PL423529A1 - Air intake, integral with the fuselage of ultra-light aircraft - Google Patents
Air intake, integral with the fuselage of ultra-light aircraftInfo
- Publication number
- PL423529A1 PL423529A1 PL423529A PL42352917A PL423529A1 PL 423529 A1 PL423529 A1 PL 423529A1 PL 423529 A PL423529 A PL 423529A PL 42352917 A PL42352917 A PL 42352917A PL 423529 A1 PL423529 A1 PL 423529A1
- Authority
- PL
- Poland
- Prior art keywords
- fuselage
- integral
- air
- grip
- ultra
- Prior art date
Links
Landscapes
- Gyroscopes (AREA)
Abstract
Przedmiotem zgłoszenia jest dynamiczny chwyt powietrza (1) integralny z kadłubem (2) ultralekkiego statku powietrznego z rodziny wiropłatów - wiatrakowca. Chwyt powietrza (1) integralny z kadłubem (2) ultralekkiego statku powietrznego mający na przedzie wlot (3) i z tyłu wylot (4), charakteryzuje się tym, że stanowi obłą, aerodynamiczną bryłę mającą w widoku z góry kształt zbliżony do trójkąta o wypukłych bokach, w widoku od przodu kształt zbliżony do połowy wydłużonej elipsy, stanowiący wlot powietrza (3) a w widoku z boku kształt pochylonego tyłem ku dołowi wydłużonego klina, przy czym dolna powierzchnia chwytu powietrza (1) odwzorowuje kształt górnej części kadłuba (2), na którym osadzony jest chwyt powietrza (1) i sięga poza kadłub (2) a w części chwytu (1) poza kadłubem (2) znajduje się wylot powietrza (4).The subject of the notification is a dynamic air grip (1) integral with the fuselage (2) of an ultralight aircraft from the rotorcraft family - gyroplane. The air grip (1) integral with the fuselage (2) of the ultra-light aircraft having an inlet (3) in the front and an outlet (4) at the back, is characterized by being an oval, aerodynamic solid having a top view similar to a triangle with convex sides , in a front view, the shape close to half of the elongated ellipse, constituting the air inlet (3) and in a side view, the shape of the elongated wedge leaning backwards downwards, whereby the lower air grip surface (1) reproduces the shape of the upper fuselage (2), on which the air grip (1) is located and extends beyond the fuselage (2) and in the grip portion (1) outside the fuselage (2) there is an air outlet (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL423529A PL423529A1 (en) | 2017-11-21 | 2017-11-21 | Air intake, integral with the fuselage of ultra-light aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL423529A PL423529A1 (en) | 2017-11-21 | 2017-11-21 | Air intake, integral with the fuselage of ultra-light aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| PL423529A1 true PL423529A1 (en) | 2019-06-03 |
Family
ID=66649224
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL423529A PL423529A1 (en) | 2017-11-21 | 2017-11-21 | Air intake, integral with the fuselage of ultra-light aircraft |
Country Status (1)
| Country | Link |
|---|---|
| PL (1) | PL423529A1 (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0052360A1 (en) * | 1980-11-15 | 1982-05-26 | Fuji Jukogyo Kabushiki Kaisha | Air aspiration device of aircraft-mounted gas-turbine engine |
| DE102010018928A1 (en) * | 2010-04-30 | 2011-11-03 | Gerhard Bihler | Passenger aircraft i.e. airplane, has intense internal thruster arranged at rear of fuselage, and intake ports integrated into sides of body, where air intake ports are arranged to obtain favorable aerodynamic form |
-
2017
- 2017-11-21 PL PL423529A patent/PL423529A1/en unknown
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0052360A1 (en) * | 1980-11-15 | 1982-05-26 | Fuji Jukogyo Kabushiki Kaisha | Air aspiration device of aircraft-mounted gas-turbine engine |
| DE102010018928A1 (en) * | 2010-04-30 | 2011-11-03 | Gerhard Bihler | Passenger aircraft i.e. airplane, has intense internal thruster arranged at rear of fuselage, and intake ports integrated into sides of body, where air intake ports are arranged to obtain favorable aerodynamic form |
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