PATENT CLAIM ANALYSIS

Application Number: 16137688
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2019-03
Patent Classification: ["340", "960000"]

Abstract:
A system for monitoring steering of an aircraft landing gear wheel includes: a controller; a warning device for emitting warning signals for a tractor operator maneuvering the aircraft on the ground; and at least one angular sensor. The controller compares effective steering angle information, supplied by the angular sensor(s), with angles αSD, αMD, αSG and αMG, where αMD and αMG are limits of a predefined steering angle range within which the landing gear wheel steering is to remain confined, and where αSD and αSG are intermediate angles within the range. The controller commands emission of a warning signal when the comparison indicates that the steering of the landing gear wheel is between angles αSD and αMD or between angles αSG and αMG; and modulates the warning signal depending on the effective position of the steering between the angles αSD and αMD or between the angles αSG and αMG.

Claim (Index 10):
The monitoring system according to  claim 9 , wherein the modulating device is configured to modulate the signal incrementally between the angles \u03b1SD and \u03b1MD and between the angles \u03b1SG and \u03b1MG.

Metadata:
- Claim Count in Document: 38.0
- Percentile: 97.0
- Lexical Diversity: 2.21622
- Patent Class: 340.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['14042469', '11965413', '12280356', '11159472', '14580474']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7164854999528585
- 35 USC 102 Novelty (BERT): 0.5134377044208696
- Combined Prediction Score: 0.6961807203996596
- Mean Citation Score: 199.924666
- Max Citation Score: 211.42458
- Similarity Product: 129.2608565270877

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