CN216581006U - Water delta wing aircraft - Google Patents
Water delta wing aircraft Download PDFInfo
- Publication number
- CN216581006U CN216581006U CN202122392209.5U CN202122392209U CN216581006U CN 216581006 U CN216581006 U CN 216581006U CN 202122392209 U CN202122392209 U CN 202122392209U CN 216581006 U CN216581006 U CN 216581006U
- Authority
- CN
- China
- Prior art keywords
- holes
- wing aircraft
- rod
- buoy
- connecting piece
- 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.)
- Active
Links
Images
Landscapes
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
A water delta wing aircraft comprises a delta wing aircraft and is characterized in that the delta wing aircraft is connected with a float seat frame through a wear-resistant sleeve and a hoop and a U-shaped piece; the utility model utilizes the existing framework of the delta-wing aircraft to connect the float seat frame with the delta-wing aircraft, wherein the float seat frame is provided with three vertically arranged floats, two floats at the outer side are provided with side float connecting pieces, a middle float is provided with a middle float connecting piece, and a water baffle is arranged between the front floats; triangular fixing structures are further arranged in the front and the back of the float seat frame.
Description
Technical Field
The utility model relates to a water delta wing aircraft, belonging to the technical field of water craft and water flying sports equipment.
Background
The traditional overwater delta wing aircraft has the defects that the development of the traditional overwater delta wing aircraft is influenced due to low riding comfort, complex structure and low flying efficiency, and the flying experience is seriously influenced due to splashing of water when the traditional overwater delta wing aircraft lands.
Disclosure of Invention
To solve the above problems, the present invention provides a water delta wing aircraft.
A water delta wing aircraft comprises a delta wing aircraft and is characterized in that the delta wing aircraft is connected with a buoy seat frame through a wear-resistant sleeve and a hoop and a U-shaped part; the utility model utilizes the existing framework of the delta wing aircraft to connect the buoy seat frame with the delta wing aircraft.
Two, a three angel wing aircraft on water, characterized by set up wear-resisting cover in the middle of the three angel wing aircraft fossil fragments, wear-resisting cover is equipped with big annular groove by the centre of polymer polyethylene material preparation, and both sides are equipped with little annular groove and set up the sleeve pipe of vertical open slot at its both ends, and middle big groove portion sheathes in the U type spare, and the clamp is overlapped to the little groove in both sides, is equipped with the hole on the clamp, uses double-screw bolt and nut to tighten up the clamp and makes wear-resisting cover be connected with fossil fragments, with double-screw bolt and nut handle big groove department in the middle of wear-resisting cover is fixed to the U type spare, and restriction U type spare reciprocates from beginning to end, only allows the U type spare to follow wear-resisting cover center pin horizontal hunting (be used for changing three angel wing aircraft focus and realize left and right horizontal side manipulation).
Three a three on water delta wing aircraft, characterized by U type spare links to each other with the float seat frame, U type spare middle part is equipped with two holes (is used for blocking wear-resisting cover recess, makes U type spare can only follow wear-resisting cover center pin horizontal hunting), U type spare lower part is equipped with great hole (is connected with double-screw bolt and nut the hole that float seat frame upper boom corresponds to thereby make the float seat frame can only realize the every single move manipulation to the delta wing aircraft along the center pin fore-and-aft oscillation of double-screw bolt, wherein the float seat frame can divide into float frame, seat frame and the fixed subassembly triplex of triangle-shaped.
