PATENT CLAIM ANALYSIS

Application Number: 16026226
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2018-11
Patent Classification: ["102", "439000"]

Abstract:
The invention here described of novel aerodynamics and construction has been shown to alleviate the problems inherent in subsonic ballistics, such as, but not limited to, tumbling in flight, loss of impact energy, as well as the changes in both accuracy and precision of the firearm shots fired at subsonic speeds. The subsonic bullet herein described has three main aerodynamic components that aid in subsonic flight: 1) a parabolic or hemispherical nose; 2) a cylindrical center length with parallel sides; 3) a cone-like parabolic tail with an optimized tail geometry to slowly converge the laminar flow around the bullet without introducing turbulence. These features serve to reduce air pressure and turbulent airflow around the bullet during flight.

Claim (Index 4):
The bullet of  claim 2  where said cone-like parabolic tail and tail section extend into the interior of said standard caliber casing.

Metadata:
- Claim Count in Document: 11.0
- Percentile: 95.0
- Lexical Diversity: 1.47191
- Patent Class: 102.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14953315', '13208619', '15282160', '12660802', '11899647']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7452530594157134
- 35 USC 102 Novelty (BERT): 0.5033754576953414
- Combined Prediction Score: 0.7210652992436761
- Mean Citation Score: 184.814594
- Max Citation Score: 210.15579
- Similarity Product: 118.5027150321114

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

Dataset: test