CN103274041A - Lifting suspension aircraft - Google Patents
Lifting suspension aircraft Download PDFInfo
- Publication number
- CN103274041A CN103274041A CN2013101919381A CN201310191938A CN103274041A CN 103274041 A CN103274041 A CN 103274041A CN 2013101919381 A CN2013101919381 A CN 2013101919381A CN 201310191938 A CN201310191938 A CN 201310191938A CN 103274041 A CN103274041 A CN 103274041A
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- motor
- chain barrel
- suspension
- tapered sleeve
- lifting
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Abstract
The invention relates to the lifting and flight field, in particular to a suspension device used for flight and a lifting suspension aircraft which is applied to aerial photography and firefighting and also can be used as a firefighting assisting device. The lifting suspension aircraft is characterized in that a landing platform is designed to be arranged at the upper end of a supporting frame. A turning wheel is fixed below the supporting frame and matched with a chain cylinder. One end of the chain cylinder is wound on a winding machine of a winding cylinder and the other end of the chain cylinder penetrates through the middle of the landing platform and is further connected with a cone sleeve below the suspension device. The suspension device comprises an annular suspension shell body. A motor is fixed in the middle of the suspension shell body through a supporting rod. The output shaft of the upper end of the motor is combined with a propeller. A shell body of the lower end of the motor is connected with the cone sleeve. A hydraulic system is installed in the cone sleeve and combined with the output shaft of the lower end of the motor. The output end of a hydraulic cylinder of the hydraulic system is connected with a connection rod through a joint. The connection rod is further combined with vanes. The chain cylinder is connected below the cone sleeve. A circuit wire is arranged in the chain cylinder.
Description
Technical field
The present invention relates to lifting and flight field, relate in particular to for flight a kind of levitation device, relate to especially the hovering flight device take photo by plane and fire-fighting in utilization, can be used as the fire-fighting auxiliary equipment again, be a kind of hovering flight device of lifting.
Background technology
Since oneth century, the human machine that uses promotes, draws, oneself serving the human height that can't arrive itself.Well-known flight is very strict for the requirement of machinery, and institute is so that the flight field can not greatly leap with going on foot.Show in the fire-fighting that its drawback also is appreciiable.Aerial ladder is used for putting out a fire to save life and property of fire of high-rise building by the elevator scoop turntable in fire-fighting.But the use of aerial ladder but exists defective: the heavy volume of the load wagon of aerial ladder is big, this makes that the operation of elevator scoop turntable can not be comprehensive, autonomous reverses its direction, cause fire fighting efficient slow, bring about great losses for economy, personal casualty, the greatest drawback that aerial ladder exists is existing exactly can only to reach more than 100 meter highly at most, and its height and the scope of turning are far from being enough.So study a kind of fire-fighting auxiliary equipment, safe and practical, easy to operate that can be used for, it is extremely necessary can be used for field lifting hovering flight device such as marine monitoring again.
Summary of the invention
For solving the problems of the technologies described above, the invention provides a kind of hovering flight device of lifting.
The following solution that the present invention takes is:
Comprise supporting seat, support, landing stage, winch, runner, chain barrel, tapered sleeve, motor, the suspension housing, fin, it is characterized in that: support upper end design one place's landing stage, fixedly there is runner the support below, runner is combined with chain barrel, one end chain barrel is wrapped on the reel of winch, other end chain barrel passes the centre of landing stage and further is connected with the tapered sleeve of suspension device below, suspension device comprises the suspension housing that ring is circular, the centre of suspension housing is by the strut bar fixed electrical machinery, motor upper end output shaft combines with screw propeller, the housing of motor lower end connects tapered sleeve, and hydraulic efficiency pressure system is installed in the tapered sleeve, and this hydraulic efficiency pressure system combines with motor lower end output shaft, the hydraulic actuating cylinder mouth of this hydraulic efficiency pressure system connects connecting rod by the joint, connecting rod is further combined with fin, and the below of described tapered sleeve connects chain barrel, chain barrel built-in circuit lead.
Described winch is installed on the supporting seat, comprises that electrical motor, plunging joint, drg, gear case and reel form, and an end of this reel is provided with current colector, and the built-in circuit lead of current colector and chain barrel is connected, current colector and then combine with brush.
