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Inventor profile of:

Jon E. Sobanski

City:

Glastonbury, Connecticut

Country:

United States

Published Applications:

74

Last publication date:

2026-05-21

Top Assignees for applications by Jon E. Sobanski

The entities that hold a legal rights for patent applications filed by inventor Sobanski Jon E.:

Recent patent applications by Sobanski Jon E.

Jon E. Sobanski from Glastonbury, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-05-21
US20260139604A1
Mechanical engineering

VANE WITH PIN MOUNT AND ANTI-ROTATION

 #2 | 2026-04-30
US20260116570A1
Performing operations; transporting

AIRCRAFT WITH SYMMETRIC OPEN PROPULSOR ROTATING PATTERNS

 #3 | 2026-04-30
US20260116569A1
Performing operations; transporting

AIRCRAFT WITH SYMMETRIC OPEN PROPULSOR ROTATING PATTERNS

 #4 | 2026-04-02
US20260092556A1
Mechanical engineering

OPEN ROTOR PROPULSION SYSTEM WITH FORWARD EXHAUST OUTLET(S)

 #5 | 2026-04-02
US20260091873A1
Performing operations; transporting

OPEN ROTOR PROPULSION SYSTEM WITH EXHAUST MIXER(S)

 #6 | 2026-03-05
US20260062117A1
Performing operations; transporting

ADJUSTING PITCH FOR AIRFOILS OF AN AIRCRAFT PROPULSION SYSTEM

 #7 | 2026-01-15
US20260015968A1
Mechanical engineering

OPEN ROTOR WITH AERODYNAMICALLY ISOLATABLE FREE TURBINE

 #8 | 2026-01-15
US20260015098A1
Performing operations; transporting

Differential Driven Open Rotor with Brake

 #9 | 2025-12-04
US20250369825A1
Physics

ACTUATABLE INSPECTION PROBE FOR NON-DESTRUCTIVE INSPECTION

 #10 | 2025-09-04
US20250277472A1
Mechanical engineering

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH BYPASS FLOWPATH

 #11 | 2025-09-02
US18594936
Mechanical engineering

Open rotor aircraft propulsion system with bypass flowpath

 #12 | 2025-07-08
US18778489
Mechanical engineering

Open rotor variable pitch blade with retracting inboard trailing edge

 #13 | 2025-06-19
US20250197013A1
Performing operations; transporting

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH ANTI-ICING SYSTEM

 #14 | 2025-01-09
US20250012213A1
Mechanical engineering

AIRCRAFT PROPULSION SYSTEM ENGINE WITH MULTIPLE INDEPENDENT ROTATING STRUCTURES

 #15 | 2024-12-26
US20240426245A1
Mechanical engineering

WATER ACTUATED TIP CLEARANCE CONTROL SYSTEM FOR TURBINE ENGINE

 #16 | 2024-12-10
US18243456
Mechanical engineering

Selectable inlet for aircraft propulsion system heat exchanger

 #17 | 2024-11-21
US20240384659A1
Mechanical engineering

Axially offset vane arrays in turbine engine bypass

 #18 | 2024-11-14
US20240376834A1
Mechanical engineering

SUPPORTING ELONGATED ROTATING ASSEMBLY WITHIN A TURBINE ENGINE

 #19 | 2024-09-12
US20240302101A1
Mechanical engineering

HEAT EXCHANGER WITH CROSSING HEAT EXCHANGE TUBES

 #20 | 2024-09-12
US20240301830A1
Mechanical engineering

Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products

 #21 | 2024-09-12
US20240301823A1
Mechanical engineering

Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products

 #22 | 2024-09-12
US20240301808A1
Mechanical engineering

Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products

 #23 | 2024-08-15
US20240271881A1
Mechanical engineering

TUBE HEAT EXCHANGER WITH VARYING DIAMETERS

 #24 | 2024-07-16
US18213654
Mechanical engineering

Aircraft powerplant water and/or heat energy recovery system with water treatment device

 #25 | 2024-06-18
US18199767
Mechanical engineering

Water separator for turbine engine

 #26 | 2024-06-06
US20240183276A1
Mechanical engineering

AIRFOIL ASSEMBLY WITH FIBER-REINFORCED COMPOSITE RINGS

 #27 | 2024-06-04
US18119169
Mechanical engineering

Heat exchanger(s) for recovering water and/or heat energy from turbine engine combustion products

