Configuration-Sensitive Aircraft Range Rings for Emergency Landing

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Solution Overview

Problem

Existing aircraft range determination systems do not accurately account for various aircraft conditions and configurations, particularly in emergency situations, leading to potential overshooting or undershooting of landing targets.

Innovation Solution

A system and method for generating and displaying range rings on an aircraft's display device, which considers user-defined and sensor-collected data to calculate and visualize the aircraft's range based on multiple conditions and configurations, including landing gear, wing flaps, speed brakes, and engine thrust, providing accurate range estimation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional range determination systems are used, then the system is simple, but the range determination accuracy deteriorates because it does not accurately account for various aircraft conditions and configurations

Engineering Contradiction:
Improverange determination accuracyVSAvoidsystem complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system segments the range determination process by creating multiple independent range rings, each representing a specific aircraft configuration or condition. Each range ring is calculated separately based on specific parameters (fuel reserves, airspeed, altitude, landing gear position, wing flap position), allowing the system to handle complex variations in aircraft state without overwhelming complexity in a single monolithic calculation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system dynamically adjusts the range rings based on real-time or selected aircraft configurations. By making the range determination adaptive to different operating conditions (clean configuration, landing gear down, wing flaps extended), the system maintains high accuracy across varying scenarios without requiring a completely complex recalibration of the entire system.

Inventive Principle:
Principle #15Dynamics

2Measurement precision

If multiple aircraft configurations are considered, then the range determination accuracy improves, but the ease of operation deteriorates due to multiple input requirements

Engineering Contradiction:
Improverange determination accuracyVSAvoiduser input complexity
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The system makes the display device multi-functional by enabling it to serve both as a traditional display and as an interactive configuration selector. The same display device that shows range rings also accepts user inputs for different aircraft configurations, eliminating the need for separate control interfaces and maintaining ease of operation while improving accuracy.

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

Solution Approach 2:

The system prepares multiple pre-defined aircraft configurations in advance (clean configuration, landing gear down, wing flaps extended) so that users can select from predetermined options rather than entering complex parameters manually. This preliminary preparation of configuration options maintains ease of operation while enabling accurate range determination across multiple scenarios.

Inventive Principle:
Principle #10Preliminary action

3Loss of information

If range rings are displayed for multiple conditions, then the information completeness improves, but the display complexity increases

Engineering Contradiction:
Improveinformation completenessVSAvoiddisplay complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The display device segments the information presentation by displaying multiple range rings, where each ring represents a specific aircraft configuration or condition. This segmentation allows the system to present comprehensive information about range under different scenarios without creating a single overwhelming complex display, as each ring is a distinct, easily interpretable visual element.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS20250282488A1Configuration sensitive range rings and glide rings
Publication Date: 2025.09.11 HAMILTON SUNDSTRAND CORP
  • US20250282488A1 patent drawing
  • US20250282488A1 patent drawing
  • US20250282488A1 patent drawing

AI summary

A system for generating and displaying one or more range rings on an aircraft includes a processor, a display device, a communication device, and computer-readable memory. The display device contains a user interface. In operation, the system receives a user configuration input via the user interface of the display device. The system receives aircraft data from a connected aircraft avionics system via the communication device. The system calculates one or more ranges of the aircraft based upon the user configuration input and/or the aircraft data. The system generates one or more range rings based upon the one or more ranges of the aircraft, wherein the one or more range rings are visual depictions of the one or more ranges of the aircraft. The system displays the one or more range rings on the display device.