PATENT CLAIM ANALYSIS

Application Number: 15869972
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-07
Patent Classification: ["415", "178000"]

Abstract:
An aircraft turbine-engine module casing including an external module casing and at least one sealing ring intended to surround a movable impeller of the module and arranged radially towards the inside with respect to the external casing. The casing includes at least one capillary heat pipe, a first end which is fixed to the sealing ring, and a second end which, opposite to the first, is fixed to a casing element arranged radially towards the outside with respect to the ring.

Claim (Index 7):
The casing according to  claim 6 , wherein the tubes are arranged within the same wall of heat pipes, annular in shape.

Metadata:
- Claim Count in Document: 3.0
- Percentile: 86.0
- Lexical Diversity: 1.97727
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['11693270', '15501161', '13981358', '14593483', '13291147']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7612765806242981
- 35 USC 102 Novelty (BERT): 0.4363426957708879
- Combined Prediction Score: 0.7287831921389571
- Mean Citation Score: 142.57703600000005
- Max Citation Score: 147.10817
- Similarity Product: 104.61920045211612

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