 #28 | 2024-05-02
US20240141837A1
Mechanical engineering

REVERSE FLOW HYDROGEN STEAM INJECTED TURBINE ENGINE

 #29 | 2024-01-18
US20240018875A1
Mechanical engineering

Vane with pin mount and anti-rotation

 #30 | 2024-01-18
US20240018871A1
Mechanical engineering

Airfoil assembly with fiber-reinforced composite rings and toothed exit slot

 #31 | 2023-08-03
US20230243303A1
Mechanical engineering

Off-set duct heat exchanger

 #32 | 2023-08-03
US20230242267A1
Performing operations; transporting

Boundary layer ducted fan propulsion system

 #33 | 2023-07-27
US20230235699A1
Mechanical engineering

Aircraft skin heat exchanger

 #34 | 2023-05-25
US20230159175A1
Performing operations; transporting

Aircraft propulsor and method for using said propulsor

 #35 | 2023-04-27
US20230130242A1
Mechanical engineering

Vane arc segment with flange and gusset

 #36 | 2023-03-09
US20230076312A1
Mechanical engineering

Multi-direction hole for rail effusion

 #37 | 2023-02-16
US20230053047A1
Mechanical engineering

Two-piece baffle

 #38 | 2023-01-19
US20230020644A1
Mechanical engineering

Airfoil assembly with fiber-reinforced composite rings and toothed exit slot

 #39 | 2023-01-10
US17832256
Mechanical engineering

Airfoil assembly with composite rings and sealing shelf

 #40 | 2022-10-06
US20220316350A1
Mechanical engineering

Vane arc segment with flange and gusset

 #41 | 2022-09-29
US20220307378A1
Mechanical engineering

Airfoil assembly with fiber-reinforced composite rings

 #42 | 2022-09-29
US20220307374A1
Mechanical engineering

Vane arc segment with flange having step

 #43 | 2022-09-08
US20220282628A1
Mechanical engineering

Vane arc segment with radially projecting flanges

 #44 | 2022-07-21
US20220228509A1
Mechanical engineering

Vane arc segment support platform with curved radial channel

 #45 | 2022-07-21
US20220228500A1
Mechanical engineering

Vane with pin mount and anti-rotation

 #46 | 2022-07-21
US20220228499A1
Mechanical engineering

Vane with pin mount and anti-rotation stabilizer rod

 #47 | 2022-07-19
US17193343
Mechanical engineering

Vane arc segment with seal

 #48 | 2022-06-28
US17213705
Mechanical engineering

Vane with pin mount and anti-rotation baffle

 #49 | 2022-06-23
US20220195874A1
Mechanical engineering

Vane with baffle and recessed spar

 #50 | 2022-06-16
US20220186620A1
Mechanical engineering

Spar with embedded plenum passage

 #51 | 2022-05-19
US20220154587A1
Mechanical engineering

Vane arc segment with curved radial flange

 #52 | 2022-04-12
US17191121
Mechanical engineering

Vane arc segment having spar with pin fairing

 #53 | 2022-03-17
US20220082256A1
Mechanical engineering

Aerodynamic component for a gas turbine engine

 #54 | 2022-03-17
US20220082024A1
Mechanical engineering

CMC vane with support spar and baffle

 #55 | 2022-03-01
US17034200
Mechanical engineering

Vane having rib aligned with aerodynamic load vector

 #56 | 2021-12-30
US20210404659A1
Mechanical engineering

Multi-direction hole for rail effusion

 #57 | 2021-11-18
US20210355834A1
Mechanical engineering

Airfoil vane with coated jumper tube

 #58 | 2021-10-14
US20210317786A1
Mechanical engineering

VANE SUPPORT SYSTEM

 #59 | 2021-10-14
US20210317748A1
Mechanical engineering

Vane support system with seal

 #60 | 2021-08-12
US20210246808A1
Mechanical engineering

Vane arc segment load path

 #61 | 2021-08-12
US20210246788A1
Mechanical engineering

Vane arc segment platform flange with cap

 #62 | 2021-05-13
US20210140320A1
Mechanical engineering

Two-piece baffle

 #63 | 2021-05-06
US20210131296A1
Mechanical engineering

Vane with chevron face

 #64 | 2021-04-08
US20210102469A1
Mechanical engineering

CMC vane mate face flange

 #65 | 2020-10-15
US20200326072A1
Mechanical engineering

Combustor heat shield panel

 #66 | 2020-09-24
US20200300469A1
Mechanical engineering

AERODYNAMIC COMPONENT FOR A GAS TURBINE ENGINE

 #67 | 2020-09-24
US20200298302A1
Performing operations; transporting

Investment casting method including forming of investment casting core

 #68 | 2020-06-25
US20200200386A1
Mechanical engineering

Diffusing hole for rail effusion

 #69 | 2020-02-06
US20200041132A1
Mechanical engineering

Tapered panel rail

 #70 | 2020-01-02
US20200003165A1
Mechanical engineering

Electrostatic flame control technology

 #71 | 2019-08-22
US20190257248A1
Mechanical engineering

Gas turbine combustor heat shield panel having multi-direction hole for rail effusion cooling

 #72 | 2019-08-08
US20190242580A1
Mechanical engineering

Undercut combustor panel rail

 #73 | 2019-08-08
US20190242579A1
Mechanical engineering

Pull-plane effusion combustor panel

 #74 | 2019-05-30
US20190162134A1
Mechanical engineering

RETENTION OF A NOZZLE ASSEMBLY FOR AN ENGINE
InventorID:

2515102 ⎘