CN108357663A - The gas compressor expander wing of seaplane - Google Patents
The gas compressor expander wing of seaplane Download PDFInfo
- Publication number
- CN108357663A CN108357663A CN201810268203.7A CN201810268203A CN108357663A CN 108357663 A CN108357663 A CN 108357663A CN 201810268203 A CN201810268203 A CN 201810268203A CN 108357663 A CN108357663 A CN 108357663A
- Authority
- CN
- China
- Prior art keywords
- wing
- plate
- inflatable bladder
- edge
- abdomen
- 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- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/30—Wings comprising inflatable structural components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The gas compressor expander wing of seaplane, including inflatable bladder, axis connected device, soft even water-impermeable piece, air pump and reel motor；It is characterized in that：There are one inflatable bladders for installation between the wing wing backboard and wing wing web of wing,Rear courage face of the inflatable bladder between wing wing backboard back plate edge and wing wing web back plate edge is flexible courage face,The inflation of inflatable bladder is completed by air pump,The deflation of inflatable bladder is folded to be driven to reel line and fold the back plate edge of wing wing web and move to wing wing backboard back plate edge from reel motor and be completed,Reel motor is mounted on the inside of wing wing backboard back plate edge,More one end for reeling line are on the spool of reel motor,The more other ends for reeling line are evenly distributedly fixed on the inside of wing wing web back plate edge,Unlatching reel motor, which rotates and opens motor-driven valve, opens appendix,Reel motor winding reels line and wing wing web back plate edge is pulled to be moved to wing wing backboard back plate edge,Squeezing inflatable bladder makes the air in inflatable bladder be discharged outside inflatable bladder through appendix and the motor-driven valve of opening.
Description
Technical field
The present invention relates to the gas compressor expander wings of seaplane, are suitable for various middle-size and small-size aircrafts, belong to aircraft technology neck
Domain.
Background technology
The buoyancy of present amphibious aircraft in water is mainly formed by space in fuselage, gives fuselage increased in this way
Spatial band carrys out larger fuselage resistance, and the present invention is one inflatable bladder of installation in wing, allow wing wing wing backboard and
The front end of wing wing web is connected by axis connected device, and the rear end of wing wing backboard and wing wing web and can freely be opened around axis connected device
It closes, aircraft can land when flight in the air after so that inflatable bladder is inflated, and can also be parked on the water surface and float and take off, this is inflatable
The big buoyancy that is formed in water of wing brought convenience to aircraft stop on the water and taking off.
Invention content
Utilize the installation inflatable bladder inflation in the wing of aircraft that aircraft is allow to exist the object of the present invention is to provide a kind of
The gas compressor expander wing of the seaplane of takeoff and landing on the water surface.
The gas compressor expander wing of seaplane, including inflatable bladder, axis connected device, soft even water-impermeable piece, air pump and reel motor；
It is characterized in that：
1, wing is made of wing wing backboard and wing wing web, and wing wing backboard is upper, and wing wing web is under, the wing wing back of the body
There are one inflatable bladders for installation between plate and wing wing web, and the section of parallel airframe axis is at one after inflatable bladder inflation
A triangle, each angle of triangle are fillet, and an angle of triangle is clipped in wing nose, and second angle of triangle is after wing
The wing wing backboard back plate edge at end, the third angle of triangle is in the wing wing web back plate edge in rear airfoil end, inflatable bladder
Upper courage face is pasted onto on the inside of the wing inner panel of wing wing backboard, and courage face is pasted onto the wing inner panel of wing wing web under inflatable bladder
Inside, the courage face between the third courage face, that is, wing wing backboard back plate edge and wing wing web back plate edge of inflatable bladder are rear courage
Face, rear courage face is flexible courage face, after inflatable bladder is inflated, rear courage face camber face, after inflatable bladder is deflated, rear courage face at
Fold plane, foldable layer reels line by more and receives gear in wing wing backboard back plate edge and the wing wing web back plate edge when rear courage face folds
In the closure mouth of closure；Inflatable bladder is that rubberized fabric constitutes air seal bag, or constitutes air seal bag for nylon cloth line with rubber.
