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 2):
The aircraft according to  claim 1 , wherein the first lift body of each of the aerofoils comprises fastening means for supportingly fastening the aerofoil to the fuselage of the aircraft or is integrally connected to the fuselage of the aircraft.

Metadata:
- Claim Count in Document: 26.0
- Percentile: 99.0
- Lexical Diversity: 2.46667
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15135624', '14915101', '14904597', '14784342', '11802139']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8791278440525941
- 35 USC 102 Novelty (BERT): 0.5669516008346118
- Combined Prediction Score: 0.8479102197307959
- Mean Citation Score: 338.4033080000001
- Max Citation Score: 510.51245
- Similarity Product: 381.3563191929578

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