Static Aircraft Privacy Panel Floor Mounting
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Solution Overview
Problem
Aircraft cabin privacy panels integrated with aircraft seats often require over-engineering to meet stringent aviation standards, leading to increased weight, cost, and complexity.
Innovation Solution
Designing static aircraft seat privacy panels that are not coupled to aircraft seats, instead being directly coupled to the aircraft cabin floor and overhead structures, allowing them to meet a 9G certification standard rather than the more stringent 16G standard.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If privacy panels are coupled to or integrated into aircraft seat structures, then they provide effective privacy separation, but they require over-engineering to meet aviation standards, increasing weight and complexity
Solution Approach 1:
The privacy panel system is segmented into independent components: the panel itself, the floor-mounted components, and the overhead structure components. This segmentation allows each component to be designed and certified independently, reducing overall system complexity while maintaining privacy separation effectiveness.
Solution Approach 2:
The privacy panel is extracted from the aircraft seat structure and repositioned to be mounted independently between the floor and overhead structures. This extraction eliminates the need for the panel to be integrated into the seat, thereby reducing the structural complexity and certification burden on both the seat and panel systems.
2Adaptability or versatility
If privacy panels are integrated with aircraft seats, then they move with the seat, but they require meeting stringent 16G certification standards, increasing weight
Solution Approach 1:
Instead of mounting the privacy panel to the aircraft seat and having it move with the seat, the panel is inverted to be mounted independently to the floor and overhead structures. This inversion allows the panel to remain stationary relative to the cabin while the seat moves independently, reducing the weight requirements from 16G to 9G certification standards.
3Stability of the object's composition
If privacy panels are coupled to aircraft seats, then they maintain relative position, but they require similar testing and aviation guideline compliance as seats, increasing cost
Solution Approach 1:
The system is divided into independent components (privacy panel, floor-mounted components, overhead components) that can be manufactured and certified separately. This segmentation reduces certification costs by allowing the privacy panel to be certified to 9G standards independently rather than requiring 16G seat integration certification.
Solution Approach 2:
The floor-mounted components and overhead structure components serve as intermediaries between the privacy panel and the aircraft structure. These intermediaries provide the necessary mounting and support functions without requiring direct integration with the aircraft seat, thereby reducing certification complexity and cost.
Data Source
Figure 1A
Figure 1B
Figure 1C
AI summary
A static aircraft seat privacy panel (102) may include a body (106). At least a portion of a surface of the body (106) may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge (108) of the body may be configured to couple to a floor via a set of floor-mounted components (300). The set of floor-mounted components (300) may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge (120) of the body may be configured to be offset a selected distance from a surface of one or more overhead structures (116) of the aircraft cabin when the body (106) is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel (102) may be compliant with 9G force requirements for aviation transport.