PATENT CLAIM ANALYSIS

Application Number: 16218097
Application Type: Utility
Filing Date: 2018-12
Publication Date: 2019-04
Patent Classification: ["073", "012010"]

Abstract:
According to one implementation, a damage detection system includes: a physical quantity detection unit, a flight condition changing part and a damage detection part. The physical quantity detection unit detects a physical quantity of a structural object composing an aircraft during a flight of the aircraft. The flight condition changing part changes at least one flight condition of the aircraft to at least one specific flight condition when the physical quantity of the structural object has been detected by the physical quantity detection unit. The damage detection part determines whether a damage arose in the structural object, based on a physical quantity which has been detected, from the structural object of the aircraft flying with the at least one specific flight condition, by the physical quantity detection unit.

Claim (Index 10):
A damage detection method comprising:\n detecting a physical quantity of a structural object composing an aircraft during a flight of the aircraft; changing at least one flight condition of the aircraft to at least one specific flight condition when the physical quantity of the structural object has been detected; and determining whether a damage arose in the structural object, based on a physical quantity detected from the structural object of the aircraft flying with the at least one specific flight condition, wherein at least one physical quantity of the structural object related with the at least one specific flight condition of the aircraft is previously stored, the at least one physical quantity corresponding to the at least one specific flight condition and a state where no damage exists in the structural object, the at least one flight condition of the aircraft is changed to the stored at least one specific flight condition when the at least one physical quantity of the structural object has been detected during the flight of the aircraft, and whether the damage arose in the structural object s determined based on the physical quantity detected from the structural object of the aircraft flying with the at least one specific flight condition and the at least one physical quantity corresponding to the state where the no damage exists in the structural object.

Metadata:
- Claim Count in Document: 11.0
- Percentile: 98.0
- Lexical Diversity: 2.81633
- Patent Class: 73.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['15175412', '15300655', '15062543', '12750282', '13575365']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6712609636872195
- 35 USC 102 Novelty (BERT): 0.4738791037149971
- Combined Prediction Score: 0.6515227776899973
- Mean Citation Score: 145.889902
- Max Citation Score: 177.43411
- Similarity Product: 131.6542453854668

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