Airplane Docking Identification via Transmitted Signal Feedback

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Solution Overview

Problem

Current systems for guiding airplanes to dock with passenger bridges often rely on incorrect or outdated data about airplane type and version, leading to potential accidents due to misalignment of wings or doors, as the data in central computer systems is not always accurate.

Innovation Solution

A method that uses an antenna to receive information from airplanes, extracts the identification number and coordinates, and retrieves the correct airplane type and version from a database to accurately display this information to the pilot, ensuring correct alignment and safe docking by controlling the display and distance measuring devices.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If distance measuring lasers and displays are used to guide airplane docking, then the positioning accuracy is improved, but the reliability deteriorates due to incorrect airplane type data in central computer systems

Engineering Contradiction:
Improvepositioning accuracyVSAvoiddocking safety
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent implements feedback by having the display show the actual airplane type and version detected from transmitted information, allowing verification against the expected type. This feedback loop enables the system to identify and correct data errors, ensuring the docking process uses accurate airplane type information rather than relying solely on potentially incorrect central computer system data.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system performs self-verification by automatically receiving and processing transmitted information containing airplane identification data. The local system independently verifies the airplane type against the database and displays it for confirmation, eliminating reliance on external manual input or potentially erroneous central system data, thus improving both reliability and measurement precision.

Inventive Principle:
Principle #25Self-service

2Ease of operation

If the display shows expected airplane type from central computer system, then the docking process is simplified, but the accuracy of airplane type identification deteriorates due to data errors

Engineering Contradiction:
Improvedocking process simplicityVSAvoidairplane type identification accuracy
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The system performs preliminary verification by receiving and displaying the actual airplane type information before the docking process begins. This allows operators to verify the correct airplane type is identified and take corrective action if discrepancies are found, ensuring accurate identification while maintaining operational simplicity through automated preprocessing and display of verified data.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

By displaying the actually detected airplane type and version from transmitted information rather than only expected types, the system provides feedback that enables verification of data accuracy. This feedback mechanism maintains operational simplicity while dramatically improving identification accuracy by allowing real-time verification against actual airplane characteristics.

Inventive Principle:
Principle #23Feedback

3Adaptability or versatility

If manual input of airplane data is allowed, then the system is more flexible, but the reliability deteriorates due to risk of incorrect data input

Engineering Contradiction:
Improvesystem flexibilityVSAvoiddata accuracy
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The system automatically receives and processes airplane identification data through transmitted information containing identification numbers and coordinates, eliminating the need for manual data input. This self-service approach maintains system flexibility by automatically adapting to different airplanes while dramatically improving reliability by removing human error from the data entry process.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The patent replaces manual mechanical data input with automated electronic reception of transmitted information. The antenna receives signals containing airplane identification data, which is then automatically processed and displayed. This substitution eliminates manual input errors while maintaining system adaptability through automated data extraction and verification processes.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This method ensures accurate identification and positioning of airplanes, reducing the risk of accidents by providing real-time, correct information about the airplane type and version, and guiding the passenger bridge to connect safely and securely to the airplane door.

Implementation Method 1

an antenna is caused to receive information transmitted by an airplane

Methodology Applied
Scientific EffectElectromagnetic radiation reception: Electromagnetic Induction

Implementation Method 2

The technology which nowadays is most often used to measure the distance is distance measuring lasers

Methodology Applied
Scientific EffectLaser distance measurement: LIDAR

Data Source

PatentUS8942915B2Method for identifying an airplane in connection with parking of the airplane at a stand
Publication Date: 2015.01.27 THYSSENKRUPP AIRPORT SYST
  • US8942915B2 patent drawing
  • US8942915B2 patent drawing
  • US8942915B2 patent drawing

AI summary

Method for identifying an airplane in connection to parking of the airplane at a gate or a stand, for possible connection of a passenger bridge (1) or a loading bridge to a door of an airplane, where the airplane is positioned and stopped at a predetermined position using a touchless measurement of the distance between the airplane and a fixed point, where the distance is indicated on a display (6) mounted in front of the pilot of the airplane on for instance an airport building (7), which display (6) shows the position of the airplane (5) in relation to a stop point for the airplane and shows the current airplane type, where the distance measurement and display are caused to be activated by a computer system (20) belonging to the airport or manually, and wherein an antenna (16) is caused to receive information (17) transmitted by an airplane.