PATENT CLAIM ANALYSIS

Application Number: 16081046
Application Type: Utility
Filing Date: 2018-08
Publication Date: 2019-03
Patent Classification: ["060", "752000"]

Abstract:
A flow element for fluidic contact with a hot gas flow inside an aircraft engine includes: a base material, which has a hot gas surface that faces the gas flow and a remote surface that is remote from the gas flow, the base material being completely surrounded by a chroming layer on the hot gas surface and on the remote surface; an adhesive layer on the chroming layer in first portions; an alitising layer, the alitising layer being arranged on the adhesive layer in the first portions; and a thermal barrier layer being arranged on the alitising layer in the first portions. The alitising layer is arranged on the chroming layer in second portions that do not have an adhesive layer, the chroming layer and the alitising layer forming a chroming-alitising layer in the second portions.

Claim (Index 3):
The flow element according to  claim 1 , wherein, in the chroming-alitising layer, the Cr content is higher than the Al content.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 96.0
- Lexical Diversity: 2.75472
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['09915765', '14860051', '14903272', '10870542', '10470677']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.722601202662474
- 35 USC 102 Novelty (BERT): 0.4742052242370681
- Combined Prediction Score: 0.6977616048199333
- Mean Citation Score: 113.163076
- Max Citation Score: 128.29608000000002
- Similarity Product: 80.14504067481995

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