Abschaltwelle für einen Integrierten Antriebsgenerator
Anmelder: Hamilton Sundstrand Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3081824
- Aktenzeichen
- EP16164751
- Anmeldetag
- 11. April 2016
- Veröffentlichung
- 22. April 2020
- Erteilung
- 22. April 2020
- Rechtsraum
- EP
- IPC
- F16D1/02F16D11/14F16C3/02
Abstract
A disconnect shaft 50 of an integrated drive generator is provided including a body 52 configured to rotate about an axis of rotation. The body 52 has a first end 54, a second opposite end 56, and a plurality of teeth 58 formed adjacent the first end and configured to engage a complementary portion of an adjacent component. A relief 60 is formed in the body 52 such that a first portion 62 is defined between the relief 60 and the plurality of teeth 58. The first portion 62 includes a plurality of threads having at least one of a major diameter between about 1.3044 and about 1.3125 inches (3.313-3.334 centimeters), a minor diameter between about 1.2482 and about 1.2547 inches (3.170- 3.187 centimeters), a pitch diameter between about 1.2765 and about 1.2800 inches (3.242-3.251 centimeters), and a root radius between about .0075 and .0090 inches (.0190-.0029 centimeters).
Anmelder
- Firma
- Hamilton Sundstrand Corporation
- Land
- 🇺🇸 USA
US-amerikanisches Unternehmen der Luft- und Raumfahrtindustrie, das Flugzeugsysteme wie Umweltkontroll-, Energie- und Antriebssysteme entwickelt; heute Teil von Collins Aerospace innerhalb von RTX.
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