Global Patent Index - EP 4278075 A1

EP 4278075 A1 20231122 - PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A STATOR VANE INTEGRATED INTO AN UPSTREAM PART OF A MOUNTING PYLON OF REDUCED HEIGHT

Title (en)

PROPULSION ASSEMBLY FOR AN AIRCRAFT COMPRISING A STATOR VANE INTEGRATED INTO AN UPSTREAM PART OF A MOUNTING PYLON OF REDUCED HEIGHT

Title (de)

ANTRIEBSANORDNUNG FÜR EIN FLUGZEUG MIT EINER IN EINEM VORGELAGERTEN TEIL EINES MONTAGEPYLONS MIT REDUZIERTER HÖHE INTEGRIERTEN STATORSCHAUFEL

Title (fr)

ENSEMBLE PROPULSIF POUR AERONEF COMPRENANT UNE AUBE DE REDRESSEUR INTÉGRÉE À UNE PARTIE AMONT D'UN MAT D'ACCROCHAGE DE HAUTEUR RÉDUITE

Publication

EP 4278075 A1 20231122 (FR)

Application

EP 22702295 A 20220105

Priority

  • FR 2100258 A 20210112
  • FR 2022050026 W 20220105

Abstract (en)

[origin: WO2022152994A1] The invention relates to a propulsion assembly (200) for an aircraft comprising a double-flow turbomachine (1) equipped with a fan (15), an aerodynamic outer casing (5) forming a nacelle, and a mounting pylon, the propulsion assembly having a secondary duct (18) delimited by an outer radial delimiting surface (23a) formed by the casing (5), the turbomachine comprising stator vanes (30), and the mounting pylon (7) comprising a part housed in the secondary duct, termed upstream part (7b). According to the invention, the upstream part (7b) of the pylon extends radially from the inner radial delimiting surface (40a) over a radial pylon height (Hm) strictly less than a total radial height (Ht) of the secondary duct (18), and the upstream part (7b) of the pylon extends in the downstream direction from a root part (62a) of one of the stator vanes (30).

IPC 8 full level

F02C 7/20 (2006.01); B64D 27/40 (2024.01); F01D 5/14 (2006.01); F02K 1/66 (2006.01); F02K 3/068 (2006.01)

CPC (source: EP US)

B64C 7/02 (2013.01 - US); B64D 27/10 (2013.01 - EP); B64D 27/40 (2024.01 - US); B64D 27/402 (2024.01 - US); B64D 27/404 (2024.01 - US); B64D 27/406 (2024.01 - US); F01D 5/143 (2013.01 - EP); F02C 7/20 (2013.01 - EP US); F02K 1/66 (2013.01 - EP US); F02K 3/068 (2013.01 - EP US); B64D 27/12 (2013.01 - US); F02K 1/64 (2013.01 - US); F05D 2240/122 (2013.01 - EP); F05D 2260/40311 (2013.01 - EP); F05D 2260/74 (2013.01 - EP); Y02T 50/60 (2013.01 - EP)

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

Designated extension state (EPC)

BA ME

Designated validation state (EPC)

KH MA MD TN

DOCDB simple family (publication)

FR 3118787 A1 20220715; FR 3118787 B1 20230609; CN 116917610 A 20231020; EP 4278075 A1 20231122; US 2024116644 A1 20240411; WO 2022152994 A1 20220721

DOCDB simple family (application)

FR 2100258 A 20210112; CN 202280018205 A 20220105; EP 22702295 A 20220105; FR 2022050026 W 20220105; US 202218261124 A 20220105