PATENT CLAIM ANALYSIS

Application Number: 15887136
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2018-06
Patent Classification: ["415", "184000"]

Abstract:
According to an example embodiment, a gas turbine engine assembly includes, among other things, a fan section including a fan, the fan including a plurality of fan blades, a diameter of the fan having a dimension D that is based on a dimension of the fan blades, each fan blade having a leading edge, and a forward most portion on the leading edges of the fan blades in a first reference plane, a geared architecture, a turbine section including a high pressure turbine and a low pressure turbine, the low pressure turbine driving the fan through the geared architecture, a nacelle surrounding the fan, the nacelle including an inlet portion forward of the fan, a forward edge on the inlet portion in a second reference plane, and a length of the inlet portion having a dimension L measured along an engine axis between the first reference plane and the second reference plane. A dimensional relationship of L/D is no more than 0.45.

Claim (Index 18):
The assembly of  claim 17 , wherein the mid-turbine frame includes a plurality of vanes in a core airflow path defined by the turbine section.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 88.0
- Lexical Diversity: 2.57971
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14091862', '14432377', '14875750', '14430798', '14875762']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7870046664890958
- 35 USC 102 Novelty (BERT): 0.4808665092084454
- Combined Prediction Score: 0.7563908507610307
- Mean Citation Score: 264.088094
- Max Citation Score: 319.22925
- Similarity Product: 242.37769553066792

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