Grenzschichtaufnahmegebläsesystem
Anmelder: Rolls-Royce plc 🇬🇧
Details
- Veröffentlichungs-Nr.
- EP3653513
- Aktenzeichen
- EP19204336
- Anmeldetag
- 21. Oktober 2019
- Veröffentlichung
- 1. Dezember 2021
- Erteilung
- 1. Dezember 2021
- Rechtsraum
- EP
- IPC
- B64D33/02// B64D27/14B64D27/24B64D29/04B64D27/02F01D5/14F02K3/00
Abstract
A boundary layer ingestion fan system for location aft of the fuselage of an aircraft is shown. It comprises a nacelle (501) defining a duct (502), and a fan (503) located within the duct. The fan comprises a hub arranged to rotate around a rotational axis and a plurality of blades attached to the hub, each of which has a span from a root at the hub defining a 0 percent span position (r<sub>hub</sub>) to a tip defining a 100 percent span position (r<sub>tip</sub>) and a plurality of span positions therebetween (r ∈ [r<sub>hub</sub>, r<sub>tip</sub>]). A plurality of outlet guide vanes are positioned aft of the fan. An afterbody is located aft of the plurality of outlet guide vanes and which tapers to an apex having an apex angle with respect to the rotational axis of between 35 and 45 degrees.
Anmelder
- Firma
- Rolls-Royce plc
- Land
- 🇬🇧 Großbritannien
Britisches Unternehmen mit Sitz in Derby, das Flugzeugtriebwerke sowie Antriebssysteme für Luftfahrt, Marine und Energieerzeugung entwickelt und herstellt.
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Rolls-Royce plc
Rolls-Royce plc · Derby