PATENT CLAIM ANALYSIS

Application Number: 16168041
Application Type: Utility
Filing Date: 2018-10
Publication Date: 2019-02
Patent Classification: ["700", "283000"]

Abstract:
Embodiments include a modular fuel pump apparatus for an aircraft refueling chassis and related devices, systems and methods. In one exemplary embodiment, a pump module includes a hydraulic motor driven by a hydraulic pump connected to a chassis motor. A chassis engine is operated at a substantially constant RPM, which causes the hydraulic pump to output hydraulic fluid to the pump module at a substantially constant hydraulic pressure. The speed of the hydraulic motor can be varied by a proportional flow control valve disposed between the hydraulic pump and the hydraulic motor, thereby varying the speed of the fuel pump and the flow rate of the fuel. A controller is configured to operate the pressure control valve such that the flow of the fuel is maintained at a predetermined flow rate.

Claim (Index 3):
The pump module of  claim 2 , wherein the controller is configured to determine the predetermined flow rate range at least in part by determining user selection of one of the at least two fuel delivery hose assemblies.

Metadata:
- Claim Count in Document: 45.0
- Percentile: 97.0
- Lexical Diversity: 2.08955
- Patent Class: 700.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14204691', '13840090', '10157363', '15502550', '12441489']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4432851889010272
- 35 USC 102 Novelty (BERT): 0.5319061734902788
- Combined Prediction Score: 0.4521472873599524
- Mean Citation Score: 245.734264
- Max Citation Score: 378.85474
- Similarity Product: 365.5884010175144

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