PATENT CLAIM ANALYSIS

Application Number: 16177313
Application Type: Utility
Filing Date: 2018-10
Publication Date: 2019-03
Patent Classification: ["290", "00100R"]

Abstract:
In an embodiment, an integrated ground support system for an aircraft is described herein, the system including a frame on which the system is arranged as a singular assembly. An engine, drive train, alternator, bleed air unit, one or more electrical components, and air cycle machine are mounted on the frame. The engine operates at a first operational state associated with a first rotational speed that is independent of a frequency associated with electrical power, if only the electrical power is to be used by the aircraft, and the engine operates at a second operational state associated with a second rotational speed, different from the first rotational speed, that is a function of a pressure associated with bleed air or the conditioned air, if the electrical power and one of the bleed air or the conditioned air are to be used simultaneously by the aircraft.

Claim (Index 14):
An integrated ground support system for an aircraft, the system comprising:\n a frame on which the system is arranged as a singular assembly; an engine mounted on the frame and configured to power the system; a drive train, an alternator, and a bleed air unit mounted on the frame, the drive train disposed between and interconnected to the engine and each of the alternator and the bleed air unit; an inverter and a power converter mounted on the frame, the inverter disposed between and electrically connected to the alternator and the power converter, wherein the power converter is configured to produce electrical power for use by the aircraft; a first control loop connected to the power converter and configured to monitor and maintain the electrical power at a level required by the aircraft; an air cycle machine mounted on the frame and connected to the bleed air unit, wherein the bleed air unit is configured to produce bleed air for use by the aircraft and the air cycle machine is configured to produce conditioned air for use by the aircraft; and a second control loop connected to the bleed air unit and the air cycle machine and configured to monitor and maintain the bleed air or conditioned air at a level required by the aircraft.

Metadata:
- Claim Count in Document: 37.0
- Percentile: 97.0
- Lexical Diversity: 2.28571
- Patent Class: 290.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['11693532', '10927993', '15244557', '11681686', '11944199']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.617211774713209
- 35 USC 102 Novelty (BERT): 0.4787326232631769
- Combined Prediction Score: 0.6033638595682058
- Mean Citation Score: 211.96727
- Max Citation Score: 223.29752
- Similarity Product: 182.2301383361673

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

Dataset: test