The water delta wing aircraft is characterized in that the seat frame can be divided into an upper rod, a lower rod, an engine frame, a diagonal draw bar, a bottom rod, a seat connecting plate, an inflatable seat, seat side supporting rods, a front connecting piece, a rear connecting piece and a middle connecting piece;
the upper end of the upper rod is provided with a large hole corresponding to the large hole of the U-shaped part, a connecting groove is welded below the large hole of the upper rod, holes (used for connecting the upper end of the diagonal draw bar) are formed in two sides of the connecting groove, and two holes are formed in the lower end of the upper rod and connected with the corresponding holes of the engine frame;
the engine frame is formed by welding a transverse metal sheet body with a narrow upper part and a wide lower part and two longitudinal metal sheet bodies penetrating through the upper part and the lower part, welding two reinforcing metal sheet bodies intersected with the longitudinal metal sheet bodies at the lower part to improve the overall strength, and performing sheet metal bending treatment on the small metal sheet body at the uppermost part and then welding the metal sheet body with the longitudinal metal sheet to improve the strength; each sheet body is correspondingly hollowed to reduce the weight, and holes corresponding to the upper rod and the lower rod are arranged between the two longitudinal surfaces and used for connecting the upper rod and the lower rod; the back of the engine frame is provided with an engine mounting hole for connecting an engine, a sleeve is arranged between two longitudinal surfaces and a reinforcing surface at the lower part of the engine frame, and a hole is formed in the sleeve and used for connecting the seat side supporting rod;
holes are formed in the two ends of the lower rod, one end of the lower rod is connected with the hole corresponding to the lower part of the engine frame, and the other end of the lower rod is connected with one end of the bottom rod through the hole corresponding to the rear connecting piece;
the rear connecting piece is formed by welding three longitudinal metal sheet bodies and two transverse metal sheet bodies at the bottom, each sheet body is correspondingly hollowed to reduce the weight, the upper part of the rear connecting piece is provided with two longitudinal arrangement holes corresponding to one end of the lower rod and connected with the lower rod, the middle part of the rear connecting piece is provided with two transverse arrangement holes corresponding to one end of the lower rod and connected with the lower rod, the lower part of the rear connecting piece is provided with a semicircular clamping groove, and two sides of the clamping groove are provided with two holes (used for being connected with the buoy frame);
the rear end of the bottom rod is provided with two holes corresponding to the middle part of the rear connecting piece and connected with the rear connecting piece, and the rear part of the bottom rod is also provided with a hole corresponding to the seat connecting plate (used for being connected with the seat connecting plate);
two holes are formed in the middle of the bottom rod, one hole is connected with the seat connecting plate, the middle connecting piece and the middle buoy connecting piece through long studs and nuts, and the other hole is connected with the middle connecting piece and the middle buoy connecting piece through long studs and nuts;
the front end of the bottom rod is provided with two groups of holes which are respectively connected with the holes corresponding to the two front connecting pieces, a connecting groove is welded between the two groups of holes, and the two sides of the connecting groove are provided with holes corresponding to one end of the diagonal draw bar and connected with the lower end of the diagonal draw bar;
the middle connecting piece is formed by welding an upper metal sheet body, a lower metal sheet body, a left metal sheet body and a right metal sheet body, each sheet body is correspondingly hollowed to reduce the weight, the upper surface and the lower surface are provided with through holes, one hole is used for connecting the seat connecting plate, the bottom rod and the middle buoy connecting piece, the other hole is connected with the bottom rod and the middle buoy connecting piece, the side surface of the middle connecting piece is provided with a sleeve, the sleeve is provided with a hole for connecting the seat side supporting rod, and the lower part of the middle connecting piece is provided with a semicircular clamping groove (used for being connected with the middle buoy connecting piece);
the front connecting piece is formed by welding an upper metal sheet body, a lower metal sheet body, a left metal sheet body and a right metal sheet body, each sheet body is correspondingly hollowed to reduce the weight, holes are formed in the left side and the right side and correspond to the holes in the front part of the bottom rod, a semicircular clamping groove is formed in the lower part of the front connecting piece, and holes (used for connecting the middle buoy connecting piece) are formed in the two sides of the clamping groove; the two front connecting pieces are respectively connected with the two middle buoy connecting pieces at the front part;
