PATENT CLAIM ANALYSIS

Application Number: 15947301
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2019-10
Patent Classification: ["062", "606000"]

Abstract:
The present invention refers to a cryogenic cooling system utilizing rocket propellant as the working fluid in a phase change closed loop process. The purpose of the system is to enable long term zero boil off storage of cryogenic liquid rocket propellant in space. The system will also enable transfer of cryogenic liquid from one tank volume to another in a propellant depot mode of operation.

Claim (Index 3):
The process of  claim 1  wherein the prime mover (compressor) for the thermodynamic cooling cycle also effects liquid transfer out of the storage tank.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 91.0
- Lexical Diversity: 1.5
- Patent Class: 62.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15863081', '14343180', '10947453', '14443760', '11132135']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8022755887048628
- 35 USC 102 Novelty (BERT): 0.4467409877569086
- Combined Prediction Score: 0.7667221286100674
- Mean Citation Score: 75.6520814
- Max Citation Score: 80.35455
- Similarity Product: 60.34410594897865

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