Described chain barrel designs both sides inclination breach respectively by the jacket casing two ends, the two ends that form this jacket casing are respectively bossing, each jacket casing arranges two place's active sections by this bossing and is connected to each other and forms, the arrangement that misplaces successively of the jacket casing of connection and the active section between the jacket casing.
During use, the present invention can be fixed on self-propelled vehicle or the boats and ships, by the supply of the electrical generator out-put supply that matches and the further circuit of control winch and suspension device thereof, the winch purpose is used for reclaiming or discharging chain barrel, suspension device combines with screw propeller as the thrust that makes progress by motor, suspension device and can finish in stated limit mobile, for example, directly install flexible pipe additional at chain barrel as the utilization in the fire-fighting, the quill that flexible pipe one end arranges on reel is combined, and quill connects water source or fire-fighting liquid, and flexible pipe one end is connected with the interior fixing nozzle of tapered sleeve on the suspension device, for example, as tapered sleeve on the suspension device of taking photo by plane the instrument etc. of taking photo by plane is installed.Can control suspension device orientation and shift position by regulating fin.
Description of drawings
Fig. 1 is the hovering flight device constructional drawing of a kind of lifting of the present invention.
Mark among the figure: 1-supporting seat, 2-support, 3-landing stage, 4-winch, 5-runner, 6-chain barrel, 7-tapered sleeve, 8-motor, 9-suspension housing, 10-fin.
The specific embodiment
Below be the embodiment of the invention:
In Fig. 1, comprise supporting seat 1, support 2, landing stage 3, winch 4, runner 5, chain barrel 6, tapered sleeve 7, motor 8, suspension housing 9, fin 10, it is characterized in that: place's landing stage 3 is designed in support 2 upper ends, fixedly there is runner 5 support 2 belows, runner 5 and chain barrel 6 combinations, one end chain barrel 6 is wrapped on the reel of winch 4, other end chain barrel 6 passes the centre of landing stage 3 and further is connected with the tapered sleeve 7 of suspension device below, suspension device comprises the suspension housing 9 that ring is circular, the centre of suspension housing 9 is by strut bar fixed electrical machinery 8, motor 8 upper end output shafts combine with screw propeller, the housing of motor 8 lower ends connects tapered sleeve 7, in the tapered sleeve 7 hydraulic efficiency pressure system is installed, this hydraulic efficiency pressure system combines with motor 8 lower end output shafts, and the hydraulic actuating cylinder mouth of this hydraulic efficiency pressure system connects connecting rod by the joint, and connecting rod is further combined with fin 10, the below of described tapered sleeve 7 connects chain barrel 6, chain barrel 6 built-in circuit leads.
Described winch 4 is installed on the supporting seat 1, comprises that electrical motor, plunging joint, drg, gear case and reel form, and an end of this reel is provided with current colector, and the built-in circuit lead of current colector and chain barrel is connected, current colector and then combine with brush.
Described chain barrel 6 designs both sides inclination breach respectively by the jacket casing two ends, the two ends that form this jacket casing are respectively bossing, each jacket casing arranges two place's active sections by this bossing and is connected to each other and forms, the arrangement that misplaces successively of the jacket casing of connection and the active section between the jacket casing.
Certainly, above-mentioned concrete enforcement is not to be restriction of the present invention, and those of ordinary skill also can be made some and change in essential scope of the present invention, and all technical schemes that mapping mode obtains that adopts equivalence to replace or be equal to all drop in protection scope of the present invention.
Claims (3)
1. the hovering flight device of a lifting, comprise supporting seat, support, landing stage, winch, runner, chain barrel, tapered sleeve, motor, the suspension housing, fin, it is characterized in that: support upper end design one place's landing stage, fixedly there is runner the support below, runner is combined with chain barrel, one end chain barrel is wrapped on the reel of winch, other end chain barrel passes the centre of landing stage and further is connected with the tapered sleeve of suspension device below, suspension device comprises the suspension housing that ring is circular, the centre of suspension housing is by the strut bar fixed electrical machinery, motor upper end output shaft combines with screw propeller, the housing of motor lower end connects tapered sleeve, hydraulic efficiency pressure system is installed in the tapered sleeve, this hydraulic efficiency pressure system combines with motor lower end output shaft, and the hydraulic actuating cylinder mouth of this hydraulic efficiency pressure system connects connecting rod by the joint, and connecting rod is further combined with fin, the below of described tapered sleeve connects chain barrel, chain barrel built-in circuit lead.