holes are arranged at two ends of the diagonal draw bar, the upper end of the diagonal draw bar is connected with the hole corresponding to the connecting groove at the upper part of the upper bar, and the lower end of the diagonal draw bar is connected with the hole corresponding to the connecting groove at the front part of the bottom bar;
the seat side supporting rods are divided into a left supporting rod and a right supporting rod, two ends of each seat side supporting rod are bent in a certain radian respectively, holes are formed in two ends of each seat side supporting rod, one end of each seat side supporting rod is connected with the sleeve of the lower part of the engine frame, and the other end of each seat side supporting rod is connected with the sleeve of the middle connecting piece;
the seat connecting plate is composed of an upper layer and a lower layer, the lower layer is a full-through layer, four support rods are welded to the rear portion of the lower layer and welded to the upper layer, the front portion is a single layer, the rear portion is a double layer, holes are formed in the front portion and the rear portion, the hole in the front portion corresponds to the hole in the upper portion of the middle connecting piece and is fixedly connected with one hole in the upper portion of the middle connecting piece through a stud nut, the hole in the rear portion corresponds to the hole in the rear portion of the bottom rod and is fixedly connected with the bottom rod through the stud nut, the front portion is used for connecting front-row seats, and the rear portion is used for connecting rear-row seats;
the bottom of the inflatable seat is bonded and connected with the seat connecting plate by using special glue, and the seat is in an inflatable mode, so that the purpose of the seat is to provide buoyancy to improve safety and improve riding comfort in case of rollover of the delta wing aircraft in water;
fifthly, the buoy frame can be divided into a buoy, a side buoy connecting piece, a middle buoy connecting piece, a transverse connecting rod, a water baffle fixing piece and a water baffle connecting piece;
the buoy is characterized in that the front end and the rear end of the buoy are respectively provided with an upward-warped bow-shaped hollow cylindrical air bag made of PVC material;
the side buoy connecting pieces are formed by welding metal sleeves with holes in the middle, welding metal sheet bodies on the periphery of the lower portion of the metal sleeves and arc-shaped metal plates, and are longitudinally arranged and adhered to the upper portions of the buoys by adopting special glue, wherein each of the two buoys is adhered with four side buoy connecting pieces (the buoys adhered with the side buoy connecting pieces are arranged on the outer sides of the buoy frames);
the middle buoy connecting pieces are formed by a metal sleeve pipe with a hole in the middle, metal sheet bodies are welded on the periphery of the lower portion of the metal sleeve pipe and are welded with an arc-shaped metal plate, metal blocks with holes and hollow bottoms are welded on two sides of the metal sleeve pipe (used for being connected with the seat frame), special glue is adopted for arranging and adhering the metal blocks to the upper portion of one buoy, and four middle buoy connecting pieces are adhered together (the buoy adhered with the middle buoy connecting pieces is arranged in the middle of the buoy frame);
holes corresponding to the sleeve holes of the side buoy connecting piece sleeves are formed in two ends of the transverse connecting rod, four transverse connecting rods are arranged in the front and at the back, the transverse connecting rods penetrate through the middle buoy connecting piece sleeve and the side buoy connecting piece sleeve respectively, the buoy bonded with the middle buoy connecting piece is placed in the middle, and the two buoys bonded with the side buoy connecting pieces are placed on two sides and fixed through stud nuts;
the water delta wing aircraft is characterized in that four water baffles are arranged at the inner side between the buoys of the buoy seat frame and have the function of preventing water splash from splashing upwards when the delta wing aircraft lands; the water baffle is connected with the buoy through a water baffle fixing piece and a water baffle connecting strip; the water baffle fixing pieces are welded on the arc-shaped metal plate through metal blocks with holes in the middle, the bottoms of the arc-shaped metal plates are bonded on the inner side surfaces of the front parts of the buoys through special glue, 2 water baffle fixing pieces are respectively arranged on the inner sides of the two buoys on the two sides of the buoy seat frame, and the two sides of the buoy in the middle of the buoy seat frame are provided with four water baffle fixing pieces;
the two ends of the water baffle connecting piece are provided with holes corresponding to the water baffle fixing pieces and are respectively connected to the holes of the water baffle fixing pieces which are parallel at the same side;
the water baffle is made of light-density materials (such as aluminum alloy plates), the front part of the water baffle is arc-shaped, and holes are formed in the front end and the rear end of the water baffle and used for being connected with the water baffle connecting piece.
