PATENT CLAIM ANALYSIS

Application Number: 16059377
Application Type: Utility
Filing Date: 2018-08
Publication Date: 2018-12
Patent Classification: ["060", "806000"]

Abstract:
A gas turbine engine comprises a core engine housing. A nacelle is positioned radially outwardly of the core engine housing. An outer bypass housing is positioned outwardly of the nacelle. There is at least one accessory to be cooled positioned in a chamber radially between the core engine housing and the nacelle. A manifold delivers cooling air into the chamber, and extends ng circumferentially about a central axis of the core engine. The nacelle has an asymmetric flow cross-section across a circumferential extent.

Claim (Index 17):
The gas turbine engine as set forth in  claim 16 , wherein said manifold has a greater cross-sectional area associated with a circumferential location where said inlet tube enters said manifold, and having a lesser cross-sectional area at locations spaced circumferentially from said area of greater flow cross-sectional area.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 96.0
- Lexical Diversity: 1.73077
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15111553', '13593842', '15138727', '15062442', '13731133']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7641168666513078
- 35 USC 102 Novelty (BERT): 0.5465398963328172
- Combined Prediction Score: 0.7423591696194588
- Mean Citation Score: 307.0378340000001
- Max Citation Score: 445.68747
- Similarity Product: 336.8781682513512

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

Dataset: test