PATENT CLAIM ANALYSIS

Application Number: 16202583
Application Type: Utility
Filing Date: 2018-11
Publication Date: 2020-01
Patent Classification: ["340", "973000"]

Abstract:
An aircraft flight control system and method are provided. The system provides a control module that receives inertial data, sensor data, and a target airspeed. The control module processes the received data with aircraft thrust and drag models to evaluate the aircraft energy state. Based on the aircraft energy state, the control module determines (i) a maximum predicted potential flight path “max PPFP”, defined by a maximum thrust at the target airspeed, and (ii) an idle predicted potential flight path, “idle PPFP,” defined by an idle thrust at the target airspeed. The control module generates display commands for a display system to display (i) the flight path angle, (ii) the max PPFP and (iii) the idle PPFP. In addition, the control module generates and displays a predicted flight path speed indicator (PFPS) when the FPA is above the max PPFP or below the idle PPFP.

Claim (Index 5):
The method of  claim 4 , further comprising, at the control module, commanding the PFD to display an indicator for speed in the second designated area on the PFD when the FPA is more than a configurable predetermined upper margin above the max PPFP.

Metadata:
- Claim Count in Document: 7.0
- Percentile: 98.0
- Lexical Diversity: 2.47887
- Patent Class: 340.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15700416', '12847835', '15791970', '14725432', '13008789']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6486943186518618
- 35 USC 102 Novelty (BERT): 0.6225636308362212
- Combined Prediction Score: 0.6460812498702978
- Mean Citation Score: 306.099766
- Max Citation Score: 635.6947
- Similarity Product: 464.0750652636706

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