Aircraft Seat Sleep-State Control for Real-Time Comfort Adjustment

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Solution Overview

Problem

Aircraft sleeping environments are markedly different from residential settings, posing challenges for optimizing sleep quality due to temperature fluctuations, disturbances, and turbulence, and conventional comfort systems are manually controlled, leading to suboptimal sleep conditions.

Innovation Solution

A real-time control system using optical, thermal, and pressure sensors to monitor passenger states and physiological parameters, automatically adjusting ambient light, temperature, and noise cancellation to enhance sleep quality.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If manual comfort control systems are used in aircraft seats, then device complexity is reduced, but sleep quality and passenger comfort deteriorate due to inability to adapt to changing conditions

Engineering Contradiction:
Improvedevice complexityVSAvoidsleep quality
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The system enables the aircraft seat to automatically monitor passenger sleep states through sensors and adjust environment subsystems (lighting, temperature, noise) without manual intervention. The controller processes sensor data and autonomously modifies seat parameters to maintain optimal sleep conditions throughout the flight.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system continuously monitors passenger physiological parameters and sleep states through multiple sensors, feeds this information back to the controller, and automatically adjusts environment subsystems based on the detected sleep state. This closed-loop feedback mechanism ensures adaptive comfort control throughout the flight.

Inventive Principle:
Principle #23Feedback

2Adaptability or versatility

If real-time automated control systems are implemented to improve sleep quality, then adaptability and comfort are enhanced, but device complexity and system cost increase

Engineering Contradiction:
Improvesleep qualityVSAvoidsystem complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The aircraft seat integrates multiple functions into a single system: sleep state detection, physiological parameter monitoring, and control of multiple environment subsystems (lighting, temperature, noise cancellation). This multi-functional integration reduces the need for separate systems while comprehensive sleep optimization.

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

Solution Approach 2:

The system combines sensor data from optical, thermal, and pressure sensors with control functions for lighting, temperature, and noise cancellation into a unified automated control architecture. The controller integrates multiple input signals and coordinates multiple output controls to achieve comprehensive sleep state management.

Inventive Principle:
Principle #5Merging (Combining)

3Measurement precision

If multiple sensors are used to accurately detect passenger sleep states, then measurement precision is improved, but device complexity and energy consumption increase

Engineering Contradiction:
Improvesleep state detection accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system divides sleep state detection into multiple independent sensing channels: optical sensors for eye closure detection, thermal sensors for body temperature monitoring, and pressure sensors for respiratory movement detection. Each sensor type targets specific physiological indicators, and the controller integrates these segmented measurements to determine overall sleep state with high precision.

Inventive Principle:
Principle #1Segmentation

4Adaptability or versatility

If environment subsystems are automatically adjusted in near real-time, then passenger comfort and sleep quality are improved, but energy consumption increases

Engineering Contradiction:
Improvepassenger comfortVSAvoidenergy consumption
Core Design Contradiction:
Adaptability or versatilityVSUse of energy by moving object

Solution Approach 1:

The controller adjusts environment subsystems periodically based on detected sleep states rather than continuously. Once a sleep state is detected, the system applies appropriate controls (lighting dimming, temperature adjustment, noise cancellation) and maintains them until the sleep state changes, reducing unnecessary energy consumption while maintaining comfort during sleep periods.

Inventive Principle:
Principle #19Periodic action

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

The system provides non-invasive, real-time control of aircraft environment parameters to improve sleep quality and duration by detecting passenger states and adjusting lighting, temperature, and pressure distribution.

Implementation Method 1

one or more optical sensors configured to capture one of an image feed or a video feed of a passenger

Methodology Applied
Scientific EffectOptical detection: Reflection

Implementation Method 2

one or more thermal sensors configured to measure a body temperature of the passenger

Methodology Applied
Scientific EffectThermal radiation detection: Thermal Radiation

Implementation Method 3

one or more pressure sensors

Methodology Applied
Scientific EffectPressure sensing: Pressure Gradient

Data Source

PatentUS12534205B2Real-time control for passenger comfort and sleep quality for aircraft seating
Publication Date: 2026.01.27 BE AEROSPACE INC
  • US12534205B2 patent drawing
  • US12534205B2 patent drawing
  • US12534205B2 patent drawing

AI summary

A system may include one or more optical sensors configured to capture one of an image feed or a video feed of a passenger and a controller communicatively coupled to the plurality of sensors. The controller may be configured to: receive a set of sensor data from the plurality of sensors; determine a first sleep state of the passenger; determine a first set of controls associated with the first sleep state; provide the first set of controls associated with the first sleep state to the at least one aircraft environment sub-system automatically, in near real-time; determine a second sleep state of the passenger; determine a second set of controls associated with the second sleep state; and provide the second set of controls associated with the second sleep state to the at least one aircraft environment sub-system automatically, in near real-time.