PATENT CLAIM ANALYSIS

Application Number: 16004087
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["244", "13400D"]

Abstract:
A deicing system for an aircraft may supply heat to an aircraft component in pulses. A first series of pulses may melt ice built up on the aircraft component. A second series of pulses may prevent ice from forming on the aircraft component. The length of each of the pulses in the first series of pulses may be longer than the length of each of the pulses in the second series of pulses. The pulses may be supplied by a pneumatic deicing system or an electrical deicing system.

Claim (Index 5):
The method of  claim 1 , wherein the aircraft component is at least one of an inlet for an aircraft nacelle, a wing leading edge, a horizontal stabilizer, or a vertical fin.

Metadata:
- Claim Count in Document: 11.0
- Percentile: 94.0
- Lexical Diversity: 2.38462
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14861966', '14791085', '15420808', '12167164', '14004974']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8518750699643175
- 35 USC 102 Novelty (BERT): 0.4972237809456036
- Combined Prediction Score: 0.8164099410624461
- Mean Citation Score: 215.115834
- Max Citation Score: 294.35266
- Similarity Product: 255.9925299250269

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

Dataset: test