Schaufelstrebenpositionierungs- und -Sicherungssysteme
Anmelder: United Technologies Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3093442
- Aktenzeichen
- EP16160455
- Anmeldetag
- 15. März 2016
- Veröffentlichung
- 10. Oktober 2018
- Erteilung
- 10. Oktober 2018
- Rechtsraum
- EP
- IPC
- F01D9/04F01D17/16
Abstract
A strut-flap vane system for a turbomachine includes a vane strut (211) comprising an airfoil portion (211 b) and a strut mount (211a) extending in a radially outward direction from the airfoil portion. The strut mount forms a hollow semi-cylinder and includes threading (211 c) on an outer diameter thereof. The system includes an aft mount portion or portions (201) defining a hollow semi-cylinder configured to form a strut cylinder (203) with the strut mount such that the aft mount portion can be disposed in contact with the strut mount to form the strut cylinder. The strut cylinder defines a cylinder opening (205) and the aft mount portion includes threading (201 c) on an outer diameter thereof that aligns with the threading of the strut mount to allow a strut spanner nut (207) to mesh with both the strut mount and the mount portion. Furthermore, a method of assembling is disclosed.
Anmelder
- Firma
- United Technologies Corporation
- Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrt- sowie Verteidigungskonzern, entstanden aus Raytheon und United Technologies. Entwickelt und fertigt Triebwerke, Avionik, Radarsysteme, Raketen- und Verteidigungstechnik für zivile und militärische Kunden.
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