Patents

US 12735186 B2: Systems and methods for an ice runback control zone in an electrothermal ice protection system

Granted
2026-09-15
Filed
2024-06-13 application 18742128
Type
Utility · 8 claims
Elsewhere
Google Patents ↗ · USPTO patent document ↗ · USPTO Patent Center record ↗

Abstract

An aircraft wing may comprise an airfoil having deicing zone, an anti-icing zone, and an ice runback control zone. An aircraft wing may comprise an electro-thermal ice protection system disposed in the aircraft wing. The electro-thermal ice protection system may be disposed along the deicing, anti-icing, and ice runback control zones of the airfoil to improve aerodynamic performance of the aircraft and reduce ice formation along the wings of the aircraft.

Source: PTBLXML, file of 2026-09-15 (ipgb20260915.xml).

Assignees

AssigneeTypePlaceAlso on furp.orgSource
Goodrich Corporation 1,817 patentsUS company or organizationCharlotte, NCPTBLXML, file of 2026-09-15

Inventors

InventorPlacePatentsPerson pageSource
Brandon HeinKent, OH9PTBLXML, file of 2026-09-15
Casey M. SlaneTallmadge, OHPTBLXML, file of 2026-09-15
Galdemir C. BoturaCopley, OHPTBLXML, file of 2026-09-15

CPC categories

SubclassCategoryFirst groupSource
B64DEquipment for fitting in or to aircraft; flight suits; parachutes; arrangement or mounting of power plants or propulsion transmissions in aircraftB64D15/14PTBLXML, file of 2026-09-15

Cooperative Patent Classification, as currently assigned (one row per subclass).

Assignments and security interests

No recorded assignments or security interests on file for this patent.

USPTO bulk data: PatentsView granted patents, disambiguated (PVGPATDIS) for patents, assignees, inventors, places and CPC categories; the USPTO Patent Assignment Dataset (ECORSEXC) for assignments and security interests. Patents filed in the last 20 years. No claims or full text. Links to other records are by name (and state): EXACT means the identical full name and state; FUZZY means a looser name match, with the confidence shown.