FIELD: transportation.
SUBSTANCE: group of inventions relates to a front edge unit (1), a water intake and an aircraft nacelle. The front edge unit (1) for an air intake of aircraft nacelle includes a front edge (2) and an inner edge (3), which limits inside the specified front edge (2) a longitudinal compartment (5). The front edge (2) and the inner edge (3) are made from multi-axial composite materials. The air intake comprises a front edge unit (1). The aircraft engine nacelle comprises an air intake.
EFFECT: group of inventions is aimed at weight reduction.
11 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LEADING EDGE STRUCTURE, PARTICULARLY, TO AIRCRAFT ENGINE NACELLE | 2011 |
|
RU2577975C2 |
| AIRCRAFT STRUCTURE ELEMENT | 2007 |
|
RU2438923C2 |
| ASSEMBLY OF ELEMENTS CONNECTED BY DEVICE PROTECTING SURFACE OF ONE OF SAID ELEMENTS | 2009 |
|
RU2521824C2 |
| CONFORMAL COMPOSITE ANTENNA ASSEMBLY | 2016 |
|
RU2714862C2 |
| AIR INTAKE FOR TURBOJET ENGINE NACELLE | 2020 |
|
RU2806229C2 |
| FRONT FRAME FOR THRUST REVERSER WITH DEFLECTING CASCADES | 2010 |
|
RU2542165C2 |
| METHOD OF MAKING ACOUSTIC PANEL FOR NACELLE AIR INTAKE | 2009 |
|
RU2500580C2 |
| AIRCRAFT NACELLE AIR INTAKE ASSEMBLY | 2009 |
|
RU2496687C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2011 |
|
RU2570181C2 |
| NACELLE AIR INTAKE WITH ACOUSTIC PANEL | 2020 |
|
RU2803661C2 |
