PATENT CLAIM ANALYSIS

Application Number: 16256374
Application Type: Utility
Filing Date: 2019-01
Publication Date: 2019-07
Patent Classification: ["244", "217000"]

Abstract:
An aircraft includes a fuselage and first and second pairs of aerofoils, the aerofoils of each pair extend from opposing sides of the fuselage. Each aerofoil includes a first lift body and a second lift body which is arranged behind the first lift body in a direction of flow of the aerofoil. The second lift body is pivotable relative to the first lift body between a cruising flight position in which both lift bodies together define an elongate and substantially continuous cross section of the aerofoil in the direction of flow, and a take-off/landing position in which the second lift body is angled downwards relative to the first lift body in order to increase a lift of the aerofoil. At least one engine is arranged on the second lift body of at least one of the first and second pairs of aerofoils.

Claim (Index 8):
The aircraft according to  claim 1 , further comprising a plurality of engines on at least one of the second lift bodies which are arranged side by side in a row extending transversely to the direction of flow.

Metadata:
- Claim Count in Document: 26.0
- Percentile: 99.0
- Lexical Diversity: 2.46667
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['15135624', '14915101', '14904597', '14784342', '11802139']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8661097346886169
- 35 USC 102 Novelty (BERT): 0.5637018569214569
- Combined Prediction Score: 0.8358689469119008
- Mean Citation Score: 338.4033080000001
- Max Citation Score: 510.51245
- Similarity Product: 376.5757543501557

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

Dataset: test