CN203854855U - Duct paddle helicopter equipment - Google Patents
Duct paddle helicopter equipment Download PDFInfo
- Publication number
- CN203854855U CN203854855U CN201420313773.0U CN201420313773U CN203854855U CN 203854855 U CN203854855 U CN 203854855U CN 201420313773 U CN201420313773 U CN 201420313773U CN 203854855 U CN203854855 U CN 203854855U
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- helicopter
- cabin
- duct
- ground
- duct oar
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Abstract
A duct paddle helicopter equipment comprises a helicopter, two transporters and a comprehensive cable, wherein one transporter is used for parking and transporting the helicopter, and the other transporter is used for carrying a generator set and providing electric power for the flight of the helicopter; the transporters transmit electric power to the helicopter through the comprehensive cable; the helicopter comprises electric power driven duct paddles, a cabin, a windlass and a driving operation panel, as well as an underframe and tyres; the underframe is fixedly mounted at the bottom of the cabin; the tyres are fixedly mounted at the bottom of the underframe. The duct paddle helicopter equipment provided by the utility model is light in helicopter body weight and safe, is applicable to aloft work or fire control and the rescue of trapped people, and is quite convenient.
Description
Technical field
The utility model relates to aloft work technical field, relates in particular to a kind of duct oar helicopter equipment.
Background technology
Aloft work equipment is widely used in the fields such as electric power, communication, disaster assistance, under the demand of different construction environments, the stationarity of aloft work equipment or the requirement of safety is all had nothing in common with each other.At present, most aerial platform adopts is that robotic arm elongate form reaches certain height and carries out operation, in height reach certain restriction, also be useful on the helicopter of aloft work, because the rotor volume of helicopter is larger, the more spacious driving that could be safe of required need for environment, or use sus-pension, very inconvenient, also stablize not and safety, if meet fire, need water spray rescue, the weight of the driving engine of pure helicopter and fuel tank self is added the weight of water tank, make its oil consumption power consumption more, and contained water tank water source is limited, be not suitable for continuing the disaster relief.
Utility model content
The purpose of this utility model is to propose light, the safe duct oar helicopter equipment of a kind of fuselage, is applicable to aloft work or fire control and disaster rescue and rescue trapped personnel, very convenient.
For reaching this object, the utility model by the following technical solutions:
A kind of duct oar helicopter equipment, comprises helicopter, transport trolley and comprehensive hawser, and described transport trolley is provided with two, and one for parking and transport described helicopter, and another portion is used for delivering generator set and provides electric power flight for described helicopter;
Described transport trolley is given described helicopter by described comprehensive hawser transferring electric power;
Described helicopter comprises driven by power duct oar, cabin, winch, driver behavior panel, underframe and tire, and described underframe is fixedly installed in the bottom in described cabin, and described tire is fixedly installed in the bottom of described underframe;
Described driven by power duct oar is arranged on the both sides in described cabin and drives the lifting in described cabin, described winch is arranged on the top in described cabin, described winch is controlled described comprehensive hawser, and described driver behavior panel is arranged in the cabin in described cabin and controls the motion of described helicopter.
Preferably, described driven by power duct oar is provided with two groups, one group is fixing group, described fixedly group is top wing, be fixedly installed in the both sides in described cabin, another group is activity group, and described movable group is lower wing, under to horizontal direction rotation to described top wing when parking and transporting, during work, rotation is to working orientation be connected in the counter-force pull bar that is arranged on helicopter bottom.
Preferably, described helicopter also comprises mechanical hand, and described cabin is fixed in one end of described mechanical hand, and other end movable telescopic ground pincers are grabbed skin.
Preferably, described mechanical hand is provided with two, is installed on respectively top and the bottom in described cabin, or left side and the right side in difference packing and described cabin.
Preferably, also comprise lifeline, described lifeline is controlled by described winch, and the bottom in described cabin is provided with life-saving window.
Preferably, described cabin is provided with reserve tank and water injecting system, and described reserve tank also comprises force (forcing) pump, and described reserve tank provides water source by described force (forcing) pump for described water injecting system.
Preferably, also comprise ground high pressure pump truck, described ground high pressure pump truck comprises water tank, and described comprehensive hawser comprises high service pipe, and described water tank provides to described reserve tank by described high service pipe, and described high service pipe is also provided with force (forcing) pump midway.
Preferably, described helicopter also comprises driving surface guardrail, and described driving surface guardrail is installed on described cabin.
Preferably, also comprise ground remote control, described comprehensive hawser also comprises ground driving remote-control communication cord, and described ground remote control drives by described ground the motion that remote-control communication cord is controlled described helicopter.
