CN204726669U - A kind of automatic cover-turning hydroplane delta wing - Google Patents
A kind of automatic cover-turning hydroplane delta wing Download PDFInfo
- Publication number
- CN204726669U CN204726669U CN201520356152.5U CN201520356152U CN204726669U CN 204726669 U CN204726669 U CN 204726669U CN 201520356152 U CN201520356152 U CN 201520356152U CN 204726669 U CN204726669 U CN 204726669U
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- reinforcing frame
- wing plate
- wing
- skeleton
- crossbeam
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Abstract
The utility model provides a kind of automatic cover-turning hydroplane delta wing, belongs to low-latitude flying equipment technical field.Delta wing of the present utility model to be spliced mutually with right wing plate and crossbeam by left wing plate and centered by left wing plate and right wing plate phase stitching portion axle, the another side of wing plate is connected mutually with skeleton, nose of wing floating drum and skeleton are connected and with the extended line of crossbeam for axis of symmetry tilts to both sides, outer reinforcing frame had not only been connected with left wing plate and right wing plate but also had been connected with skeleton, outer reinforcing frame is connected by torsion spring with interior reinforcing frame, in two pieces, left and right in reinforcing frame the right interior reinforcing frame in be fixed with steel ring, rope is connected with reinforcing frame in the left side through steel ring, Compound Fabric to be attached to fixed in two pieces, left and right on reinforcing frame as covering, uprights vertical is fixed on crossbeam top, spider is vertically fixed on the bottom of crossbeam.The utility model can realize delta wing and slip into the Vee formation wing in water and can swim on the water surface and the top of delta wing and automatically open, and facilitates aviator to escape from water.
Description
Technical field
The utility model relates to a kind of delta wing waterborne, particularly relates to a kind of automatic cover-turning hydroplane delta wing.
Background technology
In ultimate challenge motion, delta wing is one of most popular project, its dynamic and unpowered dividing, unpowered delta wing needs aviator to be suspended on delta wing by oneself in plateau, through the run-up of a segment distance, aviator takes in the air by the lift of delta wing, a kind of challenge extreme sport at a distance of then aloft gliding, for the sake of security, general delta wing is all glide in water.But this motion, with certain danger, not only needs aviator to have good fitness and psychological quality, also need aviator in glide to there being skill of escaping flexibly during ground; Often danger close is exactly that existing delta wing structure is simple, primarily of close wing plate composition and delta wing is bulky, under in landing water, the Vee formation wing can cover delta wing aviator, this is just for aviator brings very large danger, and also for rescue brings difficulty, so this is a difficult problem urgently to be resolved hurrily.
Summary of the invention
The purpose of this utility model be in order to solve delta wing enter water after aviator be difficult to depart from delta wing problem and a kind of automatic cover-turning hydroplane delta wing is provided.
The purpose of this utility model is achieved in that and comprises skeleton, symmetry is arranged on left wing plate on skeleton and right wing plate, for connecting the crossbeam of left wing plate and right wing plate and being symmetricly set on the nose of wing floating drum of left wing plate and right wing plate head, it is characterized in that: on described left wing plate and right wing plate, be respectively arranged with outer reinforcing frame, and described outer reinforcing frame and skeleton are connected, each outer reinforcing frame inside is provided with corresponding interior reinforcing frame, and be connected with torsion spring between each outer reinforcing frame with each interior reinforcing frame, interior reinforcing frame is attached with Compound Fabric, and the king-rod place of an interior reinforcing frame is provided with steel ring, rope through steel ring and one end of rope and in another reinforcing frame be connected, the other end of rope is pulled by aviator, the below of described crossbeam is fixed with spider, steel rope is provided with between the bottom of spider and skeleton, the top of described crossbeam is provided with column, the top of column is connected with steel rope respectively with the two ends of skeleton.
The utility model also comprises some architectural features like this:
1. be connected with two torsion springs between each outer reinforcing frame with each interior reinforcing frame.
2. column described in and spider are above and below the same position of crossbeam.
Compared with prior art, the beneficial effects of the utility model are: the utility model can swim on the water surface after overboard, and in water, automatically can open top cover, aviator can be swum out of by top cover, be unlikely to be covered under water by huge delta wing, reduce the danger of aviator and conveniently rescue, the safety of the hydroplane delta wing of also i.e. the utility model raising.
Accompanying drawing explanation
Fig. 1 is structural representation one of the present utility model;
Fig. 2 is structural representation two of the present utility model;
Fig. 3 is the connection diagram between spider of the present utility model and skeleton;
Fig. 4 is the connection diagram between column of the present utility model and skeleton.
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.
The utility model relates to aircraft field, and mainly refer to low-latitude flying apparatus field, particularly relating to a kind of device sliding delta wing, is more particularly a kind of delta wing automatically opening top cover, make aviator convenient from water device out.
