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 4):
The system of  claim 3 , wherein a frequency of the AC output is in accordance with a rotational speed of the engine and a gear ratio of a gear mechanism associated with an output shaft included in the drive train and connected to the alternator.

Metadata:
- Claim Count in Document: 37.0
- Percentile: 97.0
- Lexical Diversity: 2.28571
- Patent Class: 290.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['11693532', '10927993', '15244557', '11681686', '11944199']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6419772729131061
- 35 USC 102 Novelty (BERT): 0.4942323812617193
- Combined Prediction Score: 0.6272027837479675
- Mean Citation Score: 211.96727
- Max Citation Score: 223.29752
- Similarity Product: 156.67328958732128

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