Preferably, described cabin is also installed with camera, and described camera is provided with two, a top that is arranged on described cabin, and another is arranged on the bottom in described cabin.
The beneficial effects of the utility model: the electric power that 1, relies on terrestrial power generation unit to provide takes off, and fuselage is lighter; 2, use driven by power duct oar, can improve the safety of helicopter, when lifting, be difficult for getting to object around; 3, two groups of four Ducted helicopters more can provide the stable qualitative energy of overhead suspension, and upper arm and underarm mechanical hand can extend skin pincers and grab and fix, for fire-fighting fire extinguishing and air rescue facilitate.
Accompanying drawing explanation
Fig. 1 is the schematic top plan view of the helicopter of an embodiment of the present utility model;
Fig. 2 is the structural representation of an embodiment of the present utility model;
Fig. 3 is the structural representation that the helicopter of an embodiment of the present utility model is parked;
Fig. 4 is the structural representation of an embodiment of the present utility model.
Wherein: helicopter 1, transport trolley 2, comprehensive hawser 3, ground high pressure pump truck 4, driven by power duct oar 11, cabin 12, winch 13, driver behavior panel 14, mechanical hand 15, underframe 16, tire 17, counter-force pull bar 18, water tank 41, lifeline 120, life-saving window 121, reserve tank 122, upper arm 151, underarm 152.
The specific embodiment
Below in conjunction with accompanying drawing and by the specific embodiment, further illustrate the technical solution of the utility model.
A kind of duct oar helicopter equipment, comprises helicopter 1, transport trolley 2 and comprehensive hawser 3, and described transport trolley 2 is provided with two, and one for parking and transport described helicopter 1, and another portion is used for delivering generator set and provides electric power flight for described helicopter 1;
Described transport trolley 2 is given described helicopter 1 by described comprehensive hawser 3 transferring electric powers;
Described helicopter 1 comprises driven by power duct oar 11, cabin 12, winch 13, driver behavior panel 14, underframe 16 and tire 17, and described underframe 16 is fixedly installed in the bottom in described cabin 12, and described tire 17 is fixedly installed in the bottom of described underframe 16;
Described driven by power duct oar 11 is arranged on the both sides in described cabin 12 and drives the lifting in described cabin 12, described winch 13 is arranged on the top in described cabin 12, described winch 13 is controlled described comprehensive hawser 3, and described driver behavior panel 14 is arranged in the cabin in described cabin 12 and controls the motion of described helicopter 1.
Duct oar helicopter equipment of the present utility model comprises helicopter 1, transport trolley 2 and comprehensive hawser 3, and helicopter 1 provides power supply by the generator set of the transport trolley 2 on ground, fuselage is removed from driving engine and fuel tank are installed, and greatly alleviates fuselage weight, improves the weight of standing up.The electric power that relies on terrestrial power generation unit to provide takes off to high-rise building external and carries out fire control and disaster rescue and rescue trapped personnel, also can be to the main equipment maintenance of FRAME ON THE ROOF OF HIGH-RISE BUILDING, change landing transportation is provided.In helicopter 1, be provided with driver behavior panel 14, in cabin, personnel can conveniently control the motion of helicopter 1.Winch 13 is connected with comprehensive hawser 3, makes helicopter 1 not affected by aerial hawser.While not using helicopter 1, when parking or transporting, comprehensive hawser 3 can be drawn over to one's side in folding and unfolding hawser frame by traction machine.Helicopter 1 uses driven by power duct oar 11, can improve the safety of helicopter 1, is difficult for getting to object around when lifting.The setting of underframe 16 and tire 17 can be parked on transport trolley 2 by pulsation-free helicopter 1 when parking and transport.Comprehensive hawser 3 comprises load-bearing wires rope and cable.
Preferably, described driven by power duct oar 11 is provided with two groups, one group is fixing group, described fixedly group is top wing, be fixedly installed in the both sides in described cabin 2, another group is activity group, and described movable group is lower wing, under to horizontal direction rotation to described top wing when parking and transporting, during work, rotation is to working orientation be connected in the counter-force pull bar 18 that is arranged on helicopter bottom.Be provided with two groups of driven by power duct oars 11, two groups of four Ducted helicopters more can provide the stable qualitative energy of overhead suspension.Movable group is lower wing, when parking and transporting, to horizontal direction, rotate to described top wing, the overall width of the driven by power duct oar 11 of helicopter 1 surpasses the width of transport trolley 2 when avoiding transporting, and its length is also controlled in the length range in compartment of transport trolley 2.Arranging of counter-force pull bar 18 can be fixed movable group lower wing, makes driven by power duct oar 11 structures structure when flight more firm.