2. according to the hovering flight device of the described a kind of lifting of claim 1, it is characterized in that: winch is installed on the supporting seat, comprise electrical motor, plunging joint, drg, gear case and reel composition, one end of this reel is provided with current colector, the built-in circuit lead of current colector and chain barrel is connected, current colector and then combine with brush.
3. according to the hovering flight device of the described a kind of lifting of claim 1, it is characterized in that: chain barrel designs both sides inclination breach respectively by the jacket casing two ends, the two ends that form this jacket casing are respectively bossing, each jacket casing arranges two place's active sections by this bossing and is connected to each other and forms, the arrangement that misplaces successively of the jacket casing of connection and the active section between the jacket casing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101919381A CN103274041A (en) | 2013-05-23 | 2013-05-23 | Lifting suspension aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101919381A CN103274041A (en) | 2013-05-23 | 2013-05-23 | Lifting suspension aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103274041A true CN103274041A (en) | 2013-09-04 |
Family
ID=49056705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013101919381A Pending CN103274041A (en) | 2013-05-23 | 2013-05-23 | Lifting suspension aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103274041A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111665061A (en) * | 2020-05-15 | 2020-09-15 | 广东博智林机器人有限公司 | Rack mechanism and system suitable for steering wheel test |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3217097A (en) * | 1961-08-09 | 1965-11-09 | Fritz K Pauli | Tethered hovering platform for aerial surveillance |
| US5295643A (en) * | 1992-12-28 | 1994-03-22 | Hughes Missile Systems Company | Unmanned vertical take-off and landing, horizontal cruise, air vehicle |
| CN1125677A (en) * | 1995-06-23 | 1996-07-03 | 阮明振 | Auto-stabilization type flying top |
| DE19808777A1 (en) * | 1998-03-03 | 1999-09-09 | Quaas | Annular free flight body used as carrier for observation and measurement systems |
| CN1647998A (en) * | 2003-07-30 | 2005-08-03 | C.R.F.阿西安尼顾问公司 | Flying machine |
| US20100108807A1 (en) * | 2008-10-31 | 2010-05-06 | University Of Kansas | Tethered hovering platform |
| CN101866711A (en) * | 2010-06-22 | 2010-10-20 | 董翔 | Snake-like anchor chain and application thereof |
| CN102458987A (en) * | 2009-04-06 | 2012-05-16 | 天空智慧有限公司 | System, floating unit and method for elevating payloads |
| CN202449203U (en) * | 2011-12-21 | 2012-09-26 | 航宇救生装备有限公司 | Mooring hot gas airship anchoring device |
-
2013
- 2013-05-23 CN CN2013101919381A patent/CN103274041A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3217097A (en) * | 1961-08-09 | 1965-11-09 | Fritz K Pauli | Tethered hovering platform for aerial surveillance |
| US5295643A (en) * | 1992-12-28 | 1994-03-22 | Hughes Missile Systems Company | Unmanned vertical take-off and landing, horizontal cruise, air vehicle |
| CN1125677A (en) * | 1995-06-23 | 1996-07-03 | 阮明振 | Auto-stabilization type flying top |
| DE19808777A1 (en) * | 1998-03-03 | 1999-09-09 | Quaas | Annular free flight body used as carrier for observation and measurement systems |
| CN1647998A (en) * | 2003-07-30 | 2005-08-03 | C.R.F.阿西安尼顾问公司 | Flying machine |
| US20100108807A1 (en) * | 2008-10-31 | 2010-05-06 | University Of Kansas | Tethered hovering platform |
| CN102458987A (en) * | 2009-04-06 | 2012-05-16 | 天空智慧有限公司 | System, floating unit and method for elevating payloads |
| CN101866711A (en) * | 2010-06-22 | 2010-10-20 | 董翔 | Snake-like anchor chain and application thereof |
| CN202449203U (en) * | 2011-12-21 | 2012-09-26 | 航宇救生装备有限公司 | Mooring hot gas airship anchoring device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111665061A (en) * | 2020-05-15 | 2020-09-15 | 广东博智林机器人有限公司 | Rack mechanism and system suitable for steering wheel test |
| CN111665061B (en) * | 2020-05-15 | 2022-02-22 | 广东博智林机器人有限公司 | Rack mechanism and system suitable for steering wheel test |
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| 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: 20130904 |