The seaplane delta wing aircraft is characterized in that the triangle fixing components are arranged at the front part and the rear part of the float seat frame and can be divided into a large fastener, a small fastener, two front oblique rods and two rear oblique rods;
the two ends of the large fastener are provided with holes, and the middle of the large fastener is a semi-arc metal piece;
the small fastener is provided with holes at two ends, the middle part of the small fastener is a semi-arc metal piece, the shape of the metal piece is similar to that of the large fastener, and the difference is that the semi-arcs are different in size;
the rear inclined rod is provided with a left inclined rod and a right inclined rod, and is characterized in that two ends of the rear inclined rod are provided with a notch and a hole;
the front inclined rod is provided with a left inclined rod and a right inclined rod, and is characterized in that the upper end of the front inclined rod is provided with an inclined groove with a certain angle, the lower end of the front inclined rod is provided with a vertical groove, and the two ends of the front inclined rod are provided with openings.
Seventhly, the water delta wing airplane is characterized by further comprising a propeller, wherein the propeller comprises a propeller driven by a motor;
the propeller is fixed on the engine frame;
eighthly, power and flight modes;
the water delta wing aircraft can adopt an electric motor as a power device, also can adopt an aero-engine as a power device, and also can adopt water surface traction as a power device.
Drawings
FIG. 1 is a first perspective view of the present invention;
FIG. 2 is a second perspective view of the present invention;
FIG. 3 is a third perspective view of the present invention;
FIG. 4 is a fourth perspective view of the present invention;
FIG. 5 is a perspective view of the present invention;
FIG. 6 is a front view of the present invention;
FIG. 7 is a side view of the present invention;
FIG. 8 is a top view of the present invention;
FIG. 9 is a bottom view of the present invention;
FIG. 10 is a rear view of the present invention;
FIG. 11 is a schematic view of a delta wing aircraft;
FIG. 12 is a schematic view of a spar seat mount;
FIG. 13 is a schematic view of the connection of the delta wing aircraft keel to the pontoon seat frame;
FIG. 14 is a schematic view of the U-shaped member with the wear sleeve and clip;
FIG. 15 is a schematic view of a seat frame assembly;
FIG. 16 is a schematic view of a buoy frame assembly;
FIG. 17 is a schematic view of the attachment of the float frame to the seat frame and its components;
FIG. 18 is a schematic view of a triangular fixation assembly;
FIG. 19 is a schematic view of a first embodiment of a seat frame and hole locations thereof;
FIG. 20 is a second schematic view of parts of the seat frame and hole locations thereof;
FIG. 21 is a schematic view of the pontoon mount components and their hole sites;
FIG. 22 is a schematic view of a motor engine and its hole site;
FIG. 23 is a schematic view of each part of the triangular fixing member and its hole site;
FIG. 24 is a schematic view of a stud and nut.
Wherein, 1, a delta wing aircraft, 2, a buoy seat frame, 3, a wear-resistant sleeve, 4, a U-shaped member, 5, a hoop, 6, a keel, 7, an upper rod, 8, an engine frame, 9, a lower rod, 10, a rear connecting piece, 11, a bottom rod, 12, a middle connecting piece, 13, a front connecting piece, 14, a diagonal draw bar, 15, a seat side supporting rod, 16, a seat connecting plate, 17, an inflatable seat, 18, a buoy, 19, a side buoy connecting piece, 20, a middle buoy connecting piece, 21, a transverse connecting rod, 22, a water baffle fixing piece, 23, a water baffle connecting strip, 24, a water baffle, 25, a front diagonal rod, 26, a small fastener, 27, a rear diagonal rod, 28, a large fastener, 29, an engine, 30, a stud (8 x 15), 31, a stud (8 x 40), 32, a stud (8 x 50), 33, a stud (8 x 75), 34, a stud (8 x 100), 35, a stud (14 x 75), 36. nuts (14M), 37, nuts (8M);
wherein, a hole 501 is arranged on the hoop 5;
the lower rod 9 is provided with holes 91, 92, 93, 94;
the rear connecting piece 10 is provided with holes 101, 102, 103, 104, 105, 106;
the bottom bar 11 is provided with holes 110, 111, 112, 113, 114, 115, 116, 117, 118, 119;
