FIELD: construction of aircraft aerodynamic surfaces. SUBSTANCE: load-bearing structure consists of at least two spars, several ribs and skins. Skins and ribs are divided into several parts in way of chord of profile. Load-bearing structure is formed from several box-shaped structural members each of which consists of spar, two members of skin and several members of ribs. During assembly, each subsequent structural member enters previous one between projecting edges of members of skins. Length and number of parts of ribs of structural member are independent on length and number of parts of ribs of previous structural member. EFFECT: ease of mounting aerodynamic surface having insignificant thickness and rather large chord of profile. 2 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
SEALANT FEEDING UNIT | 1993 |
|
RU2106927C1 |
CABLE DUCT FOR ROUTING INSULATED POWER LINES | 1993 |
|
RU2134008C1 |
AUTOMATIC RIVETING MACHINE | 1993 |
|
RU2106926C1 |
DRILL PRESS | 1993 |
|
RU2120833C1 |
LARGE-CAPACITY AIRCRAFT | 1994 |
|
RU2131826C1 |
ULTRA LOW MASS AIRPLANE | 2005 |
|
RU2336200C2 |
AIRCRAFT FOOD-STUFF AND DRINKS HANDLING SYSTEM | 1994 |
|
RU2133695C1 |
LARGE-SIZED AERODYNAMIC MODEL | 2015 |
|
RU2607675C1 |
CABIN VENTILATION SYSTEM FOR AIR-CONDITIONING OF PASSENGER AIRCRAFT FUSELAGE COMPARTMENTS | 1994 |
|
RU2089791C1 |
METHOD FOR MANUFACTURING AN ADAPTIVE WING WITH FLEXIBLE GAPLESS MECHANIZATION | 2022 |
|
RU2784223C1 |
Authors
Dates
1999-07-27—Published
1994-05-10—Filed