Cockpit PCA Indicator Box for APU Fuel Reduction

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Solution Overview

Problem

Pilots often fail to turn off the aircraft's auxiliary power unit (APU) unnecessarily due to a lack of convenient information about the status of the preconditioned air unit (PCA) supply, leading to increased fuel costs and pollution.

Innovation Solution

An electrically controlled PCA indicator box is mounted at the gate, visible from the cockpit, with distinct appearances indicating whether the PCA unit is operating or not, ensuring pilots can easily determine if the PCA is connected, thereby prompting them to shut off the APU when PCA is available.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If the pilot leaves the cockpit to check the PCA connection status, then the pilot can verify the PCA status, but the pilot is no longer at the cockpit controls for the APU

Engineering Contradiction:
ImprovePCA status informationVSAvoidCockpit control accessibility
Core Design Contradiction:
Loss of informationVSEase of operation

Solution Approach 1:

An intermediary indicator box is installed at the gate to mediate the information transfer between the PCA unit and the pilot. The indicator box displays the PCA operational status visually, allowing the pilot to obtain information without leaving the cockpit. This resolves the contradiction by providing a remote information display that eliminates the need for the pilot to physically check the PCA connection or leave the cockpit controls.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If the APU is run continuously to ensure power availability, then the aircraft remains ready for operation, but fuel consumption and pollution increase

Engineering Contradiction:
ImproveAircraft power readinessVSAvoidFuel consumption
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The indicator box provides real-time feedback to the pilot about the PCA unit's operational status. When the PCA is successfully connected and operating, the indicator displays this information, enabling the pilot to receive feedback and turn off the APU. This feedback mechanism resolves the contradiction by allowing the pilot to make informed decisions about APU operation based on actual PCA availability, thereby reducing unnecessary fuel consumption while maintaining aircraft readiness.

Inventive Principle:
Principle #23Feedback

3Loss of energy

If the pilot turns off the APU when PCA is available, then fuel costs and pollution are reduced, but the pilot needs reliable information about PCA connection status

Engineering Contradiction:
ImproveFuel consumptionVSAvoidPCA connection status
Core Design Contradiction:
Loss of energyVSLoss of information

Solution Approach 1:

The indicator box serves as an intermediary that provides reliable PCA connection status information to the pilot. By displaying the operational status of the PCA unit, the indicator box eliminates information loss and enables the pilot to make accurate decisions about turning off the APU. This resolves the contradiction by ensuring the pilot has access to accurate real-time information about PCA availability, thereby reducing fuel consumption without compromising decision-making reliability.

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS8174396B1Communication system from airport gate to cockpit
Publication Date: 2012.05.08 TWIST INC
  • US8174396B1 patent drawing
  • US8174396B1 patent drawing
  • US8174396B1 patent drawing

AI summary

An apparatus for visually communicating to a pilot in the cockpit of a parked aircraft the status of a preconditioned air (PCA) unit associated with the gate has an electrically controlled PCA indicator box positioned so that it is visible to the pilot in the cockpit. The PCA indicator box has a first appearance when the preconditioned air unit is not operating and a second appearance when the preconditioned air unit is operating. A method of assisting aircraft operators to reduce fuel costs and emissions of an aircraft parked at a gate includes mounting to the gate an electrical PCA indicator and electrically coupling it to a preconditioned air unit at the gate.