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Inventor profile of:

Anthony R. Bifulco

City:

Ellington, Connecticut

Country:

United States

Published Applications:

58

Last publication date:

2026-06-11

Top Assignees for applications by Anthony R. Bifulco

The entities that hold a legal rights for patent applications filed by inventor Bifulco Anthony R.:

Recent patent applications by Bifulco Anthony R.

Anthony R. Bifulco from Ellington, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-06-11
US20260162638A1
Physics

ACOUSTIC ATTENUATION STRUCTURES

 #2 | 2025-05-15
US20250154896A1
Mechanical engineering

AIRCRAFT ENGINE ENTRAINED PARTICLE SEPARATION SYSTEM AND METHOD

 #3 | 2025-03-20
US20250092826A1
Mechanical engineering

CORE COMPARTMENT VENT DURING ENGINE SHUTDOWN TO REDUCED BOWED ROTOR START

 #4 | 2025-02-20
US20250059915A1
Mechanical engineering

GAS TURBINE ENGINE WITH CORE DEBRIS PROTECTION

 #5 | 2024-09-05
US20240295178A1
Mechanical engineering

BOWED ROTOR START REDUCTION VIA INTERNAL COOLING

 #6 | 2024-08-29
US20240287935A1
Mechanical engineering

Core compartment vent during engine shutdown to reduced bowed rotor start

 #7 | 2024-08-22
US20240280050A1
Mechanical engineering

GAS TURBINE ENGINE WITH BLEED DIFFUSER BAFFLES

 #8 | 2024-08-01
US20240255056A1
Mechanical engineering

Non-metallic engine case inlet compression seal for a gas turbine engine

 #9 | 2024-03-28
US20240105154A1
Physics

Acoustic attenuation structures

 #10 | 2023-11-02
US20230349330A1
Mechanical engineering

Face sheet of acoustic liner having streamlined holes with elongated edges

 #11 | 2023-05-18
US20230151777A1
Mechanical engineering

RADIAL STRUT FRAME CONNECTION BETWEEN FAN CASE AND CORE HOUSING IN A GAS TURBINE ENGINE

 #12 | 2023-05-18
US20230151742A1
Mechanical engineering

H-frame connection between fan case and core housing in a gas turbine engine

 #13 | 2023-05-18
US20230151741A1
Mechanical engineering

Triangular-frame connection between fan case and core housing in a gas turbine engine

 #14 | 2023-04-27
US20230127925A1
Mechanical engineering

Frame connection between fan case and core housing in a gas turbine engine

 #15 | 2023-04-06
US20230103861A1
Mechanical engineering

Gas turbine engine with acoustic liner

 #16 | 2023-03-21
US17701026
Mechanical engineering

Radial strut frame connection between fan case and core housing in a gas turbine engine

