PATENT CLAIM ANALYSIS

Application Number: 15943765
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-10
Patent Classification: ["016", "225000"]

Abstract:
A flexible hinge assembly for aircraft interior components and the like, including: a first structural component, wherein the first structural component includes a core material and one or more skin layers coupled to the core material; a second structural component, wherein the second structural component includes a core material and one or more skin layers coupled to the core material; wherein the one or more skin layers of the first structural component and the one or more skin layers of the second structural component are one or more of coupled together and integrally formed; and a flexure disposed between the first structural component and the second structural component, wherein the flexure is formed by the coupled together and/or integrally formed skin layers.

Claim (Index 9):
The flexible hinge assembly of  claim 1 , wherein the first structural component and the second structural component are both associated with one of a table and a door configured to be installed in an aircraft interior.

Metadata:
- Claim Count in Document: 14.0
- Percentile: 91.0
- Lexical Diversity: 3.04651
- Patent Class: 16.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13690265', '10287463', '13687232', '12752381', '15113130']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7154986711268424
- 35 USC 102 Novelty (BERT): 0.4827660912306929
- Combined Prediction Score: 0.6922254131372275
- Mean Citation Score: 143.954846
- Max Citation Score: 150.66638
- Similarity Product: 93.4279201224351

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

Dataset: test