Composition graphs 1 and Fig. 2, comprise skeleton 2, symmetry is arranged on left wing plate 14 on skeleton 2 and right wing plate 13, for connecting the crossbeam 6 of left wing plate 14 and right wing plate 13 and being symmetricly set on the nose of wing floating drum 1 of left wing plate 14 and right wing plate 13 head, described left wing plate 14 and right wing plate 13 are respectively arranged with outer reinforcing frame 3, and described outer reinforcing frame 3 is connected with skeleton 2, each outer reinforcing frame 3 inside is provided with corresponding interior reinforcing frame 4, and be connected with torsion spring 10 between each outer reinforcing frame 3 with each interior reinforcing frame 4, interior reinforcing frame 3 is attached with Compound Fabric 8, and king-rod 16 place of an interior reinforcing frame 3 is provided with steel ring 9, rope 11 through steel ring 9 and rope 11 one end and in another reinforcing frame 3 be connected, the rope other end is pulled by aviator, the below of described crossbeam 6 is fixed with spider 7, steel rope 15 is provided with between the bottom of spider 7 and skeleton 2, the top of described crossbeam 6 is provided with column 5, the top of column 5 is connected with steel rope 15 respectively with the two ends of skeleton 2.Be connected with two torsion springs 10 between each outer reinforcing frame 3 with each interior reinforcing frame 4.Described column 5 and spider 7 are above and below the same position of crossbeam 6.
Also namely the utility model comprises nose of wing floating drum 1, skeleton 2, outer reinforcing frame 3, interior reinforcing frame 4, column 5, crossbeam 6, spider 7, Compound Fabric 8, steel ring 9, torsion spring 10, rope 11, left wing plate 14, right wing plate 13 and steel wire 15.Delta wing be to be spliced mutually with right wing plate 13 and crossbeam 6 by left wing plate 14 and centered by crossbeam 6 axle (left wing plate 14 and right wing plate 13 are that axis of symmetry tilts to both sides with center shaft), the other end of left wing plate 14 and right wing plate 13 adopts with skeleton 2 and is fixedly connected with, nose of wing floating drum 1 is fixedly connected with skeleton 2 and with the extended line of crossbeam 6 for axis of symmetry tilts to both sides (angle of inclination is identical with the angle of inclination of right wing plate 13 with left wing plate 14) and left and right leading edge floating drum is the top of delta wing at the intersection of axis of symmetry, the outside of outer reinforcing frame 3 and left wing plate 14 and right wing plate 13 are fixedly connected, two ends inside outer reinforcing frame 3 and skeleton 2 are fixedly connected, the side other end that one end of torsion spring 10 is fixed on outer reinforcing frame 3 is fixed on interior reinforcing frame 4, when interior reinforcing frame 4 is in open mode, torsion spring 10 in the raw, when interior reinforcing frame 4 is in closure state, torsion spring 10 is in torsional deflection state, now torsion spring 10 has the effect of the power that interior reinforcing frame is opened to interior reinforcing frame 4, steel ring 9 to be fixed in the right reinforcing frame 4 from the nearest bar place of axis of symmetry, the intersection of interior reinforcing frame king-rod is fixed on by steel ring 9, the Main Function of steel ring 9 is change power direction of transfer in rope, rope 11 one end is connected from the bar that axis of symmetry is nearest with reinforcing frame in the left side through steel ring 9, the other end is awing hand-pulled by aviator, the length of the bar be connected with steel ring in reinforcing frame in the bar be connected with rope in reinforcing frame in the left side and the right thereof is longer than the length adding outer strong frame 3 so that reinforcing frame can cover on reinforcing frame 3 in left and right, prevent interior reinforcing frame through outer reinforcing frame.Compound Fabric 8 is attached to fixed in two pieces, left and right on reinforcing frame as covering, and column 5 is vertically fixed on crossbeam 6 top, and spider 7 is vertically fixed on the bottom of crossbeam 6.。
Composition graphs 3 and Fig. 4, column 5 is vertically fixed on the top in the middle part of crossbeam 6, the top steel wire 15 of column 5 object that is connected with the bottom of skeleton 2 keeps the aerofoil profile of delta wing and the top of the top steel wire 15 of column 4 and crossbeam and bottom thereof are connected respectively, object keeps the stability of column 4, and spider 7 is vertically fixed on bottom in the middle part of crossbeam 6 and the two bottom sides of spider 7 is the stability ensureing spider by steel wire 15 object that to be connected with the bottom of skeleton 2 respectively.
When high airflight, aviator's hand is caught spider 7 and is fully covered on outer reinforcing frame 3 through the interior reinforcing frame 4 that the rope 11 of steel ring 9 also firmly makes the attachment of two pieces, left and right be fixed wtih Compound Fabric 8, on the interior reinforcing frame be connected with steel ring 9 on the right of the interior reinforcing frame that is connected with rope 11 for the left side of covering order of interior reinforcing frame 4 is pressed in, the torsion spring 10 be now connected on outer reinforcing frame 3 is in torsional deflection state, torsion spring 10 has the effect of the power that interior reinforcing frame is opened to interior reinforcing frame 4, state of flight is now substantially identical with common delta wing state of flight; Until delta wing from after slipping in the air and entering water, under the effect of nose of wing floating drum 1, delta wing can swim on the water surface, reaction aviator by instinct can decontrol the rope 11 in hand automatically, now interior reinforcing frame 4 under the effect of torsion spring 10 power automatic turning to both sides, top cover opens, aviator swims out of from the top cover opened, or is rescued by rescue group.The utility model can realize delta wing and slip into the Vee formation wing in water and can swim on the water surface and the top of delta wing and automatically open, and facilitates aviator to escape from water.
