CN110077584A - A kind of DCB Specimen high-rise life saving aircraft - Google Patents
A kind of DCB Specimen high-rise life saving aircraft Download PDFInfo
- Publication number
- CN110077584A CN110077584A CN201910408424.4A CN201910408424A CN110077584A CN 110077584 A CN110077584 A CN 110077584A CN 201910408424 A CN201910408424 A CN 201910408424A CN 110077584 A CN110077584 A CN 110077584A
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- CN
- China
- Prior art keywords
- propeller hub
- life saving
- equipment body
- propeller
- dcb specimen
- 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
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- 239000000463 material Substances 0.000 claims description 3
- 230000005484 gravity Effects 0.000 abstract description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000872 buffer Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- 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
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/062—Belts or other passenger restraint means for passenger seats
-
- 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
- B64D31/00—Power plant control; Arrangement thereof
- B64D31/02—Initiating means
- B64D31/04—Initiating means actuated personally
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
The invention discloses a kind of DCB Specimen high-rise life saving aircraft, it is related to high-rise life saving technical field, cockpit is offered on the equipment body, safety seat is mounted in the cockpit, the both ends side wall of the cockpit is equipped with handle, the lower end two sides of the equipment body are chimeric headlight, the bottom end two sides of the equipment body are welded with bumper bracket, the top of the equipment body, which is run through, drive shaft, the driving the tip of the axis is socketed with wind deflector, and the first propeller hub and the second propeller hub are fixed in the drive shaft.The present invention uses DCB Specimen, keeps equipment lift high, can be made the blade of no flapping hinge, efficiency improves, flight speed correspondinglys increase, no antitorque rotor, due to not having tail-rotor, therefore full machine compact dimensions, whole power of engine are all used to drive rotor, improve the safety of helicopter nap of the earth flight, due to allowing gravity motion apart from larger, mobility increased, good security.
Description
Technical field
The present invention relates to high-rise life saving technical field, in particular to a kind of DCB Specimen high-rise life saving aircraft.
Background technique
Super high-rise building appearance scene, but security against fire hidden danger, surface subsidence and environment, the energy, traffic etc. can be caused
A series of relevant issues, it would be highly desirable to cause to pay high attention to.When facing a danger and rescuing not in time, save oneself be survive it is unique go out
Road, and one of saving oneself is exactly by escape equipment far from danger zone.
The escape device for high-rise buildings of self-rescue mainly has electronic fixed and two kinds of forms of Portable slowlanding device both at home and abroad at present,
It is electronic it is fixed provide lifting drive by motor, this escape apparatus there are volumes it is big, structure is complicated, at high cost the disadvantages of, it is inconvenient
It promotes, it is often more important that when the disasters such as fire occur, the phenomenon that being frequently accompanied by power failure, therefore in cases of emergency such as fire
Under often have no usage；Portable lifting device can only escape to disaster scene when happening suddenly fire in the following, cannot be far from disaster
Scene, above two self-rescue high-rise escape apparatus since disadvantage mentioned above is difficult to promote the use of, those skilled in the art provide
A kind of DCB Specimen high-rise life saving aircraft, to solve the problems mentioned in the above background technology.
Summary of the invention
The purpose of the present invention is to provide a kind of DCB Specimen high-rise life saving aircraft, to solve to propose in above-mentioned background technique
The problem of.
To achieve the above object, the technical scheme adopted by the invention is as follows:
A kind of DCB Specimen high-rise life saving aircraft, including equipment body offer cockpit on the equipment body, described
Safety seat is mounted in cockpit, the both ends side wall of the cockpit is equipped with handle, and the lower end two sides of the equipment body are embedding
Conjunction has headlight, and the bottom end two sides of the equipment body are welded with bumper bracket, and the top of the equipment body, which is run through, drive shaft, institute
State driving the tip of the axis and be socketed with wind deflector, be fixed with the first propeller hub and the second propeller hub in the drive shaft, and the first propeller hub and
It is fixed with shaft set in drive shaft between second propeller hub, the both ends of first propeller hub are equipped with the first propeller, and described second
The both ends of propeller hub are equipped with the second propeller, and the both ends of the shaft set are equipped with balancing pole.
