CN104890868B - One enters water self-opening manpower plateau aircraft - Google Patents
One enters water self-opening manpower plateau aircraft Download PDFInfo
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- CN104890868B CN104890868B CN201510282521.5A CN201510282521A CN104890868B CN 104890868 B CN104890868 B CN 104890868B CN 201510282521 A CN201510282521 A CN 201510282521A CN 104890868 B CN104890868 B CN 104890868B
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- frame
- skylight
- inserted link
- floating drum
- aircraft
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Abstract
The present invention is to provide one and enter water self-opening manpower plateau aircraft, belong to technical field of aerospace, including skeleton, skylight, float switch, control frame, push rod and foot piece, float switch is provided with multiple pulley, line is walked around multiple pulley and inserted link and floating drum is linked together, spring it is wound with on inserted link, time not by line pulling force, under spring force effect, left and right inserted link inserts in corresponding socket, thus stop skylight to be opened, after manpower plateau aircraft is overboard, left and right floating drum is floated along corresponding floating drum slide rail by buoyancy, drive line moves, now, left and right inserted link leaves socket along chute under the effect of line, thus skylight is opened naturally, operator is rescued rapidly.The present invention is to solve that existing plateau aircraft does not has escape device, rescue time is long, is susceptible to danger, and the problem that operator is easily snarled by bracing wire when escape.The present invention reduces the water discharging time of operator, there is the function of escape automatically.
Description
Technical field
The present invention relates to a kind of manpower plateau aircraft, particularly relate to one and enter water self-opening manpower plateau aircraft.
Background technology
Bird fleet-footed runner's contest, original name plateau human-powered flight's contest, it is also called " bird people " contest in the world, it is to integrate popular, one of fashion, fashionable air transport project, the aircraft that entrant needs designed, designed, make unpowered mechanism carries out independent gliding flight, has the highest sight and interest.Existing plateau man-power aircraft does not all have escape device, after operator is overboard, cannot surface in time breathing, operator can only be rescued by rescue personnel aircraft bottom of diving under water, rescue time is long, operation complexity, and when rescue, if overlong time, operator is not able to swim, it is easy to occur unexpected.It addition, have bracing wire between manpower plateau aircraft each several part, if rescuing improper, especially when operator is flurried, it is easy to be wound around, thus strengthen rescue difficulty.Comparing available man-power plateau aircraft, the present invention uses into water self-opening escape device, is automatically opened up by skylight after entering water and realizes escape, it is achieved that the automatization of escape device, and beneficially the motion of manpower plateau aircraft is universal.
Summary of the invention
The invention aims to solve existing plateau aircraft and do not have escape device, rescue time is long, is susceptible to danger, and operator is easily snarled by bracing wire when escape problem and provide one to enter water self-opening manpower plateau aircraft.
nullThe object of the present invention is achieved like this: includes aircraft body，Aircraft body is provided with skeleton，Mid portion at skeleton is provided with skylight frame，Two ends, left and right on skylight frame have been respectively articulated with left sash of skylight and right sash of skylight，The afterbody of skylight frame is fixed with foot piece，The upper end of foot piece is fixed with push rod，The lower end of foot piece is fixed with control frame，Described foot piece is installed with left runner frame and right rail frame with the junction also symmetry in skylight, left and right，Left chute frame and right rail frame are installed on left runner frame and right rail frame，Left chute frame and right rail frame are separately installed with left inserted link and right inserted link，And the two ends of left inserted link and right inserted link all extend out to outside the chute frame of correspondence，Each inserted link is positioned at winding spring in the part of corresponding chute frame，End corner at left sash of skylight and right sash of skylight is separately installed with left socket and right socket，One end of left inserted link and one end of right inserted link are respectively protruding into left socket and right socket，Left floating drum slide rail and right floating drum slide rail it is symmetrically arranged with on described control frame，It is separately installed with left floating drum and right floating drum in left floating drum slide rail and right floating drum slide rail，The end of left floating drum is fixed with line，Line walks around the lower sheave being arranged on control frame successively、It is arranged on the middle pulley done on floating drum slide rail、The top sheave being arranged on control frame、The first pulley of being arranged on left runner frame and be arranged on that the second pulley done on runner frame is vertical with left inserted link to be connected，The set-up mode of the line that the end of right floating drum is connected is identical with the set-up mode of the line that the end of left floating drum is connected.
