Inventor

Michael G. McCaffrey

Inventor
Windsor, CT, US

Overview

140→
Patents
2009–2021
Patent span
Mechanical engineering
Primary field (CPC F)

Patents· 140 as inventor

Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.

F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines28%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants26%
Y02TClimate change mitigation technologies related to transportation15%
F02CGas-turbine plants7%
F04DNon-positive-displacement pumps4%
F16JPistons4%
Y10TTechnical subjects covered by former us classification3%
C04BLime, magnesia3%
B32BLayered products, i.e. products built-up of strata of flat or non-flat, e.g. cellular or honeycomb, form1%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers1%
PatentTitleYear
11,131,207Semi-autonomous rapid response active clearance control system202111,125,093Vane with L-shaped seal202111,118,468Retention clip for a blade outer air seal202111,111,805Multi-component assembled hydrostatic seal202111,047,245CMC component attachment pin202111,041,397Non-metallic side plate seal assembly for a gas turbine engine202111,021,971CMC blade with monolithic ceramic platform and dovetail202111,008,979Passive centrifugal bleed valve system for a gas turbine engine202111,002,195Intercooled cooling air with auxiliary compressor control202110,968,782Rotatable vanes202110,969,103Protective panel and frame therefor202110,941,673Multi-component assembled hydrostatic seal202110,934,941Air seal interface with AFT engagement features and active clearance control for a gas turbine engine202110,920,618Air seal interface with forward engagement features and active clearance control for a gas turbine engine202110,920,611Vented tangential on-board injector for a gas turbine engine202110,830,145Intercooled cooling air fleet management system202010,830,357Single crystal grain structure seals and method of forming202010,822,989Adjustable blade outer air seal apparatus202010,822,953Coolant flow redirection component202010,822,964Blade outer air seal with non-linear response202010,815,830Lightweight tierod202010,815,810BOAS assemblies with axial support pins202010,808,562Seal assembly for turbine engine component202010,808,554Method for making ceramic turbine engine article202010,801,349Ceramic matrix composite blade outer air seal202010,801,348Non-contacting dynamic seal202010,787,914CMC airfoil with monolithic ceramic core202010,774,666Toggle seal for a rim seal202010,753,222Gas turbine engine blade outer air seal202010,746,038Airfoil with airfoil piece having radial seal202010,738,643Boas segmented heat shield202010,731,498Blade outer air seal mount202010,724,387Continuation of a shear tube through a vane platform for structural support202010,697,321Vented tangential on-board injector for a gas turbine engine202010,677,079Airfoil with ceramic airfoil piece having internal cooling circuit202010,648,668Gas turbine engine ceramic component assembly and bonding material202010,612,466Gas turbine engine active clearance control system using inlet particle separator202010,598,046Support straps and method of assembly for gas turbine engine202010,590,780Engine component having support with intermediate layer202010,577,963Retention clip for a blade outer air seal202010,563,534Blade outer air seal with seal arc segment having secondary radial supports202010,563,531Seal assembly for gas turbine engine202010,513,943Boas enhanced heat transfer surface201910,507,515Ceramic core for component casting201910,502,060Rotor and gas turbine engine including same201910,458,249Bonded multi-piece gas turbine engine component201910,443,508Intercooled cooling air with auxiliary compressor control201910,443,423Gas turbine engine blade outer air seal assembly201910,443,616Blade outer air seal with centrally mounted seal arc segments201910,443,421Turbomachine blade assemblies201910,443,450Seal support structure for a circumferential seal of a gas turbine engine201910,443,424Turbine engine blade outer air seal with load-transmitting carriage201910,436,051Seal support structure201910,436,053Seal anti-rotation feature201910,436,070Blade outer air seal having angled retention hook201910,422,240Turbine engine blade outer air seal with load-transmitting cover plate201910,422,241Blade outer air seal support for a gas turbine engine201910,415,417Gas turbine engine active clearance control system201910,415,418System for modulating turbine blade tip clearance201910,415,419System for modulating turbine blade tip clearance201910,415,414Seal arc segment with anti-rotation feature201910,370,991Gas turbine engine and seal assembly therefore201910,364,706Meter plate for blade outer air seal201910,358,929Composite airfoil201910,352,183High temperature seal and method201910,344,612Compact advanced passive tip clearance control201910,337,346Blade outer air seal with flow guide manifold201910,323,534Blade outer air seal with cooling features201910,317,150Staged high temperature heat exchanger201910,309,243Grooved blade outer air seals201910,309,230Co-formed element with low conductivity layer201910,294,166Densified