PATENT CLAIM ANALYSIS

Application Number: 15959778
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-08
Patent Classification: ["244", "13400A"]

Abstract:
Apparatuses for and methods of deicing aircraft surfaces, engine inlets, windmill blades and other structures are disclosed. Deicing apparatuses comprising at least one standoff coupled with an actuator and a first region of an inner surface of a skin are disclosed. A standoff can act as a moment arm and can create efficient, tailorable skin bending and acceleration, breaking an ice to skin bond. Integral as well as modular leading edges comprising deicing apparatuses are disclosed.

Claim (Index 24):
The aircraft modular leading edge of claim  1  wherein:\n said modular leading edge is an engine inlet leading edge.

Metadata:
- Claim Count in Document: 38.0
- Percentile: 91.0
- Lexical Diversity: 1.52727
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15789854', '15434288', '11770781', '11057508', '12658304']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8631174231761028
- 35 USC 102 Novelty (BERT): 0.5538851957769664
- Combined Prediction Score: 0.8321942004361892
- Mean Citation Score: 264.76938199999995
- Max Citation Score: 449.84576
- Similarity Product: 368.328869611206

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