Reconstructive options following orbital exenteration

dc.contributor.authorYesensky, Jessica
dc.contributor.authorLebo, Nicole
dc.contributor.departmentOtolaryngology -- Head and Neck Surgery, School of Medicineen_US
dc.date.accessioned2022-01-20T17:22:46Z
dc.date.available2022-01-20T17:22:46Z
dc.date.issued2020-10
dc.description.abstractPurpose of review The purpose of this review is to examine current trends in reconstruction following orbital exenteration. Defects ranging from isolated exenteration to more complex midface resections are explored. Recent findings Goals of reconstruction include separating the sino-orbital cavities and creating a safe, stable wound that can withstand adjuvant radiation. When planning for orbital rehabilitation, it is important to create a concave cavity that can accommodate a prosthesis. This is primarily achieved through secondary granulation or split-thickness skin grafts. Recently, the use of dermal allografts has been investigated and shown good success with epithelization of the orbital cavity. For complex orbitomaxillectomy defects, musculocutaneous free tissue flaps remain the mainstay for reconstruction. Summary Reconstructive options following orbital exenteration are based on extent of the defect, need for postoperative radiation, and plans for orbital rehabilitation with prosthesis.en_US
dc.eprint.versionAuthor's manuscripten_US
dc.identifier.citationYesensky, J., & Lebo, N. (2020). Reconstructive options following orbital exenteration. Current Opinion in Otolaryngology & Head and Neck Surgery, 28(5), 352–354. https://doi.org/10.1097/MOO.0000000000000662en_US
dc.identifier.urihttps://hdl.handle.net/1805/27493
dc.language.isoenen_US
dc.publisherWolters Kluweren_US
dc.relation.isversionof10.1097/MOO.0000000000000662en_US
dc.relation.journalCurrent Opinion in Otolaryngology & Head and Neck Surgeryen_US
dc.rightsPublisher Policyen_US
dc.sourceAuthoren_US
dc.subjectorbital exenterationen_US
dc.subjectreconstructionen_US
dc.subjectsurgical resectionsen_US
dc.titleReconstructive options following orbital exenterationen_US
dc.typeArticleen_US
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