Log in
Enquire now
‌

US Patent 10113561 Secondary flow baffle for turbomachinery

Patent 10113561 was granted and assigned to Pratt & Whitney on October, 2018 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributors

Contents

Is a
Patent
Patent
0

Patent attributes

Current Assignee
Pratt & Whitney
Pratt & Whitney
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
101135610
Patent Inventor Names
Jordan T. Wall0
Victor G. Filipenco0
Date of Patent
October 30, 2018
0
Patent Application Number
151535780
Date Filed
May 12, 2016
0
Patent Citations Received
‌
US Patent 11428104 Partition arrangement for gas turbine engine and method
Patent Primary Examiner
‌
Ninh H. Nguyen
0
Patent abstract

A stage of a fan for a gas turbine engine may include a rotor blade and a stator vane disposed aft of the rotor blade. A baffle may be coupled to the stator vane. The baffle may define a secondary airflow path from aft of the stator vane to forward of the rotor blade. The baffle may further define the secondary airflow path from aft of the stator vane to forward of the stator vane.

Timeline

No Timeline data yet.

Further Resources

Title
Author
Link
Type
Date
No Further Resources data yet.

References

Find more entities like US Patent 10113561 Secondary flow baffle for turbomachinery

Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
Open Query Tool
Access by API
Golden Query Tool
Golden logo

Company

  • Home
  • Press & Media
  • Blog
  • Careers
  • WE'RE HIRING

Products

  • Knowledge Graph
  • Query Tool
  • Data Requests
  • Knowledge Storage
  • API
  • Pricing
  • Enterprise
  • ChatGPT Plugin

Legal

  • Terms of Service
  • Enterprise Terms of Service
  • Privacy Policy

Help

  • Help center
  • API Documentation
  • Contact Us
By using this site, you agree to our Terms of Service.