Present invention additionally comprises so some architectural features:
1. the cross sectional shape of left inserted link and right inserted link described in is circular, and corresponding left socket and the shape of cross section of right socket are also round shape.
2. the plane at control frame place described in is vertical with the plane at skylight frame place.
Compared with prior art, the invention has the beneficial effects as follows: the present invention escapes by using the skylight that can automatically open up, it is achieved that the automatization of escape device, decreases the water discharging time of operator, improve the safety and reliability of manpower plateau aircraft, it is easy to rescue personnel's rescue, it is to avoid operator is by guy winding, and after manpower plateau aircraft is overboard, skylight can automatically open up, thus beneficially operator directly surfaces, it is rescued rapidly, beneficially the popularization of plateau sporting flying.Present configuration is simple and can efficiently reduce the water discharging time of operator, has the function of escape automatically.
Accompanying drawing explanation
Overall structure schematic diagram when Fig. 1 is the left sash of skylight of the present invention and right sash of skylight is in closure state；
Fig. 2 is the overall structure schematic diagram that the left sash of skylight of the present invention and right sash of skylight are in open mode；
Fig. 3 is the left sash of skylight of the present invention and the structural representation of chute frame part time right sash of skylight is in closure state；
Fig. 4 is the left sash of skylight of the present invention and the structural representation of buoy section time right sash of skylight is in closure state；
Fig. 5 is the left sash of skylight of the present invention and the structural representation of chute frame part time right sash of skylight is in open mode；
Fig. 6 is the left sash of skylight of invention and the structural representation of buoy section time right sash of skylight is in open mode.
Detailed description of the invention
With detailed description of the invention, the present invention is described in further detail below in conjunction with the accompanying drawings.
In conjunction with Fig. 1 to Fig. 6, the invention belongs to technical field of aerospace, do not have escape device to solve existing plateau aircraft, rescue time is long, is susceptible to danger, and the problem that operator is easily snarled by bracing wire when escape.nullThe present invention includes aircraft body，Aircraft body is provided with skeleton 1，Mid portion at skeleton 1 is provided with skylight frame 16，Two ends, left and right on skylight frame 16 have been respectively articulated with left sash of skylight and right sash of skylight，Left sash of skylight and right sash of skylight constitute skylight 2，Skylight,The afterbody of 16 is fixed with foot piece 6，The upper end of foot piece 6 is fixed with push rod 3，The lower end of foot piece 6 is fixed with control frame 5，Described foot piece 6 is installed with left runner frame 15-1 and right rail frame 15-2 with the junction also symmetry in skylight, left and right，Left chute frame 11-1 and right rail frame 11-2 are installed on left runner frame 15-1 and right rail frame 15-2，Left chute frame 11-1 and right rail frame 11-2 are separately installed with left inserted link 9-1 and right inserted link 9-2，And the two ends of left inserted link 9-1 and right inserted link 9-2 all extend out to outside the chute frame of correspondence，Each inserted link is positioned at winding spring 8 in the part of corresponding chute frame，End corner at left sash of skylight and right sash of skylight is separately installed with left socket 7-1 and right socket 7-2，One end of left inserted link 9-1 and one end of right inserted link 9-2 are respectively protruding into left socket 7-1 and right socket 7-2，(structure is identical with left floating drum slide rail with right floating drum slide rail to be symmetrically arranged with left floating drum slide rail 13-1 on described control frame 5，In figure unmarked)，(structure is identical with left floating drum with right floating drum with being separately installed with left floating drum 14-1 in right floating drum slide rail for left floating drum slide rail 13-1，In figure unmarked)，The end of left floating drum 14-1 is fixed with line 12，Line 12 walks around the lower sheave 10-1 being arranged on control frame successively、It is arranged on the middle pulley 10-2 done on floating drum slide rail、The top sheave 10-3 being arranged on control frame、The first pulley 10-4 of being arranged on left runner frame 15-1 and be arranged on that the second pulley 10-5 done on runner frame is vertical with left inserted link 9-1 to be connected，The set-up mode of the line that the end of right floating drum is connected is identical with the set-up mode of the line that the end of left floating drum 14-1 is connected.
