Inventor
Frank J. Zupanc
Inventor
Phoenix, AZ, US
Overview
Patents· 23 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F23Rprimary
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers48%
Y02TClimate change mitigation technologies related to transportation25%
F02CGas-turbine plants9%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants5%
F23DBurners5%
Y10TTechnical subjects covered by former us classification5%
F05BIndexing scheme relating to wind, spring, weight, inertia or like motors, to machines or engines for liquids covered by subclasses f03b, f03d and f03g2%
F16NLubricating2%
PatentTitleYear
9,897,320'Effusion cooled dual wall gas turbine combustors'20189,513,010'Gas turbine engine combustor with fluidic control of swirlers'20169,404,422'Gas turbine fuel injector having flow guide for receiving air flow'20168,616,004'Quench jet arrangement for annular rich-quench-lean gas turbine combustors'20138,584,466'Circumferentially varied quench jet arrangement for gas turbine combustors'20138,485,222'Systems and methods for preventing oil migration'20138,479,490'Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters'20138,171,740'Annular rich-quench-lean gas turbine combustors with plunged holes'20128,141,365'Plunged hole arrangement for annular rich-quench-lean gas turbine combustors'20128,127,554'Quench jet arrangement for annular rich-quench-lean gas turbine combustors'20127,966,821'Reduced exhaust emissions gas turbine engine combustor'20117,942,006'Combustors and combustion systems for gas turbine engines'20117,926,284'Quench jet arrangement for annular rich-quench-lean gas turbine combustors'20117,905,094'Combustor systems with liners having improved cooling hole patterns'20117,617,689'Combustor dome assembly including retaining ring'20097,546,737'Segmented effusion cooled gas turbine engine combustor'20097,506,512'Advanced effusion cooling schemes for combustor domes'20097,506,511'Reduced exhaust emissions gas turbine engine combustor'20097,500,364'System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines'20097,185,497'Rich quick mix combustion system'20077,065,972'Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions'20067,036,321'Auxiliary power unit having a rotary fuel slinger'20066,374,615'Low cost, low emissions natural gas combustor'2002Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2002Patents assigned to ALLIED SIGNAL INC (1)· patent assignee history
2002–2018Based in Phoenix, AZ, US· patent location history
2006–2018Patents assigned to HONEYWELL INT INC (22)· patent assignee history
2012–2018Patents assigned to BRONSON THOMAS J (5)· patent assignee history
2012–2013Patents assigned to ZUPANC FRANK J (5)· patent assignee history
2012–2018Patents assigned to ZUPANC FRANK JOSEPH (3)· patent assignee history
2016Based in Fountain Hills, AZ, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| HONEYWELL INT INC | 22 | 2006–2018 |
| BRONSON THOMAS J | 5 | 2012–2018 |
| ZUPANC FRANK Jself | 5 | 2012–2013 |
| ZUPANC FRANK JOSEPHself | 3 | 2012–2018 |
| ALLIED SIGNAL INC | 1 | 2002 |
Locations
| Location | Patents | Span |
|---|---|---|
| Phoenix, AZ, US | 21 | 2002–2018 |
| Fountain Hills, AZ, US | 2 | 2016 |