 #17 | 2023-01-17
US17407275
Mechanical engineering

Frame connection between fan case and core housing in a gas turbine engine

 #18 | 2022-07-14
US20220221056A1
Mechanical engineering

Non-metallic engine case inlet compression seal for a gas turbine engine

 #19 | 2022-03-17
US20220084493A1
Physics

Acoustic attenuation structures

 #20 | 2022-02-17
US20220049621A1
Mechanical engineering

Passive transpirational flow acoustically lined guide vane

 #21 | 2022-01-13
US20220010731A1
Mechanical engineering

Acoustically treated panels

 #22 | 2021-10-21
US20210324748A1
Mechanical engineering

Composite reinforced rotor

 #23 | 2021-10-14
US20210317785A1
Mechanical engineering

COOLING SYSTEM FOR A GAS TURBINE ENGINE

 #24 | 2021-09-09
US20210277829A1
Mechanical engineering

Acoustic liner with non-uniform volumetric distribution

 #25 | 2021-08-19
US20210254500A1
Mechanical engineering

Borescope port engine fluid wash

 #26 | 2020-11-05
US20200347785A1
Mechanical engineering

Acoustic liner with obliquely angled slots

 #27 | 2020-06-25
US20200200031A1
Mechanical engineering

Stator outer platform sealing and retainer

 #28 | 2020-01-23
US20200025080A1
Mechanical engineering

Diversion of fan air to provide cooling air for gas turbine engine

 #29 | 2019-07-11
US20190211881A1
Mechanical engineering

Assembly alignment handling damage tolerant spline

 #30 | 2019-07-11
US20190211839A1
Mechanical engineering

Assembly for releasable locking of a spinner or nosecone to an engine structure

 #31 | 2019-06-27
US20190195082A1
Mechanical engineering

Bleed valve system

 #32 | 2019-05-02
US20190128274A1
Mechanical engineering

Stator segment circumferential gap seal

 #33 | 2019-03-28
US20190093492A1
Mechanical engineering

Non-metallic engine case inlet compression seal for a gas turbine engine

 #34 | 2018-07-19
US20180202449A1
Mechanical engineering

Stator outer platform sealing and retainer

 #35 | 2018-07-19
US20180202359A1
Mechanical engineering

Lock for threaded in place nosecone or spinner

 #36 | 2018-02-15
US20180045138A1
Mechanical engineering

Nose cone assembly and method of circulating air in a gas turbine engine

 #37 | 2017-10-12
US20170292400A1
Mechanical engineering

Method and apparatus for adjusting variable vanes

 #38 | 2017-09-28
US20170276018A1
Mechanical engineering

Geared unison ring for variable vane actuation

 #39 | 2017-01-05
US20170002834A1
Mechanical engineering

COOLED COMPRESSOR

 #40 | 2016-09-22
US20160273373A1
Mechanical engineering

Multi-element inner shroud extension for a turbo-machine

 #41 | 2016-09-08
US20160258359A1
Mechanical engineering

Diversion of fan air to provide cooling air for gas turbine engine

 #42 | 2016-08-04
US20160222982A1
Mechanical engineering

Fluid injector for cooling a gas turbine engine component

 #43 | 2016-06-02
US20160153463A1
Mechanical engineering

Fiber reinforced spacer for a gas turbine engine

 #44 | 2016-05-26
US20160146030A1
Mechanical engineering

Non-metallic engine case inlet compression seal for a gas turbine engine

 #45 | 2016-05-26
US20160146023A1
Mechanical engineering

Rotor with blades secured by woven fiber attachment system

 #46 | 2016-05-19
US20160138399A1
Mechanical engineering

Reinforced gas turbine engine rotor disk

 #47 | 2015-10-08
US20150285147A1
Mechanical engineering

Cooling system with a bearing compartment bypass

 #48 | 2015-09-03
US20150247461A1
Mechanical engineering

GEARED TURBOFAN WITH HIGH FAN ROTOR POWER INTENSITY

 #49 | 2015-08-06
US20150218955A1
Mechanical engineering

Complaint cantilevered airfoil

 #50 | 2014-11-27
US20140345294A1
Mechanical engineering

Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events

 #51 | 2014-09-04
US20140248140A1
Mechanical engineering

Shiplap cantilevered stator

 #52 | 2014-05-29
US20140144151A1
Mechanical engineering

Engine Compressor Wash System

 #53 | 2013-01-10
US20130008144A1
Mechanical engineering

Efficient, low pressure ratio propulsor for gas turbine engines

 #54 | 2012-07-05
US20120171029A1
Mechanical engineering

Turbine engine rotating cavity anti-vortex cascade

 #55 | 2012-03-22
US20120070271A1
Mechanical engineering

GAS TURBINE ENGINE WITH BLEED DUCT FOR MINIMUM REDUCTION OF BLEED FLOW AND MINIMUM REJECTION OF HAIL DURING HAIL INGESTION EVENTS

 #56 | 2010-10-21
US20100266401A1
Mechanical engineering

Turbine engine rotating cavity anti-vortex cascade

 #57 | 2010-05-20
US20100124495A1
Mechanical engineering

Turbine engine rotor hub

 #58 | 2005-04-26
US10261471
-

Shim lock/pin anti-rotation bumper design
InventorID:

19799 ⎘