PATENT CLAIM ANALYSIS

Application Number: 16264760
Application Type: Utility
Filing Date: 2019-02
Publication Date: 2019-07
Patent Classification: ["702", "034000"]

Abstract:
A method of monitoring a gas turbine engine includes the steps of: (a) receiving information from actual flights of an aircraft including an engine to be monitored, and including at least one of the ambient temperature at takeoff, and internal engine pressures, temperatures and speeds; (b) evaluating the damage accumulated on an engine component given the data received in step (a); (c) storing the determined damage from step (b); (d) repeating steps (a)-(c); (e) recommending a suggested future use for the component based upon steps (a)-(d). A system is also disclosed.

Claim (Index 1):
A method of monitoring a gas turbine engine comprising the steps of:\n (a) receiving information from actual flights of an aircraft including an engine to be monitored, and including at least one of the ambient temperature at takeoff, and internal engine pressures, temperatures and speeds; (b) evaluating the damage accumulated on an engine component given the data received in step (a); (c) storing the determined damage from step (b); (d) repeating steps (a)-(c); (e) recommending a suggested future use for the component based upon steps (a)-(d).

Metadata:
- Claim Count in Document: 51.0
- Percentile: 99.0
- Lexical Diversity: 1.86765
- Patent Class: 702.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15161323', '15616589', '15617338', '15346571', '13144358']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.1864532080726215
- 35 USC 102 Novelty (BERT): 0.5298845466075788
- Combined Prediction Score: 0.2207963419261172
- Mean Citation Score: 201.549736
- Max Citation Score: 368.3607
- Similarity Product: 364.37517943770285

Labels:
- Claim Label 101: 1
- Claim Label 102: 0
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 0
- Label 101 Adjusted: 1

Dataset: test