Specific works process of the present utility model is: first, when high airflight, aviator's hand is caught spider and is fully covered on outer reinforcing frame through the interior reinforcing frame that the rope of steel ring also firmly makes the attachment of two pieces, left and right be fixed wtih Compound Fabric, on the interior reinforcing frame be connected with steel ring on the right of the interior reinforcing frame that is connected with rope for the left side of covering order of interior reinforcing frame is pressed in, the torsion spring be now connected on outer reinforcing frame is in torsional deflection state, the internal reinforcing frame of spring has the effect of the power that interior reinforcing frame is opened, state of flight is now substantially identical with common delta wing state of flight, until delta wing from after slipping in the air and entering water, under the effect of nose of wing floating drum, delta wing can swim on the water surface, aviator can decontrol the rope in hand automatically by instinct, now interior reinforcing frame under the effect of torsion spring force automatic turning to both sides, top cover opens, aviator swims out of from the top cover opened, or is rescued by rescue group.
Saying specifically, outer reinforcing frame 3 described in the utility model limit each two every with the torsion spring about 10 be connected between interior reinforcing frame 4.Described tripod 7 is fixed on the bottom of column 5.
During described delta wing flight, interior reinforcing frame 4 covers on outer reinforcing frame 3 completely, the bar that in the left side, reinforcing frame is connected with rope is pressed on the steel ring of reinforcing frame in the right, and the length of the bar be connected with steel ring in reinforcing frame in the bar be connected with rope in reinforcing frame in the left side and the right thereof is longer than the length of reinforcing frame 3.
Claims (3)
1. an automatic cover-turning hydroplane delta wing, comprise skeleton, symmetry is arranged on left wing plate on skeleton and right wing plate, for connecting the crossbeam of left wing plate and right wing plate and being symmetricly set on the nose of wing floating drum of left wing plate and right wing plate head, it is characterized in that: on described left wing plate and right wing plate, be respectively arranged with outer reinforcing frame, and described outer reinforcing frame and skeleton are connected, each outer reinforcing frame inside is provided with corresponding interior reinforcing frame, and be connected with torsion spring between each outer reinforcing frame with each interior reinforcing frame, interior reinforcing frame is attached with Compound Fabric, and the king-rod place of an interior reinforcing frame is provided with steel ring, rope through steel ring and one end of rope and in another reinforcing frame be connected, the other end of rope is pulled by aviator, the below of described crossbeam is fixed with spider, steel rope is provided with between the bottom of spider and skeleton, the top of described crossbeam is provided with column, the top of column is connected with steel rope respectively with the two ends of skeleton.
2. a kind of automatic cover-turning hydroplane delta wing according to claim 1, is characterized in that: be connected with two torsion springs between each outer reinforcing frame with each interior reinforcing frame.
3. a kind of automatic cover-turning hydroplane delta wing according to claim 1 and 2, is characterized in that: described column and spider are above and below the same position of crossbeam.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520356152.5U CN204726669U (en) | 2015-05-28 | 2015-05-28 | A kind of automatic cover-turning hydroplane delta wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520356152.5U CN204726669U (en) | 2015-05-28 | 2015-05-28 | A kind of automatic cover-turning hydroplane delta wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204726669U true CN204726669U (en) | 2015-10-28 |
Family
ID=54385041
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520356152.5U Withdrawn - After Issue CN204726669U (en) | 2015-05-28 | 2015-05-28 | A kind of automatic cover-turning hydroplane delta wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204726669U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890870A (en) * | 2015-05-28 | 2015-09-09 | 哈尔滨工程大学 | Hydroplaning delta wing with automatic flipping cover |
| CN109353496A (en) * | 2018-07-04 | 2019-02-19 | 哈尔滨工业大学（威海） | A kind of novel expansion dalta wing flight instruments |
-
2015
- 2015-05-28 CN CN201520356152.5U patent/CN204726669U/en not_active Withdrawn - After Issue
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890870A (en) * | 2015-05-28 | 2015-09-09 | 哈尔滨工程大学 | Hydroplaning delta wing with automatic flipping cover |
| CN104890870B (en) * | 2015-05-28 | 2016-08-24 | 哈尔滨工程大学 | A kind of automatic cover-turning hydroplane dalta wing |
| CN109353496A (en) * | 2018-07-04 | 2019-02-19 | 哈尔滨工业大学（威海） | A kind of novel expansion dalta wing flight instruments |
| CN109353496B (en) * | 2018-07-04 | 2022-05-31 | 哈尔滨工业大学（威海） | Unfolding type delta wing flying device |
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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: 20151028 Effective date of abandoning: 20160824 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |