WO2008147339A4 - Aircraft systems for rescuing life - Google Patents
Aircraft systems for rescuing life Download PDFInfo
- Publication number
- WO2008147339A4 WO2008147339A4 PCT/TR2008/000017 TR2008000017W WO2008147339A4 WO 2008147339 A4 WO2008147339 A4 WO 2008147339A4 TR 2008000017 W TR2008000017 W TR 2008000017W WO 2008147339 A4 WO2008147339 A4 WO 2008147339A4
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- freight
- lights
- air
- glider
- aircraft
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/12—Ejectable capsules
Landscapes
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
This invention is related to a mechanical, electronic and pneumatic system, which will be activated in emergency situations of possible falling down of the aircraft. At this system pilot and passenger cabins (1) will be separated from the aircraft by means of air-pressure, spring power and dividing clips (27), at the height of opening parachutes (24) a glider will run up and the passengers will land in a safe way. Further on, this system includes another independent system, which rescues freight. This system provides a rescue of freight by a glider and inflatable boot on the freight (25), which are discharged through a gate on the. bottom. By force of these systems, important steps will be taken to rescue life and freight.
Claims
1. The lights in the indicator (9), representing the air pressure stations (6), should be turned from green to red; the lights (28), representing the springs should be yellow coloured and all lights should be turned out in cancelling-position. All these representation lights and switches should be manufactured in desired main colours. All switches, used on the panel should have single-level and only for one operation. The crank, used on the panel should have two levels. With the level forward, the light on it, should turn on and the emergency landing valves (16) on the glider's wings should be opened, the closing of these valves (16) should be operated with moving the crank downwards.
2. Compressing of air should be done by hydraulics.
3. The foldable air routes (29), which are opening the glider's wings (14), should be installed on the top of cabin, on right and left side, on each side 4 pieces with suitable spaces.
4. According to claim 3, on this foldable air routes (29) should be an air and rail moving system, which is going to each wing.
5. According to claim 3 and 4, this system should move to right, left, upwards and downwards.
6. According to claim 5, this moving system should be turned back at its first modus.
7. On the freight (22), it must have a barcode, and in emergency cases the data of the freight should be seen on this barcode.
8. There must be an emergency-freight-gate (23) in two pieces on the bottom of the aircraft.
9. According to claim 8, there must be 10 clips (32), which are installed in suitable spaces and which enables the automatic opening of this gate and can be operated altogether at the same time.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2007/03725A TR200703725A2 (en) | 2007-05-31 | 2007-05-31 | Life saving aircraft systems. |
| TR2007/03725 | 2007-05-31 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| WO2008147339A1 WO2008147339A1 (en) | 2008-12-04 |
| WO2008147339A4 true WO2008147339A4 (en) | 2009-01-29 |
Family
ID=39657780
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/TR2008/000017 WO2008147339A1 (en) | 2007-05-31 | 2008-02-25 | Aircraft systems for rescuing life |
Country Status (2)
| Country | Link |
|---|---|
| TR (1) | TR200703725A2 (en) |
| WO (1) | WO2008147339A1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1396034B1 (en) * | 2009-10-15 | 2012-11-09 | Rolla | AIRCRAFT WITH QUICK RELEASE DEVICE FOR THE FUSER AND CONTROL IN THE LAND OF THE SAME. |
| CN104554730A (en) * | 2013-10-11 | 2015-04-29 | 天津得瑞丰凯新材料科技有限公司 | Passenger plane parachute bay collective escape device |
| CN110606185A (en) * | 2019-10-11 | 2019-12-24 | 王彪 | Safety airplane with combined structure |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH403502A (en) * | 1963-07-12 | 1965-11-30 | P Von Arx Ag | Passenger airplane |
| CH497315A (en) * | 1967-08-08 | 1970-10-15 | Physik Chem Forschungs Inst Pr | Device for rescuing the occupants of an aircraft that is making an emergency landing, landing in an emergency, or is falling or is in danger of falling |
| US6042051A (en) * | 1996-11-25 | 2000-03-28 | Jon C. Hagerty | Emergency self inflating aircraft landing assist system |
| DE19908861A1 (en) * | 1999-03-01 | 2000-09-07 | Dietmar Wolter | Aircraft for transporting useful load, with separate transport units for freight which can be released |
| GR1003755B (en) * | 2000-03-31 | 2002-01-15 | Aircraft with detachable cabin equipped with shock-absorbing parachutes-airbags-seats and conventional aircraft equipped with said safety systems | |
| DE10206306A1 (en) * | 2002-02-12 | 2003-08-21 | Dieter Lampart | Rescue cabin for aircraft accident, separates from remaining body of aircraft and carries passengers safely to ground using parachutes |
| US6655636B1 (en) * | 2002-04-29 | 2003-12-02 | The United States Of America As Represented By The Secretary Of The Navy | Product wrapping incorporating air drag device |
| JP2009505875A (en) * | 2005-08-26 | 2009-02-12 | ロレンツォ ベルターニ，ロモロ | Aircraft safety system |
-
2007
- 2007-05-31 TR TR2007/03725A patent/TR200703725A2/en unknown
-
2008
- 2008-02-25 WO PCT/TR2008/000017 patent/WO2008147339A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO2008147339A1 (en) | 2008-12-04 |
| TR200703725A2 (en) | 2007-12-24 |
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