FIELD: aviation. SUBSTANCE: proposed aircraft has fuselage with replaceable nose compartments provided with frames taking up load from respective equipment. Replaceable nose compartments are bounded by third frame. Nose fuselage is engageable with frame of replaceable compartment by its own frame. Pilot s cabin is located in nose fuselage. Replaceable nose compartments may take up entire load from equipment located in them. EFFECT: extended functional capabilities of aircraft. 4 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
LIGHT MULTI-PURPOSE AIRCRAFT | 2002 |
|
RU2210522C1 |
AIRCRAFT | 2002 |
|
RU2220075C1 |
INTEGRATED ON-BOARD EQUIPMENT COMPLEX FOR LIGHT COMBAT TRAINER | 2002 |
|
RU2203200C1 |
AIRCRAFT ENGINE AIR INTAKE | 2002 |
|
RU2209154C1 |
LIGHT SUPERSONIC MULTI-PURPOSE AIRCRAFT | 2004 |
|
RU2271305C1 |
MULTI-PURPOSE DEVICE FOR SECURING EXTERNAL STORES ON FLYING VEHICLE | 2003 |
|
RU2232107C1 |
SUPERSONIC MULTI-PURPOSE AIRCRAFT | 2004 |
|
RU2268846C1 |
COMPLEX OF ON-BOARD ELECTRONIC EQUIPMENT FOR LIGHT MULTI-PURPOSE AIRCRAFT | 2002 |
|
RU2215668C1 |
SHORT-, MID-RANGE MAIN LINE AIRCRAFT | 2009 |
|
RU2384463C1 |
AIRLINER WITH AIRCRAFT GENERAL HARDWARE CONTROL SYSTEM AND AIRCRAFT SYSTEMS | 2013 |
|
RU2529248C1 |
Authors
Dates
2003-08-20—Published
2002-10-02—Filed