FIELD: machine building.
SUBSTANCE: device of backward protection of airship body of rigid type during parking is characterized by that air ducts of warm air supply are installed between gas bags and outer skin of airship. Radial air ducts are made with possibility of connection in lower part of housing by means of connecting elbows to detachable heat installation, and in housing upper part are connected by means of connecting elbows to longitudinal air ducts located along airship housing and having hot air outlets distributed along their length.
EFFECT: disclosed is a device for back-to-back protection of a rigid-type airship body during parking.
1 cl, 7 dwg, 2 tbl
Title | Year | Author | Number |
---|---|---|---|
ANTI-ICING SYSTEM | 2014 |
|
RU2583111C1 |
AIRCRAFT DE-ICING SYSTEM AND AIRCRAFT WITH SUCH SYSTEM | 2011 |
|
RU2529927C1 |
ANTI-ICE SYSTEM FOR AIRCRAFT WING SLATS | 2019 |
|
RU2742203C1 |
AEROWINDENERGY BALLOON DE-ICING | 2018 |
|
RU2679060C1 |
METHOD OF ANTI-ICING PROTECTION OF STRUCTURAL MEMBERS OF FLYING VEHICLES | 2002 |
|
RU2233232C2 |
FLYING VEHICLE WITH PASSENGER EMERGENCY AND RESCUE MODULES | 2000 |
|
RU2172277C1 |
SYSTEM FOR DISTRIBUTION AND DISCHARGE OF ANTI-ICING FLUID IN AIRCRAFT SKIN | 2023 |
|
RU2824828C1 |
ECOLOGICAL HYBRID VERTICAL TAKEOFF AND LANDING FLYING VEHICLE WITH STORAGE FOR HELIUM USED IN IT | 1993 |
|
RU2097272C1 |
METHOD FOR INCREASING STRENGTH OF MEMBRANE BASED ON POLYTETRAFLUOROETHYLENE (PTFE) BY HIGH-TEMPERATURE MICROEUTECTICS UNDER HIGH LINE PRESSURE | 2020 |
|
RU2786882C1 |
METHOD FOR PREVENTING ACING OF AIRCRAFT WINGS WITH THE USE OF LASER ANTI-ICING SYSTEM | 2017 |
|
RU2671069C1 |
Authors
Dates
2020-07-07—Published
2015-09-29—Filed