As above-mentioned technical proposal to further describe: the safety seat is equipped with air bag, and airbag design by back
Corrugated structure, the safety seat is equipped with safety belt, and safety belt one end is fixed on by back, and the other end is fixed on bottom
On end, the bottom end two sides of the safety seat are welded with baffle, and are placed with cushion on safety seat bottom end.
As above-mentioned technical proposal to further describe: the bumper bracket is made of column, feet and sleeve, neutral
The upper end of column is socketed in sleeve, and the lower end of column is socketed in feet.
It is as above-mentioned technical proposal to further describe: spring to be equipped between the column and feet, and spring is fixed on
The inner bottom of feet.
As above-mentioned technical proposal to further describe: the handle design is at horizontal positioned L-type structure, and in handle
Top be equipped with control button.
As above-mentioned technical proposal to further describe: first propeller hub and the second propeller hub are divided into upper layer and lower layer, and
One propeller and the second propeller are clipped in respectively between the first propeller hub and the upper layer and lower layer of the second propeller hub, the top of first propeller hub
Hub cap is equipped at portion center.
As above-mentioned technical proposal to further describe: the both ends of the balancing pole are chimeric clump weight, and counterweight
Block uses lead material die cast.
The invention has the following beneficial effects:
1, compared with prior art, this programme uses DCB Specimen, keeps equipment lift high, can be made the paddle of no flapping hinge
Leaf, efficiency improve, and flight speed correspondinglys increase, no antitorque rotor, due to there is no tail-rotor, full machine compact dimensions, engine
Whole power are all used to drive rotor, improve the safety of helicopter nap of the earth flight, due to allowing gravity motion apart from larger,
Mobility increased, and manipulate simple, good security, for crowd of the Working Life in skyscraper encounter fire,
A kind of new best-effort path and special equipment are provided when the disaster accidents such as shake, when fundamentally overcoming him and rescuing formula and delay
Between, the power failure of electronic self-rescue be not available cannot be far from disaster scene with portable self-rescue the shortcomings that.
2, compared with prior art, this programme disposes escape personnel by the cockpit of setting, by safety seat come
Life safety, while the handle being arranged is effectively ensured in fixed user of service, the protection of safety belt and baffle, on the one hand can be to make
The function of holding body is provided with personnel, while being equipped with control button on handle, for starting, and adjusts escape equipment itself
Velocity magnitude.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of DCB Specimen high-rise life saving aircraft；
Fig. 2 is a kind of schematic diagram of safety seat in DCB Specimen high-rise life saving aircraft；
Fig. 3 is centrifuged the schematic diagram of bumper bracket in wind for a kind of multi-direction blast type.
In figure: 1, the first propeller；2, balancing pole；3, the second propeller；4, handle；5, cockpit；6, headlight；7, it buffers
Frame；8, the first propeller hub；9, shaft set；10, drive shaft；11, the second propeller hub；12, wind deflector；13, safety seat；14, equipment master
Body；15, air bag；16, cushion；17, safety belt；18, baffle；19, column；20, feet；21, sleeve；22, spring.
Specific embodiment
Referring to Fig.1-3, a kind of DCB Specimen high-rise life saving aircraft, including equipment body 14 offer on equipment body 14
Cockpit 5, safety seat 13 is mounted in cockpit 5, and the both ends side wall of cockpit 5 is equipped with handle 4, the lower end of equipment body 14
Two sides are chimeric headlight 6, and the bottom end two sides of equipment body 14 are welded with bumper bracket 7, and the top of equipment body 14, which is run through, driving
Axis 10, the end of drive shaft 10 are socketed with wind deflector 12, and the first propeller hub 8 and the second propeller hub 11, and are fixed in drive shaft 10
Shaft set 9 is fixed in drive shaft 10 between one propeller hub 8 and the second propeller hub 11, the both ends of the first propeller hub 8 are equipped with the first spiral
Paddle 1, the both ends of the second propeller hub 11 are equipped with the second propeller 3, and the both ends of shaft set 9 are equipped with balancing pole 2.
Safety seat 13 is equipped with air bag 15 by back, and air bag 15 is designed to wave structure, sets on safety seat 13
There is safety belt 17, and 17 one end of safety belt is fixed on by back, the other end is fixed on bottom end, the bottom end two sides of safety seat 13
It is welded with baffle 18, and is placed with cushion 16 on 13 bottom end of safety seat, in the design, air bag 15 mainly protects user of service's ridge
Vertebra preserves from, and does corrugated raising comfort level while improving intensity, and safety belt 17 is important safeguard measure, and baffle 18 prevents
User of service's body inclination；
Bumper bracket 7 is made of column 19, feet 20 and sleeve 21, and the upper end of central post 19 is socketed in sleeve 21,
The lower end of column 19 is socketed in feet 20, and after device lands, impact force is transmitted to first on sleeve 21, is made under sleeve 21
It drops, the air compression in such sleeve 21 carries out bradyseism, is simultaneously from the reaction force on ground, moves upwards feet 20, but
Due to gravity factor, then column 19 is caused to decline the bradyseism again of compressed spring 22；
Spring 22 is equipped between column 19 and feet 20, and spring 22 is fixed on the inner bottom of feet 20, spring 22 is main
Eliminate the reaction force on ground；
Handle 4 is designed to horizontal positioned L-type structure, and is equipped with control button at the top of handle 4, and user of service passes through
It grabs the progress body of handle 4 to be auxiliarily fixed, oneself control equipment, the control button designed on handle 4 can open equipment；
First propeller hub 8 and the second propeller hub 11 divide for upper layer and lower layer, and the first propeller 1 and the second propeller 3 are clipped in respectively
Between first propeller hub 8 and the upper layer and lower layer of the second propeller hub 11, hub cap is equipped at the top center of the first propeller hub 8, which is just
In connection and later period detachable maintaining, hub cap prevents first propeller hub 8 to be detached from；
The both ends of balancing pole 2 are chimeric clump weight, and clump weight uses lead material die cast, which mainly protects
Holding equipment balance and upset airflow function, the balanced weight on both sides is made by lead.
Working principle: the present invention is a kind of DCB Specimen high-rise life saving aircraft, and equipment is placed on platform first by when use
Or on roof, opens 17 user of safety belt and sit on safety seat 13, and fasten seat belts 17, and grasp handle 4, press
Control button on handle hand 4 rotates drive shaft 10, and when drive shaft 10 rotates, the first propeller hub 8 and the second propeller hub 11 are followed
Rotation, such first propeller 1 and the second propeller 3 start actively, the first spiral shell of promotion to be rotated after moving to a certain extent
Paddle 1 and the second propeller 3 are revolved, device is made to take off, when falling behind under device, impact force is transmitted to first on sleeve 21, makes sleeve 21
Declining, the air compression in such sleeve 21 carries out bradyseism, is simultaneously from the reaction force on ground, moves upwards feet 20,
But due to gravity factor, then column 19 is caused to decline the bradyseism again of compressed spring 22.
Finally, it should be noted that the foregoing is only a preferred embodiment of the present invention, it is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features,
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in of the invention
Within protection scope.
Claims (7)
1. a kind of DCB Specimen high-rise life saving aircraft, including equipment body (14), it is characterised in that: on the equipment body (14)
It offers cockpit (5), is mounted with safety seat (13) in the cockpit (5), the both ends side wall of the cockpit (5) is equipped with
Handle (4), the lower end two sides of the equipment body (14) are chimeric to be had headlight (6), the bottom end two sides weldering of the equipment body (14)
It is connected to bumper bracket (7), through having drive shaft (10), the end of the drive shaft (10) is socketed at the top of the equipment body (14)
Have wind deflector (12), be fixed with the first propeller hub (8) and the second propeller hub (11) on the drive shaft (10), and the first propeller hub (8) and
It is fixed with shaft set (9) in drive shaft (10) between second propeller hub (11), the both ends of first propeller hub (8) are equipped with the first spiral shell
It revolves paddle (1), the both ends of second propeller hub (11) are equipped with the second propeller (3), and the both ends of the shaft set (9) are equipped with balancing pole
(2)。
2. a kind of DCB Specimen high-rise life saving aircraft according to claim 1, it is characterised in that: the safety seat (13)
Be equipped with air bag (15) by back, and air bag (15) is designed to wave structure, and the safety seat (13) is equipped with safety belt
(17), and safety belt (17) one end is fixed on by back, and the other end is fixed on bottom end, the bottom end two of the safety seat (13)
Side is welded with baffle (18), and is placed with cushion (16) on safety seat (13) bottom end.
