PATENT CLAIM ANALYSIS

Application Number: 16218961
Application Type: Utility
Filing Date: 2018-12
Publication Date: 2019-05
Patent Classification: ["361", "679340"]

Abstract:
A shock resistant fuselage system includes first and second fuselage side walls, each of the first and second fuselage side walls having a plurality of guide posts, and a printed circuit board (PCB) rigidly attached to at least one of the first and second fuselage side walls, the PCB having a plurality of guide slots, each of the plurality of guide posts slideably seated in a respective one of the plurality of guide slots so that elastic deformation of the PCB is guided by the guide slots between the first and second fuselage side walls.

Claim (Index 5):
The system of  claim 1 , wherein a major longitudinal axis of each of the plurality of guide slots extends parallel to the major longitudinal axis of the frame.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 98.0
- Lexical Diversity: 2.21739
- Patent Class: 361.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15074236', '10976153', '13892358', '13974350', '15086386']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8289112124412337
- 35 USC 102 Novelty (BERT): 0.5354110795108461
- Combined Prediction Score: 0.7995611991481949
- Mean Citation Score: 176.112008
- Max Citation Score: 379.04257
- Similarity Product: 310.9750643231523

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