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 9):
Cradle ( 10 ) according to  claim 8 , wherein the free longitudinal edges of the longitudinal lateral walls are configured to receive hinges for the lateral protection hoods of the turbopropeller engine.

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): 0.8571213359814267
- 35 USC 102 Novelty (BERT): 0.4810675282980491
- Combined Prediction Score: 0.819515955213089
- Mean Citation Score: 188.813692
- Max Citation Score: 221.18883
- Similarity Product: 163.15823468725202

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