Teilweise Eingelassene Periodische Rippenstrukturen

EP3782905 Art B1 11. Juni 2025

Anmelder: Lockheed Martin Corporation 🇺🇸

Details

Veröffentlichungs-Nr.
EP3782905
Aktenzeichen
EP20190584
Anmeldetag
11. August 2020
Veröffentlichung
11. Juni 2025
Erteilung
11. Juni 2025
Rechtsraum
EP
IPC
B64C21/10F15D1/00
Offizieller Volltext

Abstract

In one embodiment, a method for reducing drag includes forming a smooth surface (130) on a first portion (120) of a physical object (100). The method also includes forming periodic riblets (110) on a second portion (130) of the physical object (100). The method further includes generating a flow over the periodic riblets (110) of the second portion (130) of the physical object (100) and over the smooth surface (130) of the first portion (120) of the physical object (100). The second portion (130) of the physical object (100) is adjacent to the first portion (120) of the physical object (100). Each peak of each riblet (110) of the periodic riblets (110) of the second portion (130) of the physical object (100) is located above a plane of the smooth surface (130) of the first portion (120) of the physical object (100). Each valley between adjacent riblets of the periodic riblets (110) of the second portion (130) of the physical object (100) is located below the plane of the smooth surface (130) of the first portion (120) of the physical object (100). A length of each riblet (110) of the periodic riblets (110) runs parallel to a direction of the flow.

Anmelder

Firma
Lockheed Martin Corporation
Land
🇺🇸 USA
🇺🇸 Lockheed Martin

US-amerikanischer Luft- und Raumfahrt- sowie Rüstungskonzern mit Sitz in Maryland, tätig in Entwicklung von Kampfflugzeugen, Raketensystemen, Satelliten und Verteidigungstechnik.

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