PATENT CLAIM ANALYSIS

Application Number: 16320264
Application Type: Utility
Filing Date: 2019-01
Publication Date: 2019-09
Patent Classification: ["244", "054000"]

Abstract:
The invention relates to a cradle ( 10 ) for an aircraft turbopropeller engine ( 12 ) of a substantially axial orientation, comprising a front arch ( 16 ) and a rear arch ( 18 ) extending transversely relative to said axial direction (A), said arches ( 16, 18 ) being open at their lower ends and connected to each other by at least one axial longeron ( 34 ) extending between said arches ( 16, 18 ), characterised in that the longeron ( 34 ) is arranged in an upper portion of the cradle ( 10 ) and is formed in a single piece with the front arch ( 16 ).

Claim (Index 1):
Cradle for the turbopropeller engine of an aircraft oriented in a substantially radial direction, comprising a front arch and a rear arch extending transversally with respect to said axial direction (A), said arches being open at their lower ends and connected to one another by at least one axial longeron that extends between said arches,\n wherein the longeron is arranged in the upper portion of the cradle and in that it is formed of one single part with the front arch, and with at least one tubular section configured to define an air inlet duct of said turbopropeller engine.

Metadata:
- Claim Count in Document: 21.0
- Percentile: 99.0
- Lexical Diversity: 1.93548
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['15729504', '15654030', '15654087', '15381821', '12674796']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.842880323400174
- 35 USC 102 Novelty (BERT): 0.4713989485390147
- Combined Prediction Score: 0.8057321859140582
- Mean Citation Score: 188.813692
- Max Citation Score: 221.18883
- Similarity Product: 177.12294490172263

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

Dataset: test