2, the inflation of inflatable bladder is completed by air pump, and air pump is connect with inflatable bladder by appendix, on appendix there are one
Motor-driven valve opens motor-driven valve and just opens appendix access, closes motor-driven valve and just blocks appendix access, air pump and motor-driven valve are by flying
The control system of machine controls, when inflatable bladder is inflated, as the inflation of inflatable bladder makes wing wing web back plate edge to far from machine
The movement in thriving backboard back plate edge direction, wing wing web back plate edge, which hauls, to be reeled line and reel motor is driven to rotate, and lengthen receipts
Bracing wire.
3, the deflation of inflatable bladder folds to be driven from reel motor and reels line and fold the back plate edge of wing wing web to wing
The movement of wing backboard back plate edge is completed, and reel motor is mounted on the inside of wing wing backboard back plate edge, the more one end windings for reeling line
On the spool of reel motor, the more other ends for reeling line are evenly distributedly fixed on the inside of wing wing web back plate edge, are opened
Reel motor rotation is opened, motor-driven valve is opened simultaneously and opens appendix, reel motor winding reels line and pulls wing wing web back plate
Edge is moved to wing wing backboard back plate edge, and squeezing inflatable bladder makes motor-driven valve of the air in inflatable bladder through appendix and opening
It is discharged outside inflatable bladder.
4, the foreboard edge of wing wing backboard is connected with the multiple axis connected devices of the back plate cause of wing wing web, each axis connected device by
Axis connects curved boom, axis connects straight-arm and axis connects shaft composition, and axis connects curved boom on the inside of the wing outside plate foreboard edge of wing wing backboard,
Axis connects straight-arm on the inside of the wing outside plate foreboard edge of wing wing web, and axis connects curved boom and axis connects straight-arm and connects shaft company by axis
It connects, so that axis is connected curved boom and axis connects straight-arm can connect shaft rotation, the wing outside plate of the wing wing web near axis connected device around axis
The soft even water proof of a block length bar shaped is installed between on the outside of foreboard edge and on the inside of the wing outside plate foreboard edge of wing wing backboard
The effect of piece, soft even water-impermeable piece is that water is prevented to enter in the wing outside plate of wing, and soft even water-impermeable piece is rubberized fabric or nylon cloth
Line with rubber cloth.
5, it is installed with more support steels between wing outside plate and wing inner panel, makes wing outside plate, wing inner panel, bearing
Steel three is composed of a fixed connection the wing wing backboard and wing wing web of wing.
6, one piece of elevating plane is installed, elevating plane can be carried on the back around elevating plane and the wing wing on the outside of the back plate edge of wing wing backboard
Plate connecting shaft is done to rotate up and down, is drawn high to vertical angle or downward diving flight with controlling aircraft.
Compared with the prior art, the present invention has the following advantages：
1, currently on the market it has not been found that the product similar or similar with the present invention, does not find pertinent literature or patent money yet
Material；
2, the present invention is inflated using wing, simple in structure, using flexible, reliable and stable；
3, wing inflation of the present invention, not will increase the skyborne flight resistance of aircraft.
Description of the drawings
Fig. 1 is wing swelling state schematic diagram in the embodiment of the present invention；
Fig. 2 is wing deflation status schematic diagram in embodiment illustrated in fig. 1；
Fig. 3 is wing schematic view of the mounting position in embodiment illustrated in fig. 1；
Fig. 4 is wing profile structural schematic diagram in embodiment illustrated in fig. 1；
Fig. 5 is P enlarged diagrams in embodiment illustrated in fig. 2；
Fig. 6 is Q enlarged diagrams in embodiment illustrated in fig. 5；
Fig. 7 is A-A cross-sectional views in embodiment illustrated in fig. 6；
Fig. 8 is R enlarged diagrams in embodiment illustrated in fig. 6；
Fig. 9 is S enlarged diagrams in embodiment illustrated in fig. 1.
