PATENT CLAIM ANALYSIS

Application Number: 15891869
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2019-04
Patent Classification: ["340", "978000"]

Abstract:
An airspeed indicator display for an aircraft having a main rotor system and a translational thrust system includes a first indicator operable to display an actual airspeed of the aircraft and a second indicator positioned adjacent the first indicator. The second indicator is operable to display an actual pitch angle of the translational thrust system.

Claim (Index 5):
The airspeed indicator of  claim 1 , further comprising a third indicator operable to display a digital, numerical readout of the second indicator.

Metadata:
- Claim Count in Document: 10.0
- Percentile: 88.0
- Lexical Diversity: 1.9
- Patent Class: 340.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15892045', '15504248', '15508346', '15514115', '15501095']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6783929868983918
- 35 USC 102 Novelty (BERT): 0.5286087817114384
- Combined Prediction Score: 0.6634145663796964
- Mean Citation Score: 227.941084
- Max Citation Score: 318.57495
- Similarity Product: 203.96190484371184

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