the middle connecting piece 12 is provided with holes 121, 122, 123 and 124;
the front connecting piece 13 is provided with holes 131, 132, 133, 134;
the diagonal member 14 has holes 141, 142;
the seat side stay 15 is provided with holes 151, 152;
the seat attachment plate 16 is provided with holes 161, 162;
the side buoy connection piece 19 is provided with a hole 191;
the middle buoy connecting piece 20 is provided with holes 201 and 202;
the transverse connecting rod 21 is provided with holes 211 and 212;
the water baffle fixing piece 22 is provided with a hole 221;
the water baffle connecting strip 23 is provided with holes 231, 232, 233 and 234;
the water guard plate 24 is provided with holes 241, 242;
the front diagonal 25 is provided with holes 251, 252;
the small fastener 26 is provided with holes 261, 262;
the rear diagonal 27 is provided with holes 271, 272;
the large fastener 28 is provided with holes 281 and 282;
the engine 29 is provided with holes 291, 292, 293, 294;
Detailed Description
The water delta wing aircraft comprises a delta wing aircraft 1 and is characterized in that the delta wing aircraft 1 is connected with a buoy seat frame 2 through a wear-resistant sleeve 3, a U-shaped part 4 and a clamp 5; a wear-resistant sleeve 3 is sleeved on the middle of a keel 6 of the delta wing aircraft 1, grooves on two sides of the wear-resistant sleeve 3 are respectively sleeved with a hoop 5, and a stud 30 and a nut 37 are used for fastening a hole 501 of the hoop 5, so that the wear-resistant sleeve 3 is connected to the keel 6; the U-shaped part 4 is sleeved on a groove in the middle of the wear-resistant sleeve 3, and the holes 402 and 403 of the U-shaped part 4 are connected and fastened by using a stud 33 and a nut 37, so that the U-shaped part 4 can only swing left and right along the central axis of the wear-resistant sleeve 3 (the function is to realize left and right transverse operation by changing the gravity center of the delta wing aircraft 1);
the holes 401 of the U-shaped members 4 are aligned with the holes 71 in the upper beam 7 of the pontoon seat frame 2 and fastened using the studs 35 and nuts 36, so that the pontoon seat frame 2 can only swing back and forth along the central axis of the studs 35 (for pitch angle manoeuvres by changing the centre of gravity of the delta wing vehicle 1).
As shown in fig. 15-18, the pontoon seat frame 2 can be divided into a seat frame, a pontoon frame and a triangular fixed component;
the seat frame can be divided into an upper rod 7, an engine frame 8, a lower rod 9, a rear connecting piece 10, a bottom rod 11, a middle connecting piece 12, two front connecting pieces 13, a diagonal draw bar 14, two seat side supporting rods 15, a seat connecting plate 16 and two inflatable seats 17;
as shown in fig. 14-15 and fig. 19-20, the upper end of the upper rod 7 is provided with a hole 71 which is aligned with a hole 401 of the U-shaped member 4 and is connected and fastened by using a stud 35 and a nut 36, and the lower end holes 73 and 74 of the upper rod 7 are respectively aligned with holes 82 and 83 of the engine frame 8 and are connected and fastened by using a stud 33 and a nut 37;
the holes 80 and 81 of the engine frame 8 are respectively aligned with the holes 91 and 92 at one end of the lower rod 9 and are connected and fastened by using a stud 33 and a nut 37; the holes 93 and 94 at the other end of the lower rod 9 are respectively aligned with the holes 101 and 102 of the rear connecting piece 10 and are connected and fastened by using a stud 33 and a nut 37;
the holes 103 and 104 of the rear connecting piece 10 are respectively aligned with the holes 118 and 119 at one end of the bottom rod 11 and are connected and fastened by using a stud 33 and a nut 37;
the hole 117 of the bottom bar 11 is aligned with the hole 162 of the seat attachment plate 16 and fastened using the stud 33 and nut 37 connection;
the bottom rod 11 passes through the middle connecting piece 12, the hole 116 in the middle of the bottom rod 11 is respectively aligned with the hole 161 of the seat connecting plate 16, the hole 124 of the middle connecting piece 12 and the hole 201 of the middle buoy connecting piece 20 and is connected and fastened by using the stud 34 and the nut 37, and the hole 115 of the bottom rod 11 is aligned with the hole 123 of the middle connecting piece 12 and is connected and fastened by using the stud 34 and the nut 37;
