PATENT CLAIM ANALYSIS

Application Number: 16018445
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2019-01
Patent Classification: ["340", "686600"]

Abstract:
Methods and systems for detecting skew in a wing slat of an aircraft are provided. At least one pair of sensors associated with the wing slat is excited via at least one first electronic device. In response to the exciting and at the at least one first electronic device, at least one pair of signals indicative of at least one pair of state-change counts for the at least one pair of sensors is obtained. The at least one pair of state-change counts is transmitted to at least one second electronic device communicatively coupled to the at least one first electronic device. At the at least one second electronic device, a skew level of the wing slat is determined based on the at least one pair of state-change counts.

Claim (Index 12):
The method of  claim 1 , wherein transmitting the first pair of state-change counts to the at least one second electronic device comprises transmitting the at least first pair of state-change counts via at least one data module cabinet (DMC).

Metadata:
- Claim Count in Document: 44.0
- Percentile: 94.0
- Lexical Diversity: 2.7
- Patent Class: 340.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14683036', '13684340', '14034987', '12946323', '12433021']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.683251732066849
- 35 USC 102 Novelty (BERT): 0.500017642333771
- Combined Prediction Score: 0.6649283230935412
- Mean Citation Score: 158.34642200000005
- Max Citation Score: 169.50229
- Similarity Product: 106.99337407309532

Labels:
- Claim Label 101: 1
- Claim Label 102: 0
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 0
- Label 101 Adjusted: 1

Dataset: test