically placed within the cockpit to enhance alertness and focus.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If multiple information channels (visual, auditory) are used to transmit information to the pilot, then the completeness and priority of information transmission is improved, but the complexity of the transmission system increases

Engineering Contradiction:
Improveinformation transmission completenessVSAvoidtransmission system complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The information transmission system is segmented into multiple independent channels (visual display, auditory output, vibration feedback) that can operate simultaneously. Each channel handles specific types of information or priority levels, allowing comprehensive information delivery without requiring a single complex integrated system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The control unit serves multiple functions by managing both visual display output and auditory/vibration output channels. This multi-functional approach allows a single control unit to coordinate multiple transmission channels, reducing overall system complexity while maintaining information completeness.

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

2Ease of operation

If vibration feedback is added to the information transmission system, then pilot alertness and information perception are improved, but the device complexity and number of components increase

Engineering Contradiction:
Improvepilot information perceptionVSAvoidnumber of vibrating devices
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

Vibration feedback is applied locally at specific contact points between the pilot and aircraft controls (control stick, throttle lever, rudder pedal) rather than throughout the entire cockpit. This targeted approach enhances information perception where the pilot naturally interacts with the aircraft, minimizing the number of vibrating devices needed.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The control stick, throttle lever, and rudder pedal serve as intermediary elements that transmit vibration feedback from the vibrating devices to the pilot's hands and feet. These existing control surfaces act as natural mediators, eliminating the need for separate feedback mechanisms and reducing overall system complexity.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If information is transmitted through multiple modalities (visual, auditory, vibration), then the reliability of information delivery is improved, but the energy consumption increases

Engineering Contradiction:
Improveinformation delivery reliabilityVSAvoidenergy consumption of transmission system
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The system uses periodic or intermittent vibration feedback rather than continuous operation. Vibration is activated only when specific information needs to be conveyed to the pilot, and the duration/intensity can be varied based on information priority. This periodic activation maintains reliable information delivery while significantly reducing energy consumption compared to continuous multi-modal transmission.

Inventive Principle:
Principle #19Periodic action

Data Source

PatentUS10407161B2Information transmission system, information transmission method, and aircraft
Publication Date: 2019.09.10 SUBARU CORP
  • US10407161B2 patent drawing
  • US10407161B2 patent drawing
  • US10407161B2 patent drawing

AI summary

According to one implementation, an information transmission system includes: a transmission information determination part, an output device; and at least one vibrating device. The transmission information determination part is adapted to determine transmission information to a pilot of an aircraft. The output device is adapted to transmit the transmission information to the pilot by a visual representation, voice, sound or a light. The at least one vibrating device is adapted to propagate a vibration to the pilot when the transmission information is transmitted to the pilot.