PL415538A1 - Parachute rescue system - Google Patents
Parachute rescue systemInfo
- Publication number
- PL415538A1 PL415538A1 PL415538A PL41553815A PL415538A1 PL 415538 A1 PL415538 A1 PL 415538A1 PL 415538 A PL415538 A PL 415538A PL 41553815 A PL41553815 A PL 41553815A PL 415538 A1 PL415538 A1 PL 415538A1
- Authority
- PL
- Poland
- Prior art keywords
- parachute
- aircraft
- fuselage
- cover
- rescue system
- Prior art date
Links
Landscapes
- Emergency Lowering Means (AREA)
- Toys (AREA)
Abstract
Zgłoszenie dotyczy spadochronowy system ratunkowy lekkiego samolotu z silnikiem odrzutowym zamontowanym na kadłubie. Spadochronowy system ratunkowy lekkiego samolotu z silnikiem odrzutowym (8), zamontowanym na kadłubie, zawierający spadochron w kadłubie samolotu (1), umieszczony w zasobniku (2) z pokrywą (9) oraz rakietę wyciągową (4) spadochronu, połączoną ze spadochronem, której zapalnik uruchamiany jest poprzez cięgno rakiety (5), połączone z uchwytem (6), zamocowanym w oprawie (7) wewnątrz samolotu charakteryzuje się tym, że zasobnik (2) ze spadochronem jest umieszczony w kadłubie samolotu (1) przed wlotem powietrza do silnika odrzutowego (8) i wyposażony jest od góry w otwieraną pokrywę (9), stanowiącą część poszycia kadłuba samolotu (1), osadzoną obrotowo na jej tylnej krawędzi (10) i mechanizm otwierania pokrywy (9), uruchamiany z wnętrza samolotu, przy czym na pokrywie (9) od wewnętrznej strony przymocowana jest rakieta wyciągowa (4) spadochronu.The application concerns a parachute rescue system of a light aircraft with a jet engine mounted on the fuselage. Parachute rescue system of a light aircraft with a jet engine (8), mounted on the fuselage, containing a parachute in the aircraft fuselage (1), placed in the container (2) with a cover (9) and an exhaust rocket (4) of the parachute, combined with a parachute it is activated by a rocket cable (5), connected to the handle (6), mounted in the housing (7) inside the aircraft, characterized by the fact that the container (2) with the parachute is placed in the fuselage (1) in front of the air inlet to the jet engine ( 8) and is equipped from the top with an opening cover (9), which is part of the aircraft fuselage (1), rotatably mounted on its rear edge (10) and a cover opening mechanism (9), activated from the inside of the aircraft, with the cover ( 9) from the inside a parachute hoist (4) is attached.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL415538A PL229993B1 (en) | 2015-12-23 | 2015-12-23 | Parachute rescue system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL415538A PL229993B1 (en) | 2015-12-23 | 2015-12-23 | Parachute rescue system |
Publications (2)
Publication Number | Publication Date |
---|---|
PL415538A1 true PL415538A1 (en) | 2017-07-03 |
PL229993B1 PL229993B1 (en) | 2018-09-28 |
Family
ID=59201326
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL415538A PL229993B1 (en) | 2015-12-23 | 2015-12-23 | Parachute rescue system |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL229993B1 (en) |
-
2015
- 2015-12-23 PL PL415538A patent/PL229993B1/en unknown
Also Published As
Publication number | Publication date |
---|---|
PL229993B1 (en) | 2018-09-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP2019179249A5 (en) | ||
MY177932A (en) | Self-propelled craft | |
EP3680403A3 (en) | Cartridge and dispenser device of a jet of water incorporating such cartridge | |
GB2548480B (en) | Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box | |
BR112015025209A2 (en) | kinetic and potential energy-to-energy recovery and conversion system for aircraft | |
MX2007015026A (en) | Toy aircraft. | |
BR112015032753A2 (en) | COOKING DEVICE AND COOKING METHOD OF A FOOD PRODUCT | |
FR3041933B1 (en) | AIRCRAFT WITH A PROPULSIVE ASSEMBLY COMPRISING A PROPELLER DOUBLET ON THE REAR OF THE FUSELAGE | |
FR3011744B1 (en) | CONTAINER WITH COVER | |
BR102014022781A8 (en) | propeller blade set | |
GB2559018B (en) | Assembly for an aircraft comprising an engine of the "open rotor puller" type and means for attaching the latter to the rigid structure of an attachment pylon | |
FR3039134B1 (en) | AIRCRAFT WITH A PROPULSIVE ASSEMBLY COMPRISING A BLOWER AT THE REAR OF THE FUSELAGE | |
EP2626294A3 (en) | Low profile jettisonable door system | |
WO2011023396A3 (en) | Aircraft having at least two electrical propulsion groups mounted at a rear portion thereof | |
EP2719621A3 (en) | Aft exhaust system for rotary wing aircraft | |
EP2610179A3 (en) | Aircraft air inlet diverter assemblies with improved aerodynamic characteristics | |
ES2585283R1 (en) | Aircraft nose provided with a connection frame between the landing gear housing and the outer lining of the fuselage | |
BR112017026527A2 (en) | "system, and apparatus". | |
PL415538A1 (en) | Parachute rescue system | |
RU2015124779A (en) | CARGO COMPARTMENT OF THE AIRCRAFT | |
WO2013039981A3 (en) | Aircraft galley stowage compartment extractor | |
FR3056556B1 (en) | AIRCRAFT WITH A TURBOMACHINE INTEGRATED WITH REAR FUSELAGE COMPRISING A PROPELLER SURROUNDING AN EXHAUST CASING | |
UA110711C2 (en) | Equipment for the reduction of the radar marking of an aircraft | |
RU2011127920A (en) | HUMAN parachute system for landing with a parachutist of heavy oversized cargo | |
GB201203892D0 (en) | A fan assembly |