Aircraft Window Frame Fastening Device with Insulating Blanket Support
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Solution Overview
Problem
The existing fastening systems for aircraft fuselages require numerous holes for insulating blankets and structural reinforcements, which weaken the frames and compromise thermal and acoustic insulation, necessitating a solution that minimizes structural modifications and maintains insulation performance.
Innovation Solution
A ring-shaped base device with adjustable arms that mounts onto the aircraft window frame, using a mortise-and-tenon system and elastic locking mechanisms, allowing for various configurations without modifying the aircraft structure, and incorporating holding tabs for insulating blankets, supports conduits and cables, and utilizes a hook-and-loop fastening system for secure attachment.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If holes are made in frames to fasten insulating blankets and support systems, then fastening of systems and blankets is enabled, but the frames are weakened and structural complexity increases
Solution Approach 1:
A ring-shaped base device is introduced as an intermediary component that attaches to the window frame and provides multiple fastening points. This mediator enables blanket and system fastening without requiring direct holes in the main frame structure, thereby preserving frame strength while achieving the fastening function.
Solution Approach 2:
The fastening function is segmented from the main frame structure. Instead of making holes directly in the frame, the invention uses a separate ring-shaped base with multiple arms that can be attached to the frame and used for fastening blankets and systems independently.
2Ease of operation
If holes and cut-outs are made in insulating blankets to accommodate fastening devices, then fastening is enabled, but thermal and acoustic insulation performance deteriorates
Solution Approach 1:
The ring-shaped base serves as a mediator that fastens blankets without requiring holes or cut-outs in the blanket material itself. The blankets can be attached to the ring structure using clips or other fastening mechanisms that do not compromise the blanket's continuous insulating structure.
Solution Approach 2:
Instead of modifying the blanket to accommodate fastening devices (making holes in the blanket), the invention inverts the approach by providing fastening devices on the ring structure that attach to the blanket from the outside, preserving the blanket's integrity and insulation performance.
3Strength
If structural reinforcements are added to compensate for holes in frames, then frame strength is maintained, but device complexity and manufacturing cost increase
Solution Approach 1:
The ring-shaped base acts as a structural intermediary that distributes fastening loads away from the main frame structure. By attaching this intermediate structure to the frame, the frame itself does not require additional reinforcements, as the ring base absorbs and distributes the mechanical stresses from fastening operations.
4Adaptability or versatility
If multiple separate fastening devices are used for blankets and systems, then specific fastening functions are achieved, but the number of holes and modification points increases
Solution Approach 1:
Multiple fastening functions are merged into a single integrated ring-shaped base device. This unified structure provides multiple attachment points for both insulating blankets and various systems (electrical, hydraulic, pneumatic) without requiring separate fastening devices and multiple holes in the frame structure.
Solution Approach 2:
The ring-shaped base is designed as a universal fastening structure that can accommodate multiple different systems and blanket configurations. Its multiple arms and attachment points allow it to serve various fastening purposes simultaneously, eliminating the need for separate specialized fastening devices for each system.
Data Source
AI summary
The invention relates to a device for fastening systems in an aircraft.It comprises on the one hand a ring-shaped base (2) and on the other hand arms (4, 6) borne by the ring-shaped base (2), extending outward from the latter and bearing systems supports.


