PATENT CLAIM ANALYSIS

Application Number: 15968786
Application Type: Utility
Filing Date: 2018-05
Publication Date: 2018-09
Patent Classification: ["244", "208000"]

Abstract:
Fluid systems are described herein. An example embodiment of a fluid system has a lengthwise axis, a chord length, a first body portion, a second body portion, a spacer, and a fluid pressurizer. The first body portion and the second body portion cooperatively define an injection opening, a suction opening, and a channel that extends from the injection opening to the suction opening. The fluid pressurizer is disposed within the channel cooperatively defined by the first body portion and the second body portion. The first body portion defines a cavity that is sized and configured to filter debris that enters the channel during use and provide a mechanism for removing the debris from the system.

Claim (Index 20):
A fluid system for an aircraft comprising:\n a first body portion having a leading edge, a trailing edge, a first intermediate edge, a second intermediate edge, and a main body defining a recess, an inner surface, a recess base, and a first opening, the first intermediate edge disposed between the leading edge and the second intermediate edge, the second intermediate edge disposed between the first intermediate edge and the trailing edge, the recess extending into the main body of the first body portion from the first opening to the recess base and forming the inner surface, the first opening extending from the first intermediate edge to the second intermediate edge; a second body portion attached to the first body portion and disposed within the recess defined by the main body of the first body portion, the first body portion and the second body portion cooperatively defining an injection opening, a suction opening, and a channel extending from the injection opening to the suction opening, the channel having a first portion extending from the suction opening toward the injection opening and a second portion extending from the injection opening toward the suction opening, the first body portion and the second body portion cooperatively defining the wing of said aircraft; a spacer moveable between a first position in which the spacer obstructs a portion of the injection opening and a second position in which the spacer does not obstruct the portion of the injection opening; and a fluid pressurizer disposed within the channel cooperatively defined by the first body portion and the second body portion and having a suction port directed toward the first portion of the channel and a discharge port directed toward the second portion of the channel.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 93.0
- Lexical Diversity: 2.22807
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15255523', '15426084', '15493654', '11804434', '12119193']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8722385722708765
- 35 USC 102 Novelty (BERT): 0.5624879482164183
- Combined Prediction Score: 0.8412635098654307
- Mean Citation Score: 258.170186
- Max Citation Score: 428.61304
- Similarity Product: 355.50736824986467

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

Dataset: test