PATENT CLAIM ANALYSIS

Application Number: 16036743
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2018-11
Patent Classification: ["244", "058000"]

Abstract:
An air vehicle power and thermal management system includes an aircraft controller structured to distribute power provided by a gas turbine engine between a cooling system and an electrically powered load. The controller is configured to direct the power to create a first duration cooling power to the cooling system to cool the engine fuel cooling medium over a first power time period. The controller is configured to shift the power to reduce the first duration cooling power to create a load electrical power to drive the electrically powered load over a second power time period. By operation of the controller to shift the power from the first duration cooling power to the load electrical power a second duration cooling power is provided to the cooling system to cool the electrically powered load using the engine fuel cooling medium that was cooled during the first power time period.

Claim (Index 37):
The method of  claim 35 , further comprising reducing power to the first refrigeration system once the first heat sink fluid is directed from the first heat sink reservoir to the first electrical load.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 95.0
- Lexical Diversity: 2.76364
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14692104', '15044523', '15433681', '15358444', '13215456']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8058405882854816
- 35 USC 102 Novelty (BERT): 0.5135957028160244
- Combined Prediction Score: 0.7766160997385358
- Mean Citation Score: 168.532492
- Max Citation Score: 246.04639
- Similarity Product: 130.95022453908322

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