PATENT CLAIM ANALYSIS

Application Number: 15874335
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-06
Patent Classification: ["244", "015000"]

Abstract:
A cross flow fan to be incorporated into an aircraft fuselage comprises an ingestion fan rotor to be positioned in a tail section of an aircraft fuselage to reduce boundary layer air from a top surface of the fuselage and to drive the air away from the top surface, and a drive arrangement for the ingestion fan rotor. An aircraft is also disclosed.

Claim (Index 19):
The aircraft as set forth in  claim 10 , further comprising rear stabilizers extending upwardly from a fuselage body and connected to a tail, and said drive arrangement is mounted in at least one of said stabilizers.

Metadata:
- Claim Count in Document: 9.0
- Percentile: 86.0
- Lexical Diversity: 1.69231
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15072657', '14620259', '14930712', '15606051', '14737580']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8319474814056683
- 35 USC 102 Novelty (BERT): 0.4965893943611227
- Combined Prediction Score: 0.7984116727012138
- Mean Citation Score: 245.956214
- Max Citation Score: 259.19928
- Similarity Product: 190.29048513150207

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