PATENT CLAIM ANALYSIS

Application Number: 16004991
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-12
Patent Classification: ["290", "052000"]

Abstract:
An auxiliary power unit having internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft drivingly engaged to the engine shaft, a compressor having an outlet in communication with the internal combustion engine inlet, and a turbine having an inlet in communication with the internal combustion engine outlet. The turbine may be a first stage turbine, and the assembly may include a second stage turbine having an inlet in communication with the first stage turbine outlet. A method of providing electrical power to an aircraft is also discussed.

Claim (Index 3):
The power unit as defined in  claim 1 , further comprising a bleed conduit having an end configured for connection with a pneumatic system of the aircraft, the bleed conduit in fluid communication with the outlet of the compressor through a bleed air valve selectively opening and closing the fluid communication between the outlet of the compressor and the end of the bleed conduit configured for connection to the pneumatic system.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 94.0
- Lexical Diversity: 2.16667
- Patent Class: 290.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15616187', '14750207', '14750157', '14750187', '15227496']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6760572244041054
- 35 USC 102 Novelty (BERT): 0.5959569611986855
- Combined Prediction Score: 0.6680471980835635
- Mean Citation Score: 418.061908
- Max Citation Score: 458.56607
- Similarity Product: 452.942127624988

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

Dataset: test