the bottom rod 11 passes through the two front connecting pieces, and two groups of holes 113, 114, 111 and 112 at the front part of the bottom rod 11 are respectively aligned with the holes 131 and 132 of the two front connecting pieces 13 and are connected and fastened by using a stud 33 and a nut 37;
the hole 110 of the bottom bar 11 is aligned with the hole 141 of one end of the diagonal member 14 and fastened by the stud 32 and the nut 37;
the hole 142 at the other end of the diagonal draw bar 14 is aligned with the hole 72 at one end of the upper bar 7 and is connected and fastened by using the stud 32 and the nut 37;
two inflatable seats 17 are placed between the two seat side supporting rods 15, and the bottoms of the inflatable seats 17 are bonded and connected with the seat connecting plate 16 by using special glue;
referring to fig. 16, 17 and 21, the pontoon frame can be divided into a pontoon 18, a side pontoon connecting piece 19, a middle pontoon connecting piece 20, a transverse connecting rod 21, a water baffle fixing piece 22, a water baffle connecting strip 23 and a water baffle 24;
the water delta wing aircraft is characterized in that the number of the buoys 18 of the buoy seat frame 2 is three, four side buoy connecting pieces 19 are respectively and longitudinally arranged at the upper parts of the two outer buoys 18, and four middle buoy connecting pieces 20 are respectively and longitudinally arranged at the upper part of the middle buoy 18; the transverse connecting rod 21 respectively passes through the sleeves of the two side buoy connecting pieces 19 and the middle buoy connecting piece 20 in a horizontal position, and holes 211 and 212 at two ends of the transverse connecting rod 21 are respectively aligned with holes 191 of the two side buoy connecting pieces 19 on the side and are connected and fastened by using a stud 32 and a nut 37;
the water delta wing aircraft is characterized in that four water baffles 24 are arranged at the inner side between the buoys 18 of the buoy seat frame 2; the hole 221 of the water baffle fixing piece 22 corresponds to the holes 231 and 232 at the two ends of the water baffle connecting strip 23 respectively and is connected and fastened by a stud 30 and a nut 37;
the triangular fixing component is shown in fig. 18 and 23 and comprises a front oblique rod 25, a small fastener 26, a rear oblique rod 27 and a large fastener 28; the water delta-wing aircraft is characterized in that a lower rod 9, a diagonal draw bar 14 and a transverse connecting rod 21 of the float seat frame 2 are respectively connected with two front oblique rods 25 and two rear oblique rods 27 through small fasteners 26 and large fasteners 28 to form a front triangular fixing structure and a rear triangular fixing structure;
the small fasteners 26 are buckled on the diagonal draw bars 14, holes 251 at one end of the two front diagonal rods 25 with oblique clamping grooves are respectively aligned with holes 261 and 262 at two ends of the small fasteners 26 and are connected and fastened by using studs 30 and nuts 37; another two small fasteners 26 are fastened on two sides of a second transverse connecting rod 21 of the buoy frame, one end of each small fastener 26 is inserted into the clamping groove of the front oblique rod 25, the hole 252 in the clamping groove of the front oblique rod 25 is aligned with the hole 261 of the small fastener 26 and is connected and fastened by using a stud 30 and a nut 37, and the hole 262 at the other end of the small fastener 26 is fastened by using the stud 30 and the nut 37;
