CN101992842A - Water auxiliary take-off/landing system for airplane - Google Patents
Water auxiliary take-off/landing system for airplane Download PDFInfo
- Publication number
- CN101992842A CN101992842A CN2010105170886A CN201010517088A CN101992842A CN 101992842 A CN101992842 A CN 101992842A CN 2010105170886 A CN2010105170886 A CN 2010105170886A CN 201010517088 A CN201010517088 A CN 201010517088A CN 101992842 A CN101992842 A CN 101992842A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- speedboat
- speed
- assistance
- manipulator
- 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
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a water auxiliary take-off/landing system for an airplane, which relates to the field of speed boats and the field of runways. The water auxiliary take-off/landing system is characterized in that a speed boat is used as a carrier and provided with a manipulator; when the airplane takes off, the manipulator on the speed boat clamps a landing gear, and the airplane and the speed boat are accelerated at the same time; after the take-off speed is achieved, the manipulator releases the airplane and the airplane takes off; and when the airplane lands, the airplane flies above the speed boat and slows down to the landing speed, the speed boat is accelerated to the same speed as the air plane, the manipulator clamps the airplane, the airplane and the speed boat are decelerated to zero speed, and the airplane lands. The invention is applicable to the water take-off/landing of airplanes.
Description
Technical field
The present invention relates to speedboat field and airstrip field, having proposed a kind of is carrier with the speedboat, and second-mission aircraft is the system of lifting on the water.
Background technology
Existing open sea aeroplane lifting has only dual mode, and a kind of is lifting on aircraft carrier; Another kind is device liftings such as hydroairplane utilization floating drum.This dual mode all has its limitation.
Use aircraft carrier to be aircraft lifting and landing, a lot of existing problems are arranged, high as the aircraft carrier cost, hidden degree not excessive risk is bigger, need much escort strength.
Another kind is device liftings such as hydroairplane utilization floating drum.The weak point of active service hydroairplane is that floating drum has certain mass, can produce resistance when flight, and the consequence that causes is that the load-carrying of aircraft reduces, and gas consumption rate increases.The active service hydroairplane can't compare its many aspect with the aircraft of land lifting because jacking system such as floating drum etc. have limited the quality of its many aspect.
Summary of the invention
Purpose of the present invention is exactly to provide a kind of system that makes aircraft lifting waterborne for the defective that overcomes present technology existence.
Purpose of the present invention can be achieved through the following technical solutions: a kind of aircraft assistance for lifting waterborne system, it is characterized in that: this aircraft assistance for lifting waterborne system is a carrier with the speedboat, have on the speedboat identical with the undercarriage number can be in the certain space scope rapid-action manipulator.
Described a kind of aircraft assistance for lifting waterborne system, it is characterized in that: speedboat is provided with induction system, induction system can be sensed taking off of aircraft or landing information, can sense the space relativeness of aircraft and speedboat, can sense the relative velocity and the absolute velocitye of aircraft and speedboat.
Described a kind of aircraft assistance for lifting waterborne system, it is characterized in that: speedboat is provided with command and control system, and command and control system can obtain the information that induction system transmits, and can command the run action of control manipulator, speedboat and aircraft.
Described a kind of aircraft assistance for lifting waterborne system, it is characterized in that: when taking off, manipulator on the speedboat is clamped undercarriage, aircraft and speedboat together quicken, after reaching takeoff speed, when the lift that aircraft self produces was enough to support the gravity of aircraft, command and control system was sent instruction to the speedboat manipulator, the speedboat manipulator is decontroled undercarriage, takes off.
Described a kind of aircraft assistance for lifting waterborne system, it is characterized in that: when aircraft landing, command and control system designs an aircraft landing track and a speedboat travel track in real time according to the space relativeness and the speed of aircraft and speedboat, speedboat and aircraft are advanced and are prepared along track and land, aircraft slows down to sinking speed, speedboat quickens to sinking speed, when aircraft and speedboat reach same speed, and when aircraft is positioned at the top of the manipulator on the speedboat, manipulator on the speedboat is clamped undercarriage, be decelerated to zero velocity, aircraft landing then together.
Described a kind of aircraft assistance for lifting waterborne system is characterized in that: this aircraft assistance for lifting waterborne system can be used for the speed of taking off and takes off less than the fixed wing aircraft of the maximum gait of march of speedboat.
Described a kind of aircraft assistance for lifting waterborne system is characterized in that: this aircraft assistance for lifting waterborne system can be used for the fixed wing aircraft landing of aircraft landing speed less than the maximum gait of march of speedboat.
