PATENT CLAIM ANALYSIS

Application Number: 16137368
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2019-01
Patent Classification: ["244", "118100"]

Abstract:
Particular embodiments include a non-dedicated, temporarily installed, airborne special mission payload mounting system comprising a pressurized door plug assembly installed in an opening on the side of an aircraft fuselage. A rotationally-actuated strut extends from a first end connected to an interior of the aircraft fuselage, through the pressurized door plug assembly, to a second end of the strut connected to one or more payloads. The rotational axis of the strut is exterior to the aircraft fuselage.

Claim (Index 9):
The apparatus of  claim 7 , further comprising a shoulder armature assembly coupled to the first end of the strut, wherein the strut is coupled to the AMS plate via the shoulder armature assembly.

Metadata:
- Claim Count in Document: 15.0
- Percentile: 97.0
- Lexical Diversity: 1.68
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15692903', '15265681', '14150710', '12734159', '15658277']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8836978614780798
- 35 USC 102 Novelty (BERT): 0.5943441841397377
- Combined Prediction Score: 0.8547624937442456
- Mean Citation Score: 494.592814
- Max Citation Score: 552.86896
- Similarity Product: 465.05286876995086

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