Preferably, described helicopter 1 also comprises mechanical hand 15, and described cabin 12 is fixed in one end of described mechanical hand 15, and other end movable telescopic ground pincers are grabbed skin.Be provided with mechanical hand 15, movable end can extend skin pincers and grabs and fix, for fire-fighting fire extinguishing and air rescue or aerial work facilitate.
Preferably, described mechanical hand 15 is provided with two, is installed on respectively top and the bottom in described cabin 12, or left side and the right side in difference packing and described cabin 12.Be provided with mechanical hand 15 and be provided with two, be installed on respectively top and the bottom in described cabin 12, or left side and the right side in difference packing and described cabin 12, mechanical hand 15 is provided with two, function is abundanter, can multi-functionally operate, more steady when being arranged on the left and right sides and can making helicopter 1 hover aloft.A top that is arranged on described cabin 12 is upper arm 151 as shown in Figure 1, and the bottom that another is arranged on described cabin 2 is underarm 152.
Preferably, also comprise lifeline 120, described lifeline 120 is controlled by described winch 13, and the bottom in described cabin 12 is provided with life-saving window 121.While being used for rescuing trapped personnel, due to engine room inside limited space, the trapped personnel of rescuing can not rest in cabin for a long time, at this moment can allow the trapped personnel of rescuing by bottom life-saving window, along lifeline 120 safety jaws, drop to ground successively.
Preferably, described cabin 12 is provided with reserve tank 122 and water injecting system, and described reserve tank 122 also comprises force (forcing) pump, and described reserve tank 122 provides water source by described force (forcing) pump for described water injecting system.Cabin 12 is provided with reserve tank 122 and water injecting system, can carry out fire control and disaster rescue.
Preferably, also comprise ground high pressure pump truck 4, described ground high pressure pump truck 4 comprises water tank 41, and described comprehensive hawser 3 comprises high service pipe, described water tank 41 provides to described reserve tank 122 by described high service pipe, and described high service pipe is also provided with force (forcing) pump 31 midway.The high service pipe that is provided with reserve tank 122 and comprehensive hawser 3 in cabin is also able to continuously water source is provided, for high building fire fighting fire extinguishing provides sufficient water source.If fire zone height surpasses ground high pressure head of pump, can also continue to provide high-pressure water by the force (forcing) pump midway 31 that is arranged on high service pipe.
Preferably, described helicopter 1 also comprises driving surface guardrail, and described driving surface guardrail is installed on described cabin 12.High-altitude personnel's safety while being provided with driving surface guardrail raising aloft work.
Preferably, also comprise ground remote control, described comprehensive hawser 3 also comprises ground driving remote-control communication cord, and described ground remote control drives by described ground the motion that remote-control communication cord is controlled described helicopter 1.Drive manner is also provided with ground remote control, and ground staff can drive the motion that remote-control communication cord is controlled helicopter 1 by ground remote control and ground.During convenient rescue, ground staff controls, and persons on board can drop into rescue comprehensively.
Preferably, described cabin 12 is also installed with camera 124, and described camera is provided with two, a top that is arranged on described cabin 12, and another is arranged on the bottom in described cabin 12.Be provided with camera 124, facilitate ground staff when controlling helicopter 1, the position at its place is located accurately and observed, avoid because the impact of diff-H on human eye location.
Know-why of the present utility model has below been described in conjunction with specific embodiments.These are described is in order to explain principle of the present utility model, and can not be interpreted as by any way the restriction to the utility model protection domain.Explanation based on herein, those skilled in the art does not need to pay performing creative labour can associate other specific embodiment of the present utility model, within these modes all will fall into protection domain of the present utility model.
Claims (10)
1. a duct oar helicopter is equipped, it is characterized in that: comprise helicopter, transport trolley and comprehensive hawser, described transport trolley is provided with two, and one for parking and transport described helicopter, and another portion is used for delivering generator set and provides electric power flight for described helicopter;
Described transport trolley is given described helicopter by described comprehensive hawser transferring electric power;
Described helicopter comprises driven by power duct oar, cabin, winch, driver behavior panel, underframe and tire, and described underframe is fixedly installed in the bottom in described cabin, and described tire is fixedly installed in the bottom of described underframe;
Described driven by power duct oar is arranged on the both sides in described cabin and drives the lifting in described cabin, described winch is arranged on the top in described cabin, described winch is controlled described comprehensive hawser, and described driver behavior panel is arranged in the cabin in described cabin and controls the motion of described helicopter.