In Fig. 1-9：1, wing nose, 2, the wing wing back of the body, 3, wing wing abdomen, 4, rear airfoil end, 5, inflatable bladder, 6,
Reel line, 7, elevating plane, 8, fuselage, 9, wing, 10, support steel, 11, wing outside plate, 12, wing inner panel, 13, axis connects
Device, 14, wing outside plate commissure mouth, 15, axis connect curved boom, 16, axis connect straight-arm, 17, axis connect shaft, 18, soft even water-impermeable piece,
19, appendix, 20, air pump, 21, reel motor.
Specific implementation mode
In the embodiment shown in Fig. 1-9：The gas compressor expander wing of seaplane, including inflatable bladder 5, axis connected device 13, soft company
Water-impermeable piece 18, air pump 20 and reel motor 21；It is characterized in that：Wing 9 carries on the back 2 plates and 3 board group of wing wing abdomen into machine by the wing wing
Cautiously 2 plates of the back of the body are upper, and 3 plate of wing wing abdomen is under, and the wing wing carries on the back installation between 2 plates and 3 plate of wing wing abdomen, and there are one inflatable bladders
5, the section of parallel airframe axis is at a triangle after inflatable bladder 5 is inflated, and each angle of triangle is fillet, triangle
One angle is clipped in wing nose 1, and 2 plate back plate edge are carried on the back in second angle of triangle in the wing wing of rear airfoil end 4, and the of triangle
Three angles courage face on the 3 plate back plate edge of wing wing abdomen in rear airfoil end 4, inflatable bladder 5 is pasted onto the wing that the wing wing carries on the back 2 plates
12 inside of inner panel, 5 times courage faces of inflatable bladder are pasted onto 12 inside of wing inner panel of 3 plate of wing wing abdomen, the third of inflatable bladder 5
It is rear courage face that courage face, that is, wing wing, which carries on the back the courage face between 2 plate back plate edge and 3 plate back plate edge of wing wing abdomen, and rear courage face is flexible courage
Face, after inflatable bladder 5 is inflated, rear courage face camber face, after inflatable bladder 5 is deflated, rear courage face is at fold plane, rear courage face folding
Foldable layer reels line 6 by more and receives the closure mouth that gear is closed in the wing wing 2 plate back plate edge of the back of the body and 3 plate back plate edge of the wing wing abdomen when folded
It is interior；Inflatable bladder 5 is that rubberized fabric constitutes air seal bag, or constitutes air seal bag for nylon cloth line with rubber.
The inflation of inflatable bladder 5 is completed by air pump 20, and air pump 20 is connect with inflatable bladder 5 by appendix 19, appendix 19
Upper there are one motor-driven valves, open motor-driven valve and just open 19 access of appendix, close motor-driven valve and just block 19 access of appendix, air pump
20 and motor-driven valve by aircraft control system control, inflatable bladder 5 inflate when, as the inflation of inflatable bladder 5 makes wing wing abdomen 3
To the movement for carrying on the back 2 plate back plate edge directions far from the wing wing, 3 plate back plate edge of wing wing abdomen hauls to be reeled line 6 and drives plate back plate edge
Reel motor 21 rotates, and lengthens and reels line 6.
The deflation of inflatable bladder 5 folds to be driven from reel motor 21 and reels line 6 and fold the back plate edge of 3 plate of wing wing abdomen to machine
Cautiously the movement of 2 plate back plate edge of the back of the body is completed, and reel motor 21 is mounted on the inside of 2 plate back plate edge of the wing wing back of the body, more reel line 6 one
On the spool of reel motor 21, the more other ends for reeling line 6 are evenly distributedly fixed on 3 plate back plate of wing wing abdomen at end
It on the inside of edge, opens reel motor 21 and rotates, open simultaneously motor-driven valve and open appendix 19, the winding of reel motor 21 reels the drawing of line 6
The thriving 3 plate back plate edge of abdomen of motivation carries on the back the movement of 2 plate back plate edge to the wing wing, and squeezing inflatable bladder 5 makes the air in inflatable bladder 5 pass through
Outside appendix 19 and the motor-driven valve discharge inflatable bladder 5 opened.
