PATENT CLAIM ANALYSIS

Application Number: 15947890
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-08
Patent Classification: ["060", "796000"]

Abstract:
A gas turbine engine according to an example of the present disclosure includes, among other things, a turbine case extending along a turbine axis and a CMC turbine exhaust case mounted to the turbine case. The CMC turbine exhaust case includes a CMC core nacelle aft portion, a CMC tail cone connected to the CMC core nacelle aft portion, and a multiple of CMC turbine exhaust case struts extending between the CMC core nacelle aft portion and the CMC tail cone. The CMC core nacelle aft portion, the CMC tail cone and the turbine case are arranged along the turbine axis. The CMC turbine exhaust case is mounted to the turbine case at a flange such that the CMC tail cone is axially spaced apart from the turbine case relative to the turbine axis.

Claim (Index 4):
The gas turbine engine as recited in  claim 3 , wherein the multiple of CMC turbine exhaust case struts are bonded to said CMC core nacelle aft portion and said CMC tail cone.

Metadata:
- Claim Count in Document: 43.0
- Percentile: 91.0
- Lexical Diversity: 2.86
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13116116', '14847363', '13216281', '14915432', '13116173']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7340460761030946
- 35 USC 102 Novelty (BERT): 0.5094067263742602
- Combined Prediction Score: 0.7115821411302112
- Mean Citation Score: 231.088136
- Max Citation Score: 326.4374
- Similarity Product: 254.1587042810917

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

Dataset: test