CN204822079U - Entry from open manpower high platform aircraft - Google Patents
Entry from open manpower high platform aircraft Download PDFInfo
- Publication number
- CN204822079U CN204822079U CN201520355963.3U CN201520355963U CN204822079U CN 204822079 U CN204822079 U CN 204822079U CN 201520355963 U CN201520355963 U CN 201520355963U CN 204822079 U CN204822079 U CN 204822079U
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- CN
- China
- Prior art keywords
- frame
- skylight
- floating drum
- inserted link
- socket
- 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.)
- Withdrawn - After Issue
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Abstract
The utility model provides an entry from open manpower high platform aircraft belongs to aviation technical field, the testing tool comprises a skeleto, the skylight, the float switch, control the frame, ejector pin and foot piece, flotation pontoon switching system has a plurality of pulleys, the line is walked around a plurality of pulleys and is linked together inserted bar and flotation pontoon, around there being the spring on the inserted bar, when not receiving the line pulling force, under the spring force effect, it inserts in the corresponding socket to control the inserted bar, thereby open in the prevention skylight, after manpower high platform aircraft falls into water, it receives buoyancy along the flotation pontoon slide rail come -up that corresponds to control the flotation pontoon, the motion of drive line, then, control the inserted bar and leave the socket along the spout under the effect of line, thereby open naturally in the skylight, operator is rescued rapidly. The utility model discloses a solve present high platform aircraft and does not have escape device, rescue chronicly, cause danger problem that just operator was acted as go -between easily and snarls when fleing for one's life easily. The utility model discloses reduce operator's the play water time, had automatic function of fleing.
Description
Technical field
The utility model relates to a kind of manpower plateau aircraft, particularly relates to one and enters water self-opening manpower plateau aircraft.
Background technology
Bird fleet-footed runner contest, original name plateau human-powered flight contest, be also called " bird people " contest in the world, that afflux is capable, one of fashion, fashionable air transport project in one, entrant needs designed, designed, make the aircraft of unpowered mechanism carries out independent gliding flight, has very high sight and interest.Existing plateau man-power aircraft does not all have escape device, after operator is overboard, cannot to surface in time breathing, operator can only be rescued by rescue group aircraft bottom of diving under water, rescue time is long, complicated operation, and when rescuing, if overlong time, operator is not able to swim again, is easy to meet accident.In addition, between manpower plateau aircraft each several part, there is bracing wire, if rescue improper, especially when operator is flurried, be easy to be wound around, thus strengthen rescue difficulty.Compare available man-power plateau aircraft, the utility model adopts into water self-opening escape device, is automatically opened and realizes escape, achieve the automation of escape device by skylight after entering water, is conducive to the universal of manpower plateau aircraft movements.
Summary of the invention
The purpose of this utility model does not have escape device to solve existing plateau aircraft, and rescue time is long, easily causes danger, and the problem that operator is easily snarled by bracing wire when escaping and provide one to enter water self-opening manpower plateau aircraft.
The purpose of this utility model is achieved in that and comprises aircraft body, aircraft body is provided with skeleton, at the centre portion of skeleton, skylight frame is installed, two ends, left and right on skylight frame are hinged with left sash of skylight and right sash of skylight respectively, 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, the junction in described foot piece and skylight, left and right also symmetry is installed with left runner frame and right rail frame, left runner frame and right rail frame are provided with left chute frame and right rail frame, left inserted link and right inserted link is separately installed with in left chute frame and right rail frame, and the two ends of left inserted link and right inserted link all extend out to outside corresponding chute frame, winding spring in the part that each inserted link is positioned at corresponding chute frame, left socket and right socket is separately installed with in the end corner of left sash of skylight and right sash of skylight, one end of left inserted link and one end of right inserted link stretch in left socket and right socket respectively, described control frame is symmetrically arranged with left floating drum slide rail and right floating drum slide rail, left floating drum and right floating drum is separately installed with 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 be arranged on control frame successively, be arranged on the middle pulley on left floating drum slide rail, be arranged on the top sheave on control frame, be arranged on the first pulley on left runner frame and the second pulley be arranged on left runner frame is connected with left inserted link is vertical, 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.