The multiple axis connected devices 13 of back plate cause that the wing wing carries on the back 3 plate of foreboard edge and wing wing abdomen of 2 plates connect, each axis connected device
13 connect curved boom 15 by axis, axis connects straight-arm 16 and axis connects shaft 17 and forms, and axis connects curved boom 15 outside the wing that the wing wing carries on the back 2 plates
On the inside of 11 foreboard edge of plate, axis connects straight-arm 16 on the inside of the 11 foreboard edge of wing outside plate of 3 plate of wing wing abdomen, axis connect curved boom 15 with
Axis, which connects straight-arm 16 and connects shaft 17 by axis, to be connected, and makes that axis connects curved boom 15 and axis connects straight-arm 16 and can connect the rotation of shaft 17 around axis, in axis
On the outside of the 11 foreboard edge of wing outside plate of 3 plate of wing wing abdomen near connected device 13 and the wing wing carries on the back the 11 foreboard edge of wing outside plate of 2 plates
The soft even water-impermeable piece 18 of a block length bar shaped is installed between inside, the effect of soft even water-impermeable piece 18 is that water is prevented to enter wing
Wing outside plate 11 in, soft even water-impermeable piece 18 is the line with rubber cloth of rubberized fabric or nylon cloth.
It is installed with more support steels 10 between wing outside plate 11 and wing inner panel 12, makes wing outside plate 11, in wing
The be composed of a fixed connection wing wing of wing 9 of plate 12,10 three of support steel carries on the back 2 plates and 3 plate of wing wing abdomen.
The back plate edge outside that the wing wing carries on the back 2 plates is equipped with one piece of elevating plane 7, and elevating plane 7 can be around elevating plane 7 and the wing wing
It carries on the back 2 plate connecting shafts and does and rotate up and down, drawn high to vertical angle or downward diving flight with controlling aircraft.
Claims (3)
1. the gas compressor expander wing of seaplane, including inflatable bladder（5）, axis connected device（13）, it is soft even water-impermeable piece（18）, air pump
（20）And reel motor（21）；It is characterized in that：Wing（9）It is carried on the back by the wing wing（2）Plate and wing wing abdomen（3）Board group is at wing
The wing is carried on the back（2）Plate is in upper, wing wing abdomen（3）Plate is under, the wing wing back of the body（2）Plate and wing wing abdomen（3）There are one fill for installation between plate
Gas liner（5）, inflatable bladder（5）At a triangle, each angle of triangle is circle in the section of parallel airframe axis after inflation
One angle at angle, triangle is clipped in wing nose（1）, second angle of triangle is in rear airfoil end（4）The wing wing back of the body（2）Plate
Back plate edge, the third angle of triangle is in rear airfoil end（4）Wing wing abdomen（3）Plate back plate edge, inflatable bladder（5）Upper courage face
It is pasted onto the wing wing back of the body（2）The wing inner panel of plate（12）Inside, inflatable bladder（5）Lower courage face is pasted onto wing wing abdomen（3）Plate
Wing inner panel（12）Inside, inflatable bladder（5）Third courage face, that is, the wing wing back of the body（2）Plate back plate edge and wing wing abdomen（3）Plate
Courage face between back plate edge is rear courage face, and rear courage face is flexible courage face, works as inflatable bladder（5）After inflation, rear courage face camber face,
Work as inflatable bladder（5）After deflation, rear courage face is at fold plane, and foldable layer reels line by more when rear courage face folds（6）Gear is received in machine
The cautiously back of the body（2）Plate back plate edge and wing wing abdomen（3）In the closure mouth that plate back plate edge is closed；Inflatable bladder（5）It is constituted for rubberized fabric
Air seal bag, or constitute air seal bag for nylon cloth line with rubber；Inflatable bladder（5）Inflation by air pump（20）It completes, air pump
（20）With inflatable bladder（5）By appendix（19）Connection, appendix（19）Motor-driven valve there are one upper, opening motor-driven valve are just opened defeated
Tracheae（19）Access closes motor-driven valve and just blocks appendix（19）Access, air pump（20）With motor-driven valve by the control system of aircraft
Control, inflatable bladder（5）When inflation, with inflatable bladder（5）Inflation make wing wing abdomen（3）Plate back plate edge is to far from the wing wing
The back of the body（2）The movement in plate back plate edge