PATENT CLAIM ANALYSIS

Application Number: 16035317
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-02
Patent Classification: ["244", "099110"]

Abstract:
An aircraft wing load alleviation device is to be provided to an aircraft having a body, a main wing, and an elongated supporting member with an end fixed to the body and another end fixed to the main wing to support the main wing. The aircraft wing load alleviation device alleviates a load acting on the main wing, and includes a load detector, an actuator, and a controller. The load detector detects the load acting on the main wing. The actuator is provided to the supporting member and applies a load in a longitudinal direction of the supporting member. The controller controls, when the load acting on the main wing is detected, operation of the actuator to make the actuator apply the load to the supporting member in a direction opposite to a direction of a load applied on the supporting member as a result of the detected load.

Claim (Index 16):
The aircraft wing load alleviation device according to  claim 8 , wherein the main wing has a root that is directly fixed to the body.

Metadata:
- Claim Count in Document: 3.0
- Percentile: 95.0
- Lexical Diversity: 3.15686
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15213636', '15561807', '14222061', '12705691', '14307112']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8253072729494145
- 35 USC 102 Novelty (BERT): 0.4909951368156413
- Combined Prediction Score: 0.7918760593360372
- Mean Citation Score: 163.697848
- Max Citation Score: 168.07997
- Similarity Product: 104.26362116467716

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