Preferably, the cross sectional shape of described left inserted link 9-1 and right inserted link 9-2 is circular, and corresponding left socket 7-1 and the shape of cross section of right socket 7-2 are also round shape.
The plane at described control frame 5 place is vertical with the plane at skylight frame 16 place, namely the mounting plane of described control frame 5 is vertical with skylight frame 16 place plane.
Specifically: a kind of manpower plateau aircraft using the skylight escape that can automatically open up that the present invention provides, including skeleton 1, skylight 2, float switch, control frame 5, push rod 3 and foot piece 6, between described skeleton 1, each bar uses fixing connection, push rod 3 bottom and foot piece 6 front end meet on skylight 2 same point and are fixed on skylight 2, and control frame 5 top is fixing with skylight 2 to be connected.nullDescribed float switch 4 is by five pulley 10-1 to 10-5、Left chute frame 11-1 and right rail frame 11-2、Left runner frame 15-1 and right rail frame 15-2、Spring 8、Left inserted link 9-1 and right inserted link 9-2、Left socket 7-1 and right socket 7-2、(structure is identical with left floating drum slide rail with right floating drum slide rail for left floating drum slide rail 13-1，In figure unmarked)、(structure is identical with left floating drum with right floating drum for left floating drum 14-1，In figure unmarked) and line 12 form，Line 12 is walked around five pulleys and corresponding inserted link and corresponding floating drum is linked together，Spring 8 it is wound with respectively on left inserted link 9-1 and right inserted link 9-2，Time not by line pulling force，Under spring 8 elastic force effect，Each inserted link is along corresponding runner movement，Insert in corresponding socket，Thus stop skylight 2 to be opened，Left socket 7-1 and right socket 7-2 is fixed on skylight 2 (left sash of skylight and right sash of skylight)，Two, left and right chute is fixed on two runner frames in left and right，Guarantee two, left and right chute frame and skeleton 1 geo-stationary，Chute 11 place plane is parallel with socket 7 place plane，Left runner frame 15-1 and right rail frame 15-2 and push rod 3、Foot piece 6 is fixing to be connected，Described floating drum slide rail 13 is fixed on control frame 5 and floating drum slide rail 13 bottom circular aperture size reduces，Guarantee that each floating drum can only move in corresponding floating drum slide rail，Without departing from floating drum slide rail，The bottom of two floating drums is connected with line 12 respectively.After manpower plateau aircraft is overboard, left and right floating drum is floated along corresponding floating drum slide rail by buoyancy, line 12 is driven to move, thus create pulling force, offset with the elastic force of partial spring 8, now, left and right inserted link leaves corresponding socket along corresponding chute under the effect of line, therefore left and right socket loses the constraint of left and right inserted link respectively, thus skylight 2 under self spring force effect around axial upper deflecting, opening rapidly, namely skylight 2 can be opened under elastic force effect naturally, operator is rescued rapidly.
Claims (3)
1. enter a water self-opening manpower plateau aircraft, including aircraft body, it is characterised in that: pacify on aircraft body
Equipped with skeleton, the mid portion at skeleton is provided with skylight frame, and the two ends, left and right on skylight frame have been respectively articulated with left sash of skylight and the right side
Sash of skylight, the afterbody of skylight frame is fixed with foot piece, and the upper end of foot piece is fixed with push rod, and the lower end of foot piece is fixed with control frame, institute
The junction also symmetry stating foot piece and skylight, left and right is installed with on left runner frame and right rail frame, left runner frame and right rail frame
It is provided with in left chute frame and right rail frame, left chute frame and right rail frame and is separately installed with left inserted link and right inserted link, and left inserted link
Outside with the chute frame that the two ends of right inserted link all extend out to correspondence, each inserted link is positioned at winding spring in the part of corresponding chute frame,
End corner at left sash of skylight and right sash of skylight is separately installed with left socket and right socket, one end of left inserted link and right inserted link
One end is respectively protruding into left socket and right socket, and described control frame is symmetrically arranged with left floating drum slide rail and right floating drum slide rail, left
Being separately installed with left floating drum and right floating drum in floating drum slide rail and right floating drum slide rail, the end of left floating drum is fixed with line, and line is successively
The middle pulley walk around the lower sheave being arranged on control frame, being arranged on left floating drum slide rail, the top sheave being arranged on control frame,
The first pulley being arranged on left runner frame and the second pulley being arranged on left runner frame is vertical with left inserted link is connected, right floating drum
The set-up mode of the connected line in end set-up mode and the end of left floating drum of line that are connected identical.