3. a kind of DCB Specimen high-rise life saving aircraft according to claim 1, it is characterised in that: the bumper bracket (7) by
Column (19), feet (20) and sleeve (21) composition, wherein the upper end of the column (19) is socketed in sleeve (21), and vertical
The lower end of column (19) is socketed in feet (20).
4. a kind of DCB Specimen high-rise life saving aircraft according to claim 3, it is characterised in that: the column (19) and pad
Spring (22) are equipped between foot (20), and spring (22) is fixed on the inner bottom of feet (20).
5. a kind of DCB Specimen high-rise life saving aircraft according to claim 1, it is characterised in that: handle (4) design
Control button is equipped at horizontal positioned L-type structure, and at the top of handle (4).
6. a kind of DCB Specimen high-rise life saving aircraft according to claim 1, it is characterised in that: first propeller hub (8)
It is divided into upper layer and lower layer with the second propeller hub (11), and the first propeller (1) and the second propeller (3) are clipped in the first propeller hub (8) respectively
And second propeller hub (11) upper layer and lower layer between, at the top center of first propeller hub (8) be equipped with hub cap.
7. a kind of DCB Specimen high-rise life saving aircraft according to claim 1, it is characterised in that: the balancing pole (2)
Both ends are chimeric clump weight, and clump weight uses lead material die cast.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910408424.4A CN110077584A (en) | 2019-05-16 | 2019-05-16 | A kind of DCB Specimen high-rise life saving aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910408424.4A CN110077584A (en) | 2019-05-16 | 2019-05-16 | A kind of DCB Specimen high-rise life saving aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110077584A true CN110077584A (en) | 2019-08-02 |
Family
ID=67420549
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910408424.4A Pending CN110077584A (en) | 2019-05-16 | 2019-05-16 | A kind of DCB Specimen high-rise life saving aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110077584A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11753146B1 (en) * | 2018-07-09 | 2023-09-12 | Pinto Geoffrey P | VTOL aircraft having modular payload |
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| CN204895857U (en) * | 2015-05-08 | 2015-12-23 | 沈阳闪宁科技有限公司 | Novel anti - oar single -person aircraft of portable coaxial |
| CN105730689A (en) * | 2016-04-14 | 2016-07-06 | 天津京东智联科技发展有限公司 | Double-rotor high-rise escape aircraft |
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| CN208149602U (en) * | 2018-04-18 | 2018-11-27 | 江西中轻智能设备有限公司 | A kind of self-adapting type plant protection drone |
| CN109250082A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of multiaxis low latitude manned vehicle |
| CN109250076A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of manned aircraft of intelligent escape |
| CN109250126A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of oil electric mixed dynamic manned vehicle |
-
2019
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Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200967565Y (en) * | 2006-11-10 | 2007-10-31 | 闫波 | Safe cabin |
| CN101773736A (en) * | 2009-12-31 | 2010-07-14 | 罗之洪 | Two-rotor model helicopter control system |
| CN104491993A (en) * | 2014-12-25 | 2015-04-08 | 刘在能 | High-altitude life-saving device |
| CN204895857U (en) * | 2015-05-08 | 2015-12-23 | 沈阳闪宁科技有限公司 | Novel anti - oar single -person aircraft of portable coaxial |
| CN105730689A (en) * | 2016-04-14 | 2016-07-06 | 天津京东智联科技发展有限公司 | Double-rotor high-rise escape aircraft |
| CN107499521A (en) * | 2017-08-23 | 2017-12-22 | 芜湖超源力工业设计有限公司 | A kind of pilot's safety guard |
| CN208149602U (en) * | 2018-04-18 | 2018-11-27 | 江西中轻智能设备有限公司 | A kind of self-adapting type plant protection drone |
| CN109250082A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of multiaxis low latitude manned vehicle |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US11753146B1 (en) * | 2018-07-09 | 2023-09-12 | Pinto Geoffrey P | VTOL aircraft having modular payload |
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Application publication date: 20190802 |
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