PATENT CLAIM ANALYSIS

Application Number: 15778569
Application Type: Utility
Filing Date: 2018-05
Publication Date: 2019-07
Patent Classification: ["244", "119000"]

Abstract:
A method of constructing a panel for an aircraft subassembly is provided. The panel has interior and exterior sides relative to the subassembly and comprises a skin and a support structure. The support structure comprises a plurality of longerons and frames constituting support-structure elements and arranged substantially in a grid, and projecting substantially transversely from the skin toward the interior side. The method comprises providing a flat sheet of structural material, wherein the sheet comprises one or more cutouts, and forming the support structure by folding the sheet, wherein the longerons and frames are formed from overfolded areas of the sheet adjacent the cutouts, and wherein non-overfolded areas of the sheet constitute the skin.

Claim (Index 64):
The method according to  claim 56 , wherein said panel constitutes part of a semi-monocoque structure of said aircraft subassembly.

Metadata:
- Claim Count in Document: 5.0
- Percentile: 93.0
- Lexical Diversity: 1.98387
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['12045065', '13036199', '15383104', '10907729', '14578653']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8618411868982779
- 35 USC 102 Novelty (BERT): 0.497187240056211
- Combined Prediction Score: 0.8253757922140712
- Mean Citation Score: 202.848054
- Max Citation Score: 213.36035
- Similarity Product: 124.47529532454014

Labels:
- Claim Label 101: 1
- Claim Label 102: 0
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 0
- Label 101 Adjusted: 1

Dataset: test