The utility model also comprises some architectural features like this:
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 circular.
2. the plane at control frame place described in and the plane orthogonal at skylight frame place.
Compared with prior art, the beneficial effects of the utility model are: the utility model is by adopting the skylight escape that can automatically open, achieve the automation of escape device, decrease the water discharging time of operator, improve the safety and reliability of manpower plateau aircraft, be convenient to rescue group's rescue, avoid operator by guy winding, and after manpower plateau aircraft is overboard, skylight can be opened automatically, thus be conducive to operator and directly surface, be rescued rapidly, be conducive to the popularization of plateau sporting flying.The utility model structure is simple and effectively can reduce the water discharging time of operator, has the function of escape automatically.
Accompanying drawing explanation
Fig. 1 is left sash of skylight of the present utility model and right sash of skylight integral structure schematic diagram when being in closure state;
Fig. 2 is the integral structure schematic diagram that left sash of skylight of the present utility model and right sash of skylight are in open mode;
Fig. 3 is the structural representation of left sash of skylight of the present utility model and right sash of skylight chute frame part when being in closure state;
Fig. 4 is the structural representation of left sash of skylight of the present utility model and right sash of skylight buoy section when being in closure state;
Fig. 5 is the structural representation of left sash of skylight of the present utility model and right sash of skylight chute frame part when being in open mode;
Fig. 6 is the structural representation of the utility model left sash of skylight of the present utility model and right sash of skylight buoy section when being in open mode.
Detailed description of the invention
Below in conjunction with accompanying drawing and detailed description of the invention, the utility model is described in further detail.
Composition graphs 1 to Fig. 6, the utility model belongs to technical field of aerospace, and do not have escape device to solve existing plateau aircraft, rescue time is long, easily causes danger, and when escaping operator easily by problem that bracing wire snarls.The utility model comprises aircraft body, aircraft body is provided with skeleton 1, at the centre portion of skeleton 1, skylight frame 16 is installed, two ends, left and right on skylight frame 16 are hinged with left sash of skylight and right sash of skylight respectively, left sash of skylight and right sash of skylight form 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, the junction in described foot piece 6 and skylight, left and right also symmetry is installed with left runner frame 15-1 and right rail frame 15-2, left runner frame 15-1 and right rail frame 15-2 is provided with left chute frame 11-1 and right rail frame 11-2, left inserted link 9-1 and right inserted link 9-2 is separately installed with in left chute frame 11-1 and right rail frame 11-2, and the two ends of left inserted link 9-1 and right inserted link 9-2 all extend out to outside corresponding chute frame, winding spring 8 in the part that each inserted link is positioned at corresponding chute frame, left socket 7-1 and right socket 7-2 is separately installed with in the end corner of left sash of skylight and right sash of skylight, one end of left inserted link 9-1 and one end of right inserted link 9-2 stretch in left socket 7-1 and right socket 7-2 respectively, (structure is identical with left floating drum slide rail with right floating drum slide rail described control frame 5 to be symmetrically arranged with left floating drum slide rail 13-1, unmarked in figure), (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, unmarked in figure), the end of left floating drum 14-1 is fixed with line 12, line 12 walks around the lower sheave 10-1 be arranged on control frame successively, be arranged on the middle pulley 10-2 on left floating drum slide rail, be arranged on the top sheave 10-3 on control frame, be arranged on the first pulley 10-4 on left runner frame 15-1 and the second pulley 10-5 be arranged on left runner frame is connected with left inserted link 9-1 is vertical, 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 circular.
The plane at described control frame 5 place and the plane orthogonal at skylight frame 16 place are also mounting plane and the skylight frame 16 place plane orthogonal of described control frame 5.
