PATENT CLAIM ANALYSIS

Application Number: 16026423
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2020-01
Patent Classification: ["701", "018000"]

Abstract:
Methods and systems are provided for guiding or otherwise assisting a stabilized approach to a destination by presenting an energy state associated with an aircraft with respect to a target energy state for the stabilized approach. One method involves providing a graphical indication of a targeted energy state at a first position, a second graphical indication of a current energy state at a second position, and a third graphical indication of a configuration change at a third position. The distance with respect to a reference axis between the first position and the second position corresponds to a difference between a target parameter value associated with the targeted energy state and a current parameter value associated with the current energy state, and while a second distance between the first position and the third position with respect to the reference axis corresponds to an estimated amount of time before the configuration change.

Claim (Index 16):
A method of presenting an energy state associated with an aircraft on a supplemental energy management graphical user interface (GUI) display, the method comprising:\n providing, on a display device of an electronic flight bag (EFB), the supplemental energy management GUI display comprising a reference axis, a first graphical indication of a first parameter at a first position with respect to the reference axis, a second graphical indication of a second parameter at a second position with respect to the reference axis, wherein:\n a first distance between the first position and reference axis corresponds to a first difference between a first target value for the first parameter associated with a targeted energy state and a first current value for the first parameter associated with a current energy state of the aircraft; and \n a second distance between the second position and the reference axis corresponds to a second difference between a second target value for the second parameter associated with the targeted energy state and a second current value for the second parameter associated with the current energy state of the aircraft; and \n dynamically updating the first distance on the supplemental energy management GUI display as the aircraft travels to reflect a third difference between the first target value and a first updated value for the first parameter associated with an updated energy state of the aircraft; and dynamically updating the second distance on the supplemental energy management GUI display as the aircraft travels to reflect a fourth difference between the second target value and a second updated value for the second parameter associated with the updated energy state of the aircraft.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 95.0
- Lexical Diversity: 2.68966
- Patent Class: 701.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15047355', '14967557', '15019650', '15019675', '15357086']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4449600028329772
- 35 USC 102 Novelty (BERT): 0.5059172104134455
- Combined Prediction Score: 0.4510557235910241
- Mean Citation Score: 237.378526
- Max Citation Score: 290.7157
- Similarity Product: 204.63130969568488

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