PATENT CLAIM ANALYSIS

Application Number: 16182110
Application Type: Utility
Filing Date: 2018-11
Publication Date: 2019-06
Patent Classification: ["420", "420000"]

Abstract:
A titanium alloy having high strength, fine grain size, and low cost and a method of manufacturing the same is disclosed. In particular, the titanium alloy offers a room temperature longitudinal low cycle fatigue (LCF) maximum stress of at least about 950 MPa over about 20,000 cycles and a room temperature transverse low cycle fatigue (LCF) maximum stress of at least about 970 MPa over about 25,000 cycles. The titanium alloy is particularly useful for a multitude of applications including components of aircraft engines. The titanium alloy comprises, in weight percent, about 6.0 to about 6.7% aluminum, about 1.4 to about 2.0% vanadium, about 1.4 to about 2.0% molybdenum, about 0.20 to about 0.42% silicon, about 0.17 to about 0.23% oxygen, maximum about 0.24% iron, maximum about 0.08% carbon and balance titanium with incidental impurities.

Claim (Index 20):
The titanium alloy of  claim 19 , wherein the alloy consists essentially of:\n aluminum at about 6.5; vanadium at about 1.7; molybdenum at about 1.7; silicon at about 0.36; oxygen at about 0.2; iron at about 0.16; carbon at about 0.03; and balance titanium with incidental impurities.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 98.0
- Lexical Diversity: 1.93976
- Patent Class: 420.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13349483', '12850691', '14179946', '12790502', '13433458']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7784873245173572
- 35 USC 102 Novelty (BERT): 0.5987999949852072
- Combined Prediction Score: 0.7605185915641423
- Mean Citation Score: 380.368516
- Max Citation Score: 517.4904
- Similarity Product: 458.7347591254234

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