Described a kind of aircraft assistance for lifting waterborne system also can be used for taking off and landing of vertical takeoff and landing (VTOL).Takeoff speed approaches zero during the taking off of vertical takeoff and landing (VTOL), and sinking speed also approaches zero during landing, and this moment, the speed of speedboat also approached zero, let fly away then or the aircraft that lands.The lifting autogyro is basic identical on principle in this and on the large-scale boat such as existing aircraft carrier, so " claims " of the present invention do not mention the aircraft of vertical takeoff and landing (VTOL).
Compare with present technology, the present invention is by being carrier with the speedboat, when taking off, manipulator on the speedboat is clamped aircraft, and aircraft and speedboat together quicken, reach takeoff speed after, when the lift that aircraft self produces was enough to support the gravity of aircraft, the speedboat manipulator was decontroled aircraft, takes off; During aircraft landing, command and control system designs an aircraft landing track and a speedboat travel track in real time according to the space relativeness and the speed of aircraft and speedboat, speedboat and aircraft are advanced and are prepared along track and land, aircraft slows down to sinking speed, and speedboat quickens to sinking speed, when aircraft and speedboat reach same speed, and when aircraft is positioned at the top of the manipulator on the speedboat, manipulator on the speedboat is clamped undercarriage, is decelerated to zero velocity, aircraft landing then together.Advantage of the present invention is to have solved aircraft lifting problem waterborne, and does not resemble the active service hydroairplane and change the original profile of aircraft, weight and other attribute because of device such as floating drum, also can not sacrifice other quality of aircraft.
The specific embodiment
The invention will be further described below in conjunction with the specific embodiment.
Implementation column 1
A kind of aircraft assistance for lifting waterborne system, this aircraft assistance for lifting waterborne system is a carrier with the speedboat, be equipped with on the speedboat identical with the undercarriage number can be in the certain space scope rapid-action manipulator.Speedboat is provided with induction system and command and control system, induction system can be sensed taking off of aircraft or landing information, can sense the space relativeness of aircraft and speedboat, can sense the relative velocity and the absolute velocitye of aircraft and speedboat, and send the information of sensing to command and control system.
When taking off, the manipulator on the speedboat is clamped aircraft, and aircraft and speedboat together quicken, after reaching takeoff speed, when the lift that aircraft self produces was enough to support the gravity of aircraft, command and control system was sent instruction to the speedboat manipulator, the speedboat manipulator is decontroled aircraft, takes off.
During aircraft landing, command and control system designs an aircraft landing track and a speedboat travel track in real time according to the space relativeness and the speed of aircraft and speedboat, speedboat and aircraft are advanced and are prepared along track and land, aircraft slows down to sinking speed, and speedboat quickens to sinking speed, when aircraft and speedboat reach same speed, and when aircraft is positioned at the top of the manipulator on the speedboat, manipulator on the speedboat is clamped aircraft, is decelerated to zero velocity, aircraft landing then together.
Claims (7)
1. aircraft assistance for lifting waterborne system, it is characterized in that: this aircraft assistance for lifting waterborne system is a carrier with the speedboat, have on the speedboat identical with the undercarriage number can be in the certain space scope rapid-action manipulator.
2. a kind of aircraft according to claim 1 assistance for lifting waterborne system, it is characterized in that: speedboat is provided with induction system, induction system can be sensed taking off of aircraft or landing information, the space relativeness of aircraft and speedboat can be sensed, the relative velocity and the absolute velocitye of aircraft and speedboat can be sensed.
3. a kind of aircraft according to claim 1 assistance for lifting waterborne system, it is characterized in that: speedboat is provided with command and control system, command and control system can obtain the information that induction system transmits, and can command the run action of control manipulator, speedboat and aircraft.
4. a kind of aircraft according to claim 1 assistance for lifting waterborne system, it is characterized in that: when taking off, manipulator on the speedboat is clamped undercarriage, aircraft and speedboat together quicken, after reaching takeoff speed, when the lift that aircraft self produces was enough to support the gravity of aircraft, command and control system was sent instruction to the speedboat manipulator, the speedboat manipulator is decontroled aircraft, takes off.
5. a kind of aircraft according to claim 1 assistance for lifting waterborne system, it is characterized in that: when aircraft landing, command and control system designs an aircraft landing track and a speedboat travel track in real time according to the space relativeness and the speed of aircraft and speedboat, speedboat and aircraft are advanced and are prepared along track and land, aircraft slows down to sinking speed, speedboat quickens to sinking speed, when aircraft and speedboat reach same speed, and when aircraft is positioned at the top of the manipulator on the speedboat, manipulator on the speedboat is clamped undercarriage, be decelerated to zero velocity, aircraft landing then together.
6. a kind of aircraft according to claim 1 assistance for lifting waterborne system is characterized in that: this aircraft assistance for lifting waterborne system can be used for the speed of taking off and takes off less than the fixed wing aircraft of the maximum gait of march of speedboat.
