Faseroptische Gyroskop(fog)-Anordnung
Anmelder: Northrop Grumman Systems Corporation 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3736533
- Aktenzeichen
- EP20172886
- Anmeldetag
- 5. Mai 2020
- Veröffentlichung
- 1. März 2023
- Erteilung
- 1. März 2023
- Rechtsraum
- EP
- IPC
- G01C19/72
Abstract
One example includes a FOG assembly including a spool that includes a flattened portion corresponding to a flange comprising an axial center corresponding to a sensitive axis about which an associated FOG system is configured to measure rotation. The FOG assembly also includes a magnetic shield arranged as a capped concentric cover about the sensitive axis and coupled to the spool and the flange to create a toroidal cavity between the magnetic shield and the flange. A fiber coil is disposed within the toroidal cavity and coupled to the flange. The fiber coil includes an optical fiber which is counter-wound in first and second orientations. The fiber coil has an axial dimension along the sensitive axis that is less than or equal to approximately 160% of a radial width corresponding to a difference between an outer radius and an inner radius of the fiber coil.
Anmelder
- Firma
- Northrop Grumman Systems Corporation
- Land
- 🇺🇸 USA
US-amerikanischer Rüstungs- und Luftfahrtkonzern mit Sitz in Virginia, tätig in den Bereichen Verteidigungselektronik, Flugzeugbau, Raumfahrt und Cybersicherheit.
1.414 Patente in unserer Datenbank