PATENT CLAIM ANALYSIS

Application Number: 15743594
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-07
Patent Classification: ["123", "192100"]

Abstract:
An internal combustion engine for use with a propeller driven aircraft includes a camshaft adapted to function as an output shaft that rotates a propeller to provide propulsive thrust. A gear set is configured to transfer rotational power from the crankshaft to the camshaft and to rotate the camshaft at a velocity that is proportional to the rotational velocity of the crankshaft. The gear set is disposed rearward of the engine housing rearward wall and is configured to rotate the camshaft in a direction opposite the crankshaft rotation. The length of the camshaft reduces engine torsional vibration. In one embodiment, the engine is a six-cylinder compression ignition engine having a boxer configuration and can generate a peak output power within a range from about 300 horsepower to about 350 horsepower.

Claim (Index 8):
The internal combustion engine of  claim 1  wherein the length of the camshaft reduces engine torsional vibration.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 86.0
- Lexical Diversity: 1.81333
- Patent Class: 123.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13286323', '12567401', '09935425', '14902625', '12954945']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7588172553681332
- 35 USC 102 Novelty (BERT): 0.4865230667025179
- Combined Prediction Score: 0.7315878365015717
- Mean Citation Score: 215.283702
- Max Citation Score: 220.32816
- Similarity Product: 148.38950582828522

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