7. a kind of aircraft according to claim 1 assistance for lifting waterborne system is characterized in that: this aircraft assistance for lifting waterborne system can be used for the fixed wing aircraft landing of aircraft landing speed less than the maximum gait of march of speedboat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105170886A CN101992842A (en) | 2010-10-25 | 2010-10-25 | Water auxiliary take-off/landing system for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105170886A CN101992842A (en) | 2010-10-25 | 2010-10-25 | Water auxiliary take-off/landing system for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101992842A true CN101992842A (en) | 2011-03-30 |
Family
ID=43783727
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010105170886A Pending CN101992842A (en) | 2010-10-25 | 2010-10-25 | Water auxiliary take-off/landing system for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101992842A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615114A (en) * | 2019-09-17 | 2019-12-27 | 陈建武 | Method and device for assisting landing and landing of airplane |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4311290A (en) * | 1979-11-01 | 1982-01-19 | The United States Of America As Represented By The Secretary Of The Navy | Arrestment system |
| CN1204603A (en) * | 1997-07-03 | 1999-01-13 | 卢正直 | Land and ship-based take-off and landing vehicle for airplane and heliopter taxing, take-off and landing and corollary measure equipment |
| US7264204B1 (en) * | 2005-12-12 | 2007-09-04 | The United States Of America As Represented By The Secretary Of The Navy | Unmanned aerial vehicle catcher |
| US7568658B2 (en) * | 2006-04-05 | 2009-08-04 | Li Maxwell W | Aircraft emergency landing assist vehicle |
-
2010
- 2010-10-25 CN CN2010105170886A patent/CN101992842A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4311290A (en) * | 1979-11-01 | 1982-01-19 | The United States Of America As Represented By The Secretary Of The Navy | Arrestment system |
| CN1204603A (en) * | 1997-07-03 | 1999-01-13 | 卢正直 | Land and ship-based take-off and landing vehicle for airplane and heliopter taxing, take-off and landing and corollary measure equipment |
| US7264204B1 (en) * | 2005-12-12 | 2007-09-04 | The United States Of America As Represented By The Secretary Of The Navy | Unmanned aerial vehicle catcher |
| US7568658B2 (en) * | 2006-04-05 | 2009-08-04 | Li Maxwell W | Aircraft emergency landing assist vehicle |
Non-Patent Citations (2)
| Title |
|---|
| 马世强: "中国STOVL舰载机遐想", 《舰载武器》 * |
| 马威等: "海军通用无人机及其起降方式分析", 《飞航导弹》 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110615114A (en) * | 2019-09-17 | 2019-12-27 | 陈建武 | Method and device for assisting landing and landing of airplane |
| CN110615114B (en) * | 2019-09-17 | 2023-04-25 | 陈建武 | Auxiliary landing method and device for airplane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8485468B2 (en) | Ground-based apparatus for the take-off, landing and taxiing of aircraft | |
| CN105173073A (en) | Composite lift force type unmanned aerial vehicle realizing vertical take-off and landing | |
| CN201678037U (en) | Natural power levitation platform | |
| NZ592991A (en) | Aircraft system that enables ground traveling | |
| CN103803079A (en) | Small-size rotor aircraft | |
| CN203439258U (en) | Combined type rotor-wing aircraft | |
| CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
| CN103318406A (en) | Composite rotor craft | |
| CN106477060A (en) | Security landing-assistant rescuing system for undercarriage fault | |
| CN105564664A (en) | Ultra-short-range airplane takeoff method | |
| CN206243476U (en) | VTOL fixed-wing unmanned plane | |
| CN101214856A (en) | Safety self-saving device for vertically taking off and landing flyer | |
| CN206068176U (en) | A kind of nacelle arrangement of fixed-wing aerial survey unmanned plane | |
| CN101992842A (en) | Water auxiliary take-off/landing system for airplane | |
| CN204895867U (en) | Three unmanned navigation wares of dwelling | |
| CN203032936U (en) | Passenger helicopter | |
| CN204134213U (en) | Aeromodelling airplane VTOL power rack | |
| CN106915464A (en) | The landing-gear and mode of a kind of aircraft | |
| CN204473134U (en) | Arrow formula aircraft | |
| CN104210669A (en) | Plane takeoff mode and device | |
| CN106741934A (en) | Tandem coaxial double-oar tailstock formula VUAV | |
| CN202219839U (en) | Omnidirectional flight wing structure of vertically taking-off and landing aircraft | |
| CN204701766U (en) | Arrow formula vertical take-off and landing aircraft (VTOL aircraft) | |
| CN203419259U (en) | Micro tilt-rotor aircraft | |
| CN107315420A (en) | A kind of unmanned plane turning method |
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: 20110330 |