polymer infiltrated and pyrolysis-based CMC articles201910,280,782Segmented clearance control ring201910,280,784Adjustable blade outer air seal apparatus201910,233,763Seal assembly for turbine engine component201910,215,048Variable area vane arrangement for a turbine engine201910,202,863Seal ring for gas turbine engines201910,196,918Blade outer air seal made of ceramic matrix composite201910,189,219Method of fabricating a ceramic article201910,184,356Blade outer air seal support structure201910,174,624Composite blade root lay-up201910,161,258Boas rail shield201810,138,750Boas segmented heat shield201810,138,749Seal anti-rotation feature201810,132,184Boas spring loaded rail shield201810,107,129Blade outer air seal with spring centering201810,107,109Gas turbine engine component cooling assembly201810,094,232Self crystalline orientation for increased compliance201810,094,229Cooling system of a stator assembly for a gas turbine engine having a variable cooling flow mechanism and method of operation201810,077,670Blade outer air seal made of ceramic matrix composite201810,053,999Radial position control of case supported structure with axial reaction member201810,047,629Multi-segment adjustable stator vane for a variable area vane arrangement201810,036,264Variable area gas turbine engine component having movable spar and shell201810,036,281Mid turbine frame (MTF) for a gas turbine engine201810,024,173CMC blade with integral 3D woven platform20189,988,921Circumferential seal with seal dampening elements20189,970,310System and method for an assembled ring shroud20189,963,991Brush seal plate20189,957,821Gas turbine engine composite airfoil trailing edge20189,957,834Rotor blade tip clearance20189,957,830Hybrid passive and active tip clearance system20189,945,248Vented tangential on-board injector for a gas turbine engine20189,915,163'Cam-follower active clearance control'20189,890,645'Coolant flow redirection component'20189,879,557'Inner stage turbine seal for gas turbine engine'20189,803,559'Variable vane and seal arrangement'20179,725,833'Woven structure and method for weaving same'20179,587,504'Carrier interlock'20179,574,455'Blade outer air seal with cooling features'20179,505,145'Hybrid part made from monolithic ceramic skin and CMC core'20169,447,696'Blade outer air seal system for controlled tip clearance'20169,376,916'Assembled blade platform'20169,228,447'Adjustable blade outer air seal apparatus'20169,212,560'CMC blade with integral 3D woven platform'20159,200,536'Mid turbine frame (MTF) for a gas turbine engine'20159,200,530'Radial position control of case supported structure'20159,133,726'Seal for gas turbine engine component'20159,121,296'Rotatable component with controlled load interface'20159,103,214'Ceramic matrix composite vane structure with overwrap for a gas turbine engine'20158,967,961'Ceramic matrix composite airfoil structure with trailing edge support for a gas turbine engine'20158,943,796'Variable cycle turbine engine'20158,939,728'Hybrid part made from monolithic ceramic skin and CMC core'20158,920,127'Turbine rotor non-metallic blade attachment'20148,794,925'Root region of a blade for a gas turbine engine'20148,790,067'Blade clearance control using high-CTE and low-CTE ring members'20148,568,091'Gas turbine engine systems and methods involving blade outer air seals'20138,562,285'Angled on-board injector'20138,534,995'Turbine engine sealing arrangement'20138,408,874'Platformless turbine blade'20138,328,507'Knife edge seal assembly'20128,240,983'Gas turbine engine systems involving gear-driven variable vanes'20128,206,118'Airfoil attachment'20128,202,043'Gas turbine engines and related systems involving variable vanes'20128,105,019'3D contoured vane endwall for variable area turbine vane arrangement'20128,092,157'Variable turbine vane actuation mechanism having a bumper ring'20128,052,388'Gas turbine engine systems involving mechanically alterable vane throat areas'20118,029,234'Systems and methods involving aerodynamic struts'20118,007,229'Variable area turbine vane arrangement'20117,779,540'Apparatus and method for quadrail ergonomic assembly'20107,637,709'Safety interlock system for mechanical manipulators'2009

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

2009–2021Patents assigned to UNITED TECHNOLOGIES CORP (137)· patent assignee history
2009–2021Based in Windsor, CT, US· patent location history
2012–2019Patents assigned to MCCAFFREY MICHAEL G (28)· patent assignee history
2012–2015Patents assigned to HUDSON ERIC A (4)· patent assignee history
2016–2017Patents assigned to HASKO GREGORY H (2)· patent assignee history
2020–2021Patents assigned to RAYTHEON TECH CORP (33)· patent assignee history
2020Based in Windor, CT, US· patent location history

Inventor activity

Assignee and location history derived from the patent record.

Assignees
AssigneePatentsSpan
UNITED TECHNOLOGIES CORP1372009–2021
RAYTHEON TECH CORP332020–2021
MCCAFFREY MICHAEL Gself282012–2019
HUDSON ERIC A42012–2015
HASKO GREGORY H22016–2017
Locations
LocationPatentsSpan
Windsor, CT, US1392009–2021
Windor, CT, US12020