PATENT CLAIM ANALYSIS

Application Number: 15896551
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2018-06
Patent Classification: ["428", "034000"]

Abstract:
An aircraft includes a fuselage defining a mold line, at least one frame disposed in the fuselage, at least one transparent pane suspended within the frame. The transparent pane is a deformable material that defines a first surface position h 1  when not subjected to a differential pressure ΔP thereacross and a second surface position h 2  when subject to the differential pressure ΔP thereacross. The first and second surface positions are defined with reference to the outside mold line. The first surface position h 1  defines a reverse curvature. In response to the differential pressure ΔP, the second surface position h 2  includes bulging of the transparent pane by a predetermined distance Δh. The frame is constructed to be positioned within the aircraft such that the transparent pane presents a surface, when subjected to the pressure differential ΔP, that is substantially consistent with the outside mold line of the vehicle.

Claim (Index 4):
The aircraft of  claim 1 , wherein the second surface position h 2  lies between about 0.08 and \u22120.03 inches (2 and \u22120.76 mm) from the outside mold line.

Metadata:
- Claim Count in Document: 26.0
- Percentile: 88.0
- Lexical Diversity: 2.38235
- Patent Class: 428.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14364206', '13896754', '11223297', '14451857', '14836914']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.9046749056557593
- 35 USC 102 Novelty (BERT): 0.5808140704815272
- Combined Prediction Score: 0.8722888221383359
- Mean Citation Score: 281.192532
- Max Citation Score: 501.57553
- Similarity Product: 412.4664044588244

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

Dataset: test