Adjustable Landing Supports for Uneven Terrain

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional landing supports for vertical takeoff and landing aircraft are not capable of safely landing on uneven terrain, limiting their utility and posing risks to the aircraft and its crew and cargo.

Innovation Solution

A system that includes terrain sensors and attitude sensors to detect uneven terrain characteristics, with landing supports that can be adjusted in length or pressure to level the aircraft upon landing, and a support control device to configure the landing supports based on terrain and load characteristics, ensuring safe and stable landing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If rigid fixed landing supports are used, then the structure is simple and reliable, but the aircraft cannot safely land on uneven terrain

Engineering Contradiction:
Improvelanding safetyVSAvoidterrain adaptability
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The landing supports transition from fixed rigid structures to dynamically adjustable systems that can change their configuration (extend, retract, inflate, or adjust length) based on detected terrain characteristics, enabling the aircraft to adapt to uneven surfaces while maintaining structural reliability

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes physical parameters of the landing supports (such as length, pressure, or extension state) in response to terrain conditions detected by sensors, allowing the same support structure to function effectively on both level and uneven terrain by adjusting its parameters

Inventive Principle:
Principle #35Parameter changes

2Adaptability or versatility

If adjustable landing supports are added to handle uneven terrain, then terrain adaptability improves, but device complexity increases

Engineering Contradiction:
Improveterrain adaptabilityVSAvoidlanding support system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The landing support system uses sensors to automatically detect terrain characteristics and triggers actuators to adjust the support configuration without pilot intervention, making the system self-regulating and reducing the operational complexity despite the added mechanical components

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system employs pneumatic or hydraulic actuators to adjust landing support configuration, providing smooth and controlled adjustments with simple control mechanisms, thereby managing device complexity through the use of well-established actuation technologies

Inventive Principle:
Principle #29Pneumatics and hydraulics

3Reliability

If manual pilot judgment and control are used for uneven terrain landing, then device complexity remains low, but ease of operation deteriorates and landing safety is reduced

Engineering Contradiction:
Improvelanding safetyVSAvoidlanding operation ease
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system incorporates terrain sensors that provide real-time feedback about surface characteristics to the control computer, which automatically adjusts landing support configuration based on this feedback, eliminating the need for manual pilot judgment and significantly improving both ease of operation and landing safety on uneven terrain

Inventive Principle:
Principle #23Feedback

Data Source

PatentEP2903893B1Configuring landing supports for landing on uneven terrain
Publication Date: 2018.01.10 THE BOEING CO
  • EP2903893B1 patent drawingFigure 1A~1B
  • EP2903893B1 patent drawingFigure 2
  • EP2903893B1 patent drawingFigure 3

AI summary

A system for configuring landing supports of a load to land on uneven terrain includes a terrain sensor configured to detect a terrain characteristic of the uneven terrain. The system further includes landing supports configured to support the load upon landing. The system also includes a support control device operatively coupled to the landing supports, and a landing support control computer that is operatively coupled to the terrain sensor, landing supports, and support control device. The landing support control computer may determine if landing on the uneven terrain is allowable, based on the terrain characteristic and a load characteristic of the load. Upon determining that landing on the uneven terrain is allowable, the support control device configures the landing supports for landing on the uneven terrain.