PATENT CLAIM ANALYSIS

Application Number: 16202623
Application Type: Utility
Filing Date: 2018-11
Publication Date: 2019-03
Patent Classification: ["277", "651000"]

Abstract:
An assembly for use on an aircraft wing having an aircraft skin and a fuel tank, the assembly comprising a metal access door for accessing the fuel tank, a metal retainer ring for engaging the wing and the access door. Fasteners removably couple the access door to the retainer ring. A lip, which may be on the wing surface, is configured to receive a perimeter of the access door when the access door is coupled to the retainer ring. A polyurethane elastomeric gel gasket having a metallic skeleton is configured to lay between the access door and a lip of the metal wing surface. Under compression, the polyurethane will deform and squeeze out the edges and flatten so as to provide metal-to-metal contact between the access door and the lip.

Claim (Index 4):
The gasket of  claim 1 , wherein in the compressed condition the gasket is about 40-80% of its uncompressed thickness.

Metadata:
- Claim Count in Document: 74.0
- Percentile: 98.0
- Lexical Diversity: 2.22222
- Patent Class: 277.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15085389', '15666960', '13788583', '14698416', '13793533']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8243157495191752
- 35 USC 102 Novelty (BERT): 0.5182163802337353
- Combined Prediction Score: 0.7937058125906311
- Mean Citation Score: 277.327944
- Max Citation Score: 348.29886
- Similarity Product: 345.20936411775824

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

Dataset: test