Sensor Aperture Cleaning for Aircraft Visibility

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Solution Overview

Problem

Aircraft designs with reduced out-the-window visibility, such as supersonic aircraft, face challenges in providing pilots with adequate forward visibility due to long noses and high angles of attack, which can impair depth perception and require complex mechanical solutions like droop-nose designs or additional windows, leading to increased drag and weight.

Innovation Solution

The use of sensors mounted beneath the aircraft nose, protected by transparent apertures with cleaning mechanisms, to provide a fused image of the out-the-window scene to display devices, enhancing visibility without the need for traditional cockpit windows or complex mechanical systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If a long nose and high angle of attack configuration is used for supersonic flight, then drag is reduced and high-speed performance is improved, but forward visibility and depth perception are impaired

Engineering Contradiction:
Improvehigh-speed flight capabilityVSAvoidforward visibility and depth perception
Core Design Contradiction:
SpeedVSEase of operation

Solution Approach 1:

The patent introduces sensors as intermediary devices mounted on the aircraft nose to capture external visual information. These sensors act as mediators between the external environment and the pilot, providing visual data without requiring direct line-of-sight through the aircraft structure. The sensors mount system positions sensors at optimal locations to overcome the visibility limitations imposed by the long nose configuration.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces the mechanical solution of moving or drooping the nose structure with an electronic/sensor-based system. Instead of mechanically altering the nose position to improve visibility, the system uses sensors to capture and transmit visual information electronically to the cockpit displays, eliminating the need for complex mechanical actuation systems.

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

2Ease of operation

If droop-nose design or additional cockpit windows are added to improve visibility, then forward visibility is enhanced, but aircraft weight and structural complexity increase

Engineering Contradiction:
Improveforward visibilityVSAvoidaircraft weight
Core Design Contradiction:
Ease of operationVSWeight of moving object

Solution Approach 1:

The patent extracts the visibility function from the physical cockpit window structure and relocates it to sensor-based systems. By taking out the requirement for large transparent windows or movable nose sections, the design eliminates the associated weight penalties while maintaining the essential function of providing external visual information to the pilot.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent creates a visual copy of the external scene through sensors and displays it in the cockpit. Rather than providing direct viewing through windows, the system captures an optical copy of the external environment and presents it to the pilot, achieving the same operational benefit without the weight of additional window structures.

Inventive Principle:
Principle #26Copying

3Ease of operation

If sensors are mounted beneath the aircraft nose to provide out-the-window views, then visibility is enhanced without mechanical complexity, but sensor apertures are susceptible to obstruction from ice, rain, and debris

Engineering Contradiction:
Improvevisibility enhancementVSAvoidsensor aperture clarity
Core Design Contradiction:
Ease of operationVSReliability

Solution Approach 1:

The patent applies preliminary protective actions to the sensor apertures by positioning them within recessed mount structures that protrude only slightly from the aircraft surface. This preliminary positioning protects the apertures before obstructions can accumulate, reducing the likelihood of ice and debris buildup while maintaining optical access to the external environment.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent incorporates dynamic heating elements within the sensor aperture structures to actively prevent ice and contaminant accumulation. By applying thermal energy dynamically to the aperture surfaces, the system maintains clarity despite exposure to adverse weather conditions, ensuring continuous reliable operation of the sensor systems.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS7982767B2System and method for mounting sensors and cleaning sensor apertures for out-the-window displays
Publication Date: 2011.07.19 SUPERSONIC AEROSPACE INTERNATIONAL LLC
  • US7982767B2 patent drawing
  • US7982767B2 patent drawing
  • US7982767B2 patent drawing

AI summary

Multiple sensors capture images representing scenery outside an aircraft or other type of vehicle for use within a visual display system. A protective housing encloses the sensors. This protective housing includes a transparent aperture through which the sensor captures images. A cleaning mechanism removes obstructions from the transparent aperture in order to provide continuous images representing scenery outside the aircraft through an operator display.