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 1):
An aircraft, comprising:\n a fuselage defining an outside mold line; at least one frame disposed in the fuselage; and a window disposed in the at least one frame, the window comprising\n at least one transparent pane suspended within the frame, \n wherein the transparent pane comprises a deformable material, \n wherein the transparent pane defines a first surface position h 1  when not subjected to a pressure differential \u0394P thereacross and a second surface position h 2  when subject to the differential pressure \u0394P thereacross, \n wherein the first and second surface positions are defined with reference to the outside mold line, \n wherein the first surface position h 1  defines a reverse curvature with respect to the outside mold line, \n wherein, in response to the differential pressure \u0394P, the second surface position h 2  includes bulging of the transparent pane by a predetermined distance \u0394h from the first surface position h 1 , and \n wherein the frame is constructed to be positioned within the aircraft such that the transparent pane presents a surface, when subjected to the pressure differential, that is substantially consistent with the outside mold line of the aircraft, \n and wherein the aircraft of claim  26 , wherein the first surface position h 1  lies between about 0.17 and 0.06 inches (4.32 and 1.52 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: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14364206', '13896754', '11223297', '14451857', '14836914']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8930102631490188
- 35 USC 102 Novelty (BERT): 0.584072257852734
- Combined Prediction Score: 0.8621164626193902
- Mean Citation Score: 281.192532
- Max Citation Score: 501.57553
- Similarity Product: 440.5840491603792

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