WO2025214551 - FLUGZEUGANTRIEB
National phase entry is expected:
Publication Number
WO/2025/214551
Publication Date
16.10.2025
International Application No.
PCT/DE2025/100342
International Filing Date
04.04.2025
Title **
[German]
FLUGZEUGANTRIEB
[English]
AIRCRAFT PROPULSION SYSTEM
[French]
SYSTÈME DE PROPULSION D'AÉRONEF
Applicants **
MTU AERO ENGINES AG
Inventors
BOLGAR, Istvan
SCHULDT, Simon
Priority Data
102024109986.0
10.04.2024
DE
Application details
| Total Number of Claims/PCT | * |
| Number of Independent Claims | * |
| Number of Priorities | * |
| Number of Multi-Dependent Claims | * |
| Number of Drawings | * |
| Pages for Publication | * |
| Number of Pages with Drawings | * |
| Pages of Specification | * |
| * | |
| Number of Office Actions | * |
| * | |
International Searching Authority |
EPO
* |
| Recordal of a Change of the Applicant's Name/Address |
Change of Applicant's Name and Address
* |
| Type of Assignment |
The Standard Agent's Assignment
* |
| Applicant's Legal Status |
Legal Entity
* |
| * | |
| * | |
| * | |
| * | |
| * | |
| Entry into National Phase under |
Chapter I
* |
| Patent Delivery |
Send the Letters Patent by Courier
* |
| Translation |
|
* The data is based on automatic recognition. Please verify and amend if necessary.
** IP-Coster compiles data from publicly available sources. If this data includes your personal information, you can contact us to request its removal.
Quotation for National Phase entry
| Country | Stages | Total | |
|---|---|---|---|
| China | Filing, Examination, Granting | 1965 | |
| EPO | Filing, Examination, Granting | 8159 | |
| Japan | Filing, Examination, Granting | 2108 | |
| South Korea | Filing, Examination, Granting | 1927 | |
| USA | Filing, Examination, Granting | 4740 |
Total:
18,899
Contact Us
Abstract[German]
Die Erfindung betrifft einen Flugzeugantrieb (10), aufweisend eine mit einer Gasströmung (G) durchströmbare Strömungsmaschine (20) und eine Aufhängungseinrichtung (30), wobei die Strömungsmaschine (20) mittels der Aufhängungseinrichtung (30) mit einem Flugzeug verbindbar ist.[English]
The invention relates to an aircraft propulsion system (10), comprising a turbomachine (20), through which a gas flow (G) can flow, and a suspension device (30), the turbomachine (20) being connectible to an aircraft by means of the suspension device (30).[French]
L'invention concerne un système de propulsion (10) d'aéronef, comprenant une turbomachine (20) pouvant être traversée par un flux gazeux (G), et un dispositif de suspension (30), la turbomachine (20) pouvant être connectée à un aéronef par l'intermédiaire du dispositif de suspension (30).