Specifically: the manpower plateau aircraft of the skylight escape that a kind of employing that the utility model provides can be opened automatically, comprise skeleton 1, skylight 2, float switch, control frame 5, push rod 3 and foot piece 6, between described skeleton 1, each bar adopts and is fixedly connected with, push rod 3 bottom and foot piece 6 front end meet at same point on skylight 2 and are fixed on skylight 2, and control frame 5 top is fixedly connected with skylight 2.Described 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 for left floating drum slide rail 13-1 and right floating drum slide rail, unmarked in figure), (structure is identical with left floating drum for left floating drum 14-1 and right floating drum, unmarked in figure) and line 12 form, line 12 is walked around five pulleys and the inserted link of correspondence and corresponding floating drum is linked together, left inserted link 9-1 and right inserted link 9-2 is wound with spring 8 respectively, time not by line pulling force, under the effect of spring 8 elastic force, 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 chute frame in left and right and skeleton 1 geo-stationary, chute 11 place plane and socket 7 place plane parallel, left runner frame 15-1 and right rail frame 15-2 and push rod 3, foot piece 6 is fixedly connected with, 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 the floating drum slide rail of correspondence, and floating drum slide rail can not be departed from, the bottom of two floating drums is connected with line 12 respectively.After manpower plateau aircraft is overboard, left and right floating drum is subject to buoyancy and floats along corresponding floating drum slide rail, 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 axially deflecting, open rapidly, also namely skylight 2 naturally can be opened under elastic force effect, and operator is rescued rapidly.
Claims (3)
1. one kind enters water self-opening manpower plateau aircraft, comprise aircraft body, it is characterized in that: on aircraft body, skeleton is installed, at the centre portion of skeleton, skylight frame is installed, two ends, left and right on skylight frame are hinged with left sash of skylight and right sash of skylight respectively, 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, the junction in described foot piece and skylight, left and right also symmetry is installed with left runner frame and right rail frame, left runner frame and right rail frame are provided with left chute frame and right rail frame, left inserted link and right inserted link is separately installed with in left chute frame and right rail frame, and the two ends of left inserted link and right inserted link all extend out to outside corresponding chute frame, winding spring in the part that each inserted link is positioned at corresponding chute frame, left socket and right socket is separately installed with in the end corner of left sash of skylight and right sash of skylight, one end of left inserted link and one end of right inserted link stretch in left socket and right socket respectively, described control frame is symmetrically arranged with left floating drum slide rail and right floating drum slide rail, left floating drum and right floating drum is separately installed with 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 be arranged on control frame successively, be arranged on the middle pulley on left floating drum slide rail, be arranged on the top sheave on control frame, be arranged on the first pulley on left runner frame and the second pulley be arranged on left runner frame is connected with left inserted link is vertical, 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.
2. one according to claim 1 enters water self-opening manpower plateau aircraft, it is characterized in that: the cross sectional shape of described left inserted link and right inserted link is circular, and corresponding left socket and the shape of cross section of right socket are also circular.
3. one according to claim 1 and 2 enters water self-opening manpower plateau aircraft, it is characterized in that: the plane at described control frame place and the plane orthogonal at skylight frame place.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520355963.3U CN204822079U (en) | 2015-05-28 | 2015-05-28 | Entry from open manpower high platform aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520355963.3U CN204822079U (en) | 2015-05-28 | 2015-05-28 | Entry from open manpower high platform aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204822079U true CN204822079U (en) | 2015-12-02 |
Family
ID=54679705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520355963.3U Withdrawn - After Issue CN204822079U (en) | 2015-05-28 | 2015-05-28 | Entry from open manpower high platform aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204822079U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890868B (en) * | 2015-05-28 | 2016-09-14 | 哈尔滨工程大学 | One enters water self-opening manpower plateau aircraft |
-
2015
- 2015-05-28 CN CN201520355963.3U patent/CN204822079U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890868B (en) * | 2015-05-28 | 2016-09-14 | 哈尔滨工程大学 | One enters water self-opening manpower plateau aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20151202 Effective date of abandoning: 20160914 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |