CN102343982A - Semi-open interlayer booster takeoff runway of aircraft carrier - Google Patents
Semi-open interlayer booster takeoff runway of aircraft carrier Download PDFInfo
- Publication number
- CN102343982A CN102343982A CN2011102048406A CN201110204840A CN102343982A CN 102343982 A CN102343982 A CN 102343982A CN 2011102048406 A CN2011102048406 A CN 2011102048406A CN 201110204840 A CN201110204840 A CN 201110204840A CN 102343982 A CN102343982 A CN 102343982A
- Authority
- CN
- China
- Prior art keywords
- runway
- takeoff
- booster
- form interlayer
- aircraft carrier
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Landscapes
- Road Paving Structures (AREA)
- Traffic Control Systems (AREA)
Abstract
The invention discloses a semi-open interlayer booster takeoff runway of an aircraft carrier. A takeoff runway is arranged below an upper-layer deck of the aircraft carrier; one side of the takeoff runway is open; an open booster engine passage which is parallel to the takeoff runway is arranged below the takeoff runway; and a booster engine runs on a track of the open booster engine passage and is coupled with a front wheel of a takeoff airplane above the booster engine in a takeoff process. Therefore, the boosting force is given to the takeoff airplane. Due to semi-open and open booster engine passage of the semi-open interlayer booster takeoff runway, the ejected high-temperature tail gas can be quickly dispersed outside a shipboard and is easily cooled. According to the scheme, the aircraft carrier can own two to three ejection takeoff runways, and in an emergency, lots of airplanes can take off within a short time. The scheme also can be used for a booster takeoff runway on an upper deck, namely, the booster takeoff runway is arranged on the edge of the upper deck, so that the booster engine passage below the booster takeoff runway can be open.
Description
Technical field
The present invention relates to a kind of catapult-assisted take-off runway of aircraft carrier.
Background technology
The catapult-assisted take-off runway of aircraft carrier all is arranged on the unlimited promenade deck at present, but the promenade deck area is limited, is difficult to hold an above catapult-assisted take-off runway.Launch power then or for steam or for electromagnetism.
Summary of the invention
For this reason, the present invention provides a kind of half open form interlayer accelerated take-off runway below the promenade deck.
Technical scheme of the present invention is: below the aircraft carrier promenade deck, establish the takeoff runway that a side opens wide (below title half open form interlayer takeoff runway).And below this half open form interlayer takeoff runway, establish a booster engine passage (following title open type booster engine passage) that open wide, parallel with half open form interlayer takeoff runway.Booster engine moves on the track of open type booster engine passage, and the coupling of the front-wheel of the aircraft that takes off when taking off and on half open form interlayer takeoff runway, thereby gives the boosting power of aircraft when taking off of taking off.
Half open form interlayer takeoff runway is located on the hull limit.Because the span beyond the undercarriage, double open form interlayer takeoff runway do not form load, outside the span beyond the undercarriage that takes off can be exposed on the quarter.When the catapult-assisted take-off runway on the promenade deck be used to the take off span and highly big aircrafts such as early warning plane, half open form interlayer takeoff runway were used to take off the span and highly little fighter plane, then the height of half open form interlayer takeoff runway and width can be less.
In the end section of half open form interlayer takeoff runway, because the existing lift of aircraft, load is little.The end section is departed from outside the ship side.
For the staff can work around aircraft, can open wide a side at half open form interlayer takeoff runway and establish outwardly directed work top.This work top also can be collapsible, when half open form interlayer takeoff runway does not use, and can work top is folding up or down.
Not busy when the task of taking off, when the catapult-assisted take-off runway of promenade deck was enough, the hardstand (hangar) that half open form interlayer takeoff runway can be used as in the interlayer was used.
Booster engine in the open type booster engine passage can be aero-engine or rocket engine.Booster engine moves on the track of open type booster engine passage, or hangs on track and move.
Because partly opening wide of half open form interlayer takeoff runway and opening wide of open type booster engine passage make the high-temperature tail gas that ejects, rapidly outside the dissipation on the quarter.And cooling easily.
This scheme also can be used for the accelerated take-off runway of upper deck, promptly the accelerated take-off runway is located on the upper deck limit, and the booster engine passage below it can be opened wide.
The invention has the beneficial effects as follows: half open form interlayer accelerated take-off runway can make aircraft carrier have two to three catapult-assisted take-off runways, in case of emergency, and a large amount of aircrafts but the short time takes off.Owing to use the booster engine accelerated take-off, save the steam or the electromagnetic launch device of complex and expensive.
Description of drawings
Fig. 1 half open form interlayer accelerated take-off runway schematic cross-section
Among the figure: 1 half open form interlayer takeoff runways, 2 aircraft carrier promenade decks, 3 aircrafts, 4 work tops, 5 open type booster engine passages, 6 booster engines.
Claims (4)
1. aircraft carrier half open form interlayer accelerated take-off runway; It is characterized in that: below the aircraft carrier promenade deck, establish the half open form interlayer takeoff runway that a side is opened wide; And below this half open form interlayer takeoff runway; If that open wide, parallel open type booster engine passage with half open form interlayer takeoff runway; Booster engine moves on the track of open type booster engine passage, and the coupling of the front-wheel of the aircraft that takes off when taking off and on half open form interlayer takeoff runway.
2. according to the half open form interlayer accelerated take-off runway of the aircraft carrier in the claim 1; It is characterized in that: the side in that aircraft carrier half open form interlayer takeoff runway opens wide is established fixing work top; Perhaps establish the work top that can upwards fold, perhaps establish the work top that can fold downwards.
3. according to the half open form interlayer accelerated take-off runway of the aircraft carrier in the claim 1, it is characterized in that: when half open form interlayer catapult-assisted take-off runway did not use, the hangar that can be used as in the interlayer was used.
4. according to the half open form interlayer accelerated take-off runway of the aircraft carrier in the claim 1, it is characterized in that: booster engine is aero-engine or rocket engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102048406A CN102343982A (en) | 2011-07-21 | 2011-07-21 | Semi-open interlayer booster takeoff runway of aircraft carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011102048406A CN102343982A (en) | 2011-07-21 | 2011-07-21 | Semi-open interlayer booster takeoff runway of aircraft carrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102343982A true CN102343982A (en) | 2012-02-08 |
Family
ID=45543126
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011102048406A Pending CN102343982A (en) | 2011-07-21 | 2011-07-21 | Semi-open interlayer booster takeoff runway of aircraft carrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102343982A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103359296A (en) * | 2012-03-29 | 2013-10-23 | 梁文华 | Counterweight type aircraft carrier catapult |
| CN103359297A (en) * | 2012-03-30 | 2013-10-23 | 卢振江 | Combined catapult for aircraft carriers |
| CN103723283A (en) * | 2012-10-16 | 2014-04-16 | 邓磊光 | Aircraft carrier |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2176968C1 (en) * | 2000-09-05 | 2001-12-20 | Местон Вячеслав Александрович | Spacecraft carrier-trimaran |
| CN201437404U (en) * | 2009-04-08 | 2010-04-14 | 王石诚 | Aircraft carrier with dual-layer flight deck concept |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
| CN101934862A (en) * | 2009-06-29 | 2011-01-05 | 高颖悟 | High-fulcrum launch/ski-jump system for aircraft carrier |
-
2011
- 2011-07-21 CN CN2011102048406A patent/CN102343982A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2176968C1 (en) * | 2000-09-05 | 2001-12-20 | Местон Вячеслав Александрович | Spacecraft carrier-trimaran |
| RU2390462C1 (en) * | 2009-03-13 | 2010-05-27 | Эдуард Дмитриевич Житников | Small two-deck aircraft carrier |
| CN201437404U (en) * | 2009-04-08 | 2010-04-14 | 王石诚 | Aircraft carrier with dual-layer flight deck concept |
| CN101934862A (en) * | 2009-06-29 | 2011-01-05 | 高颖悟 | High-fulcrum launch/ski-jump system for aircraft carrier |
Non-Patent Citations (2)
| Title |
|---|
| 不详: "舰载机喷气助推起飞设想", 《兵工科技》 * |
| 马世强: "舰载机喷气助推器", 《航空知识》 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103359296A (en) * | 2012-03-29 | 2013-10-23 | 梁文华 | Counterweight type aircraft carrier catapult |
| CN103359297A (en) * | 2012-03-30 | 2013-10-23 | 卢振江 | Combined catapult for aircraft carriers |
| CN103723283A (en) * | 2012-10-16 | 2014-04-16 | 邓磊光 | Aircraft carrier |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Gohardani | A synergistic glance at the prospects of distributed propulsion technology and the electric aircraft concept for future unmanned air vehicles and commercial/military aviation | |
| US8453963B2 (en) | Amphibious large aircraft without airstairs | |
| US20200017228A1 (en) | Parallel Hybrid Aircraft | |
| NZ592991A (en) | Aircraft system that enables ground traveling | |
| CN102897319A (en) | Fuselage variant type vertical take off and landing aircraft | |
| US20200331591A1 (en) | Drag recovery scheme for nacelles | |
| CN102343982A (en) | Semi-open interlayer booster takeoff runway of aircraft carrier | |
| CN109573025A (en) | It is a kind of quickly to support the land-effect plane ensured for marine | |
| CN206243476U (en) | VTOL fixed-wing unmanned plane | |
| RU2558527C1 (en) | Light boatplane (amphibious aircraft) | |
| EP2799335B1 (en) | A modular aircraft | |
| CN107434036A (en) | Ferried in the air without combustion powered arrow ship and float airport air transport system | |
| CN102152842A (en) | Design scheme of connecting and assembling dual-use ultra large ships in series into marine maneuvering airport | |
| CN107738748A (en) | A kind of multipurpose Dual module combined type hybrid power unmanned plane | |
| CN105083578A (en) | Flight airdrome | |
| CN207257983U (en) | A kind of multipurpose Dual module combined type hybrid power unmanned plane device | |
| Marques | Emerging technologies in UAV aerodynamics | |
| CN203160192U (en) | Airport fog dispersal vehicle | |
| CN207191430U (en) | A kind of unmanned composite aircraft of naval searching | |
| RU2613629C2 (en) | Drone aircraft (versions) | |
| CN103770937A (en) | Airplane capable of vertically taking off and landing with short distance | |
| CN209617447U (en) | A kind of twin vertical fin medium transport aircraft | |
| CN107776348A (en) | Land, water and air three are dwelt automobile | |
| CN108791938B (en) | Shipborne launching method of fixed-wing unmanned aircraft | |
| CN105882957A (en) | Carrier-borne vertical takeoff and landing unmanned attacker |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20120208 |