FIELD: transport.
SUBSTANCE: nacelle comprises air intake 2 to guide air to turbojet blower and central compartment surrounding said blower and whereto air intake is jointed. Air intake comprises inner panel 21 attached to central compartment structure by fastening flanges to nacelle fixed structure therewith and outer panel 20 split-jointed to said fixed structure by circular web 5 arranged at said flanges and including air intake lip 2a. Air intake edges are equipped with loc means each including lock 10 fitted at inner panel or air intake lip to interact with mating lock means 11 arranged at air intake lip or inner panel, respectively.
EFFECT: reliable joint between air intake and inner panel.
17 cl, 14 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DETACHABLE AIR INTAKE FOR TURBOJET NACELLE | 2007 |
|
RU2451804C2 |
| LOCK COMPRISING TELESCOPIC CONNECTION ROD EQUIPPED WITH RETURN FACILITY | 2008 |
|
RU2480567C2 |
| TURBOJET NACELLE | 2010 |
|
RU2524321C2 |
| TURBOJET ENGINE NACELLE WITH LATERAL OPENING OF FLAPS | 2007 |
|
RU2436712C2 |
| LATCH | 2008 |
|
RU2456214C2 |
| TURBOJET NACELLE WITH SLIDING FRONT COWL | 2009 |
|
RU2505458C2 |
| NACELLE AIR INTAKE AND NACELLE CONTAINING SUCH AIR INTAKE | 2020 |
|
RU2801764C2 |
| TURBOJET THRUST REVERSER WITH CONTROLLED-CROSS-SECTION ADJUSTABLE NOZZLE SECTION AND TURBOJET NACELLE | 2011 |
|
RU2568362C2 |
| SYSTEM OF CONNECTION BETWEEN INNER AND OUTER STRUCTURES OF TURBOJET ENGINE POD | 2008 |
|
RU2483984C2 |
| NACELLE AIR INTAKE AND NACELLE CONTAINING SUCH AIR INTAKE | 2020 |
|
RU2804492C2 |
