PATENT CLAIM ANALYSIS

Application Number: 16063250
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-12
Patent Classification: ["156", "245000"]

Abstract:
A process for manufacturing an apron board of a high-speed rail equipment cabin using a composite material is disclosed. The material includes aramid fiber honeycomb, PET foam,  3 K twill carbon fiber flame retardant prepreg, unidirectional carbon fiber flame retardant prepreg, glass fiber flame retardant prepreg, aramid flame retardant prepreg, and 300 g/m 2  single component medium temperature curing blue epoxy adhesive. The process includes manufacturing an apron main plate ( 3 ); manufacturing apron-board trim strips ( 1, 2 ), wherein there are two apron-board trim strips ( 1 ) and two apron-board trim strips ( 2 ); and obtaining the apron board through the apron main plate ( 3 ) and the apron-board trim strips ( 1, 2 ), wherein the two apron-board trim strips ( 1 ) are respectively stuck at two opposite sides of the apron main plate ( 3 ), the two apron-board trim strips ( 2 ) are respectively stuck at another two opposite sides of the apron main plate ( 3 ).

Claim (Index 2):
The process for manufacturing the apron board of the high-speed rail equipment cabin using the composite material, as recited in  claim 1 , wherein the step of manufacturing the apron main plate comprises closely pasting multiple layers of raw materials to a mold cavity in sequence from outside to inside in a form of lamination, wherein the multiple layers of raw materials are:\n 1 layer of 198-200 g/m 2  3K twill carbon fiber flame retardant prepreg; 5-8 layers of 300-315 g/m 2  glass fiber flame retardant prepreg; 2 layers of 235-240 g/m 2  aramid flame retardant prepreg; 2 layers of 100-150 g/m 2  unidirectional carbon fiber flame retardant prepreg; 1 layer of 300 g/m 2  single component medium temperature curing blue epoxy adhesive; 2 layers of the 100-150 g/m 2  unidirectional carbon fiber flame retardant prepreg; 1 piece of aramid fiber honeycomb with a thickness of 16.4 mm; 1 layer of the 100-150 g/m 2  unidirectional carbon fiber flame retardant prepreg; 1 layer of 300 g/m 2  single component medium temperature curing blue epoxy adhesive; 2 layers of 100-150 g/m 2  unidirectional carbon fiber flame retardant prepreg; 4 layers of 300-315 g/m 2  glass fiber flame retardant prepreg; and 1 layer of 198-200 g/m 2  3K twill carbon fiber flame retardant prepreg, and then shaping the apron main plate through a hot press machine with a temperature of 130-150\u00b0 C., a molding time of 3600-3800 s, and a pressure of 4 MPa-6 MPa.

Metadata:
- Claim Count in Document: 9.0
- Percentile: 94.0
- Lexical Diversity: 2.64286
- Patent Class: 156.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['16063252', '15036097', '12811135', '12453029', '15562544']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.9001981433951847
- 35 USC 102 Novelty (BERT): 0.584480343998607
- Combined Prediction Score: 0.8686263634555269
- Mean Citation Score: 257.748186
- Max Citation Score: 481.80508
- Similarity Product: 449.5390577437258

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