One the most according to claim 1 enters water self-opening manpower plateau aircraft, it is characterised in that: described left inserted link and
The cross sectional shape of right inserted link is circular, and corresponding left socket and the shape of cross section of right socket are also round shape.
One the most according to claim 1 and 2 enters water self-opening manpower plateau aircraft, it is characterised in that: described manipulation
The plane at frame place is vertical with the plane at skylight frame place.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282521.5A CN104890868B (en) | 2015-05-28 | 2015-05-28 | One enters water self-opening manpower plateau aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510282521.5A CN104890868B (en) | 2015-05-28 | 2015-05-28 | One enters water self-opening manpower plateau aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104890868A CN104890868A (en) | 2015-09-09 |
| CN104890868B true CN104890868B (en) | 2016-09-14 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510282521.5A Expired - Fee Related CN104890868B (en) | 2015-05-28 | 2015-05-28 | One enters water self-opening manpower plateau aircraft |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1710446A1 (en) * | 1990-02-27 | 1992-02-07 | Обнинское научно-производственное объединение "Технология" | Delta-glider |
| CN1086779A (en) * | 1992-11-07 | 1994-05-18 | 冯建光 | Bionic man power aircraft |
| DE19604464A1 (en) * | 1996-02-08 | 1997-08-14 | Bautek Fluggeraete Gmbh | Support construction for hang glider or other airborne craft |
| CN2490052Y (en) * | 2001-06-13 | 2002-05-08 | 上海皮恩斯电讯电子有限公司 | Framework of parasol |
| CN103847963A (en) * | 2014-02-28 | 2014-06-11 | 华南农业大学 | Unmanned power delta wing aircraft |
| CN204056298U (en) * | 2014-07-08 | 2014-12-31 | 重庆市双桥区巴工机械加工厂 | Low latitude assistant sliding delta wing device |
| CN204822079U (en) * | 2015-05-28 | 2015-12-02 | 哈尔滨工程大学 | Entry from open manpower high platform aircraft |
-
2015
- 2015-05-28 CN CN201510282521.5A patent/CN104890868B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU1710446A1 (en) * | 1990-02-27 | 1992-02-07 | Обнинское научно-производственное объединение "Технология" | Delta-glider |
| CN1086779A (en) * | 1992-11-07 | 1994-05-18 | 冯建光 | Bionic man power aircraft |
| DE19604464A1 (en) * | 1996-02-08 | 1997-08-14 | Bautek Fluggeraete Gmbh | Support construction for hang glider or other airborne craft |
| CN2490052Y (en) * | 2001-06-13 | 2002-05-08 | 上海皮恩斯电讯电子有限公司 | Framework of parasol |
| CN103847963A (en) * | 2014-02-28 | 2014-06-11 | 华南农业大学 | Unmanned power delta wing aircraft |
| CN204056298U (en) * | 2014-07-08 | 2014-12-31 | 重庆市双桥区巴工机械加工厂 | Low latitude assistant sliding delta wing device |
| CN204822079U (en) * | 2015-05-28 | 2015-12-02 | 哈尔滨工程大学 | Entry from open manpower high platform aircraft |
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| Publication number | Publication date |
|---|---|
| CN104890868A (en) | 2015-09-09 |
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| C14 | Grant of patent or utility model | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160914 |