PATENT CLAIM ANALYSIS

Application Number: 15966189
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-12
Patent Classification: ["165", "051000"]

Abstract:
An aircraft including an airframe, a propulsion system, and a heat exchanger is presented. The heat exchanger of the aircraft may include (i) a structural body including a plurality of hollow channels, (ii) a first fluid positioned within the plurality of hollow channels of the structural body, (iii) a plurality of openings positioned on a first side of the structural body and in fluid communication with the plurality of hollow channels, (iv) a wick structure positioned on the first side of the structural body, wherein the wick structure is positioned adjacent to an exterior of the plurality of hollow channels and in fluid communication with the plurality of openings, (v) an inlet to the structural body operable to provide a second fluid from an aircraft system, and (vi) an outlet from the structural body operable to receive the second fluid after receiving heat from the first fluid.

Claim (Index 2):
The aircraft of  claim 1 , wherein the aviation induced structural loads comprise proof and burst, air pressure cycling, vibration, airframe structural support, an inertial load, a thermal cycling load, or a combination thereof.

Metadata:
- Claim Count in Document: 30.0
- Percentile: 91.0
- Lexical Diversity: 2.91379
- Patent Class: 165.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['12757965', '15671031', '12383378', '13786367', '14042039']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8490236176333364
- 35 USC 102 Novelty (BERT): 0.5038659539542374
- Combined Prediction Score: 0.8145078512654266
- Mean Citation Score: 199.152256
- Max Citation Score: 207.42342
- Similarity Product: 114.22549528322696

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

Dataset: test