2. duct oar helicopter according to claim 1 is equipped, it is characterized in that: described driven by power duct oar is provided with two groups, one group is fixing group, described fixedly group is top wing, be fixedly installed in the both sides in described cabin, another group is activity group, and described movable group is lower wing, under to horizontal direction rotation to described top wing when parking and transporting, during work, rotation is to working orientation be connected in the counter-force pull bar that is arranged on helicopter bottom.
3. duct oar helicopter equipment according to claim 1, is characterized in that: described helicopter also comprises mechanical hand, and described cabin is fixed in one end of described mechanical hand, and other end movable telescopic ground pincers are grabbed skin.
4. duct oar helicopter equipment according to claim 3, is characterized in that: described mechanical hand is provided with two, is installed on respectively top and the bottom in described cabin, or left side and the right side in difference packing and described cabin.
5. duct oar helicopter equipment according to claim 1, is characterized in that: also comprise lifeline, described lifeline is controlled by described winch, and the bottom in described cabin is provided with life-saving window.
6. duct oar helicopter according to claim 1 equipment, is characterized in that: described cabin is provided with reserve tank and water injecting system, and described reserve tank also comprises force (forcing) pump, and described reserve tank provides water source by described force (forcing) pump for described water injecting system.
7. duct oar helicopter according to claim 6 is equipped, it is characterized in that: also comprise ground high pressure pump truck, described ground high pressure pump truck comprises water tank, described comprehensive hawser comprises high service pipe, described water tank provides to described reserve tank by described high service pipe, and described high service pipe is also provided with force (forcing) pump midway.
8. duct oar helicopter equipment according to claim 1, is characterized in that: described helicopter also comprises driving surface guardrail, and described driving surface guardrail is installed on the side in described cabin.
9. duct oar helicopter according to claim 1 is equipped, it is characterized in that: also comprise ground remote control, described comprehensive hawser also comprises ground driving remote-control communication cord, and described ground remote control drives by described ground the motion that remote-control communication cord is controlled described helicopter.
10. duct oar helicopter equipment according to claim 9, is characterized in that: described cabin is also installed with camera, and described camera is provided with two, a top that is arranged on described cabin, and another is arranged on the bottom in described cabin.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420313773.0U CN203854855U (en) | 2014-06-12 | 2014-06-12 | Duct paddle helicopter equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420313773.0U CN203854855U (en) | 2014-06-12 | 2014-06-12 | Duct paddle helicopter equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203854855U true CN203854855U (en) | 2014-10-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420313773.0U Expired - Fee Related CN203854855U (en) | 2014-06-12 | 2014-06-12 | Duct paddle helicopter equipment |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203854855U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354858A (en) * | 2014-11-10 | 2015-02-18 | 成都好飞机器人科技有限公司 | Agricultural multi-rotor unmanned machine |
| CN104743105A (en) * | 2015-03-31 | 2015-07-01 | 马鞍山市赛迪智能科技有限公司 | Aircraft for rescue escape |
| CN104800996A (en) * | 2015-03-31 | 2015-07-29 | 湘潭大学 | Flying equipment for high-rise firefighting |
| CN105173108A (en) * | 2015-09-20 | 2015-12-23 | 孙正鼐 | High-rise fire rescue flight cabin |
| CN106494610A (en) * | 2016-09-30 | 2017-03-15 | 成都尚智恒达科技有限公司 | A kind of traffic tour unmanned plane |
| CN110667846A (en) * | 2019-10-10 | 2020-01-10 | 闫连民 | Vehicle-mounted unmanned aerial vehicle fire rescue system |
-
2014
- 2014-06-12 CN CN201420313773.0U patent/CN203854855U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354858A (en) * | 2014-11-10 | 2015-02-18 | 成都好飞机器人科技有限公司 | Agricultural multi-rotor unmanned machine |
| CN104743105A (en) * | 2015-03-31 | 2015-07-01 | 马鞍山市赛迪智能科技有限公司 | Aircraft for rescue escape |
| CN104800996A (en) * | 2015-03-31 | 2015-07-29 | 湘潭大学 | Flying equipment for high-rise firefighting |
| CN104800996B (en) * | 2015-03-31 | 2018-09-07 | 湘潭大学 | High level fire fighting flight equipment |
| CN105173108A (en) * | 2015-09-20 | 2015-12-23 | 孙正鼐 | High-rise fire rescue flight cabin |
| CN106494610A (en) * | 2016-09-30 | 2017-03-15 | 成都尚智恒达科技有限公司 | A kind of traffic tour unmanned plane |
| CN110667846A (en) * | 2019-10-10 | 2020-01-10 | 闫连民 | Vehicle-mounted unmanned aerial vehicle fire rescue system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141001 Termination date: 20190612 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |