Properties (64)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A design for an aircraft.
|
| gptkbp:applicationNumber |
29/123,456
|
| gptkbp:applicationType |
Design Patent
|
| gptkbp:assignee |
gptkb:ABC_Corporation
|
| gptkbp:assigneeCountry |
gptkb:USA
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:claims |
10
|
| gptkbp:classification |
B64C
|
| gptkbp:description |
This patent describes a new design for an aircraft.
|
| gptkbp:design |
Material Selection
Noise Reduction Performance Metrics Operational Efficiency Regulatory Compliance Structural Integrity Fuel Efficiency Wing Shape Winglets Cargo Capacity Emergency Systems Market Adaptability Engine Placement Aerodynamic Stability Stability Augmentation Fuselage Structure Maintenance Accessibility Communication_Systems Control_Systems Navigation_Systems Propulsion_Systems Flight_Control_Systems Safety_Systems Control_Surfaces Weight_Distribution Passenger_Comfort Landing_Gear_Systems Environmental_Control_Systems Avionics_Integration Cockpit_Layout Landing_Gear_Configuration |
| gptkbp:drawings |
Figures 1-5
|
| gptkbp:examiner |
Jane_Smith
|
| gptkbp:expirationDate |
2024-09-14
|
| gptkbp:fieldOfInvention |
Aerospace Engineering
|
| gptkbp:fieldOfUse |
Commercial Aviation
|
| gptkbp:filingDate |
2004-01-30
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,166 S-60
|
| gptkbp:internationalClassification |
B64C1/00
|
| gptkbp:inventor |
gptkb:John_Doe
|
| gptkbp:inventorCountry |
gptkb:USA
|
| gptkbp:issueDate |
2004-09-14
|
| gptkbp:legalStatus |
Active
|
| gptkbp:maintenanceFee |
Paid
|
| gptkbp:nonPatentCitation |
gptkb:Journal_of_Aerospace_Engineering
|
| gptkbp:patentCitation |
gptkb:US_5,678,901_A
|
| gptkbp:patentFamily |
US_6,789,166_S-60_Family
|
| gptkbp:patentNumber |
6,789,166
|
| gptkbp:priorityDate |
2003-01-30
|
| gptkbp:relatedPatent |
US_6,789,165_S-59
|
| gptkbp:status |
Granted
|
| gptkbp:technologyArea |
Aerodynamics
|
| gptkbp:title |
S-60_Aircraft_Design
|
| gptkbp:type |
Utility
|