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 8):
Cradle according to  claim 1 , wherein it further comprises two longitudinal lateral walls, formed of one single part with the longeron, these walls extending towards the rear from the front arch and running along the entire length of the longeron.

Metadata:
- Claim Count in Document: 21.0
- Percentile: 99.0
- Lexical Diversity: 1.93548
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15729504', '15654030', '15654087', '15381821', '12674796']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.856248641268359
- 35 USC 102 Novelty (BERT): 0.4884451977960571
- Combined Prediction Score: 0.8194682969211288
- Mean Citation Score: 188.813692
- Max Citation Score: 221.18883
- Similarity Product: 149.20896279818237

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