the rear inclined rods 27 are divided into a left inclined rod and a right inclined rod, two ends of a large fastener 28 are respectively clamped into clamping grooves at the upper ends of the two rear inclined rods 27, holes 271 at the upper ends of the rear inclined rods 27 are respectively corresponding to holes 281 and 282 at two ends of the large fastener 28, the large fastener 28 is buckled on the upper part of the lower rod 9 and is connected and fastened by using a stud 30 and a nut 37, clamping grooves at the lower ends of the rear inclined rods 27 are respectively clamped at one ends of small fasteners 26, holes 272 of clamping grooves at the lower ends of the rear inclined rods 27 are aligned with holes 261 at one ends of the small fasteners 26, the small fasteners 26 are buckled with the transverse connecting rod 21 at the rear part of the buoy frame and then are connected and fastened by using the stud 30 and the nut 37 (the upper ends of the two rear inclined rods 27 are connected with the lower rod 9 through the large fastener 28, and the other ends of the two rear inclined rods 27 are respectively connected with the transverse connecting rod 21 through the other two small fasteners 26 to form a triangular stable structure);
18-24, the front connector 13 is aligned with the holes 201, 202 of the intermediate pontoon connector 20 through the holes 133, 134 and tightened using the stud 30 and nut 37;
the rear connector 10, aligned with the holes 201, 202 of the intermediate buoy connector 20 through the holes 105, 106 and fastened using the stud 30 and nut 37;
the middle connector 12 is aligned with the holes 201 and 202 of the middle buoy connector 20 through the holes 123 and 124 and fastened by using a stud 34 and a nut 37;
the engine 29 is shown in fig. 18, 20, 22 aligned with the engine mount holes 86, 87, 88, 89 through the holes 291, 292, 293, 294 and secured using the stud 30 and nut 37.
Claims (2)
1. A water delta wing aircraft comprises a delta wing aircraft (1), and is characterized in that the delta wing aircraft (1) is connected with a float seat frame (2) through a wear-resistant sleeve (3), a U-shaped part (4) and a clamp (5); lower beam (9), oblique pull rod (14), transverse connection pole (21) of flotation pontoon seat frame (2) are connected through little fastener (26), big fastener (28) with two preceding down tube (25), two back down tube (27) respectively and are formed two triangle-shaped fixed knot in front and back.
2. The seaplane as set forth in claim 1, characterized in that four water baffles (24) are provided between the pontoons (18) of the pontoon seat frame (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122392209.5U CN216581006U (en) | 2021-09-30 | 2021-09-30 | Water delta wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122392209.5U CN216581006U (en) | 2021-09-30 | 2021-09-30 | Water delta wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216581006U true CN216581006U (en) | 2022-05-24 |
Family
ID=81639996
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122392209.5U Active CN216581006U (en) | 2021-09-30 | 2021-09-30 | Water delta wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216581006U (en) |
-
2021
- 2021-09-30 CN CN202122392209.5U patent/CN216581006U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3796175A (en) | Catamaran | |
| CN110382342B (en) | Manpower-driven hydrofoil vehicle and using method | |
| US3739410A (en) | Collapsible boat with v-shaped pneumatic float | |
| US3212109A (en) | Water craft | |
| US6659403B2 (en) | Inflatable airfoils, and elevated and propulsion driven vehicles | |
| US4449473A (en) | Inflatable boat with demountable transom | |
| US7314018B2 (en) | Collapsible boat hull | |
| US4348971A (en) | Multi-hull boats | |
| US3866557A (en) | Semi-submerged vessel adaptable to sailing | |
| CN216581006U (en) | Water delta wing aircraft | |
| US3696451A (en) | Tube float or boat | |
| DE4030225C2 (en) | ||
| US5313908A (en) | Car topable catamaran with collapsible frame and universal tiller/rudder-mast daggerboard mounting constructions | |
| US4993340A (en) | Boat structure | |
| US3611459A (en) | Composite boat | |
| CN205381359U (en) | Portable deformation angling boat | |
| US6688553B2 (en) | Inflatable airfoils, and elevated and propulsion driven vehicles | |
| KR101523465B1 (en) | Portable folding boat | |
| CN206954467U (en) | A kind of anticollision device, collision-prevention device for fan ship | |
| EP0802872B1 (en) | Catamaran | |
| US20140150705A1 (en) | Inflatable hull structure and method of forming an inflatable boat hull | |
| US4397366A (en) | Air cushion vehicles | |
| KR200398223Y1 (en) | Boat | |
| GB2024112A (en) | Multi-hull boat | |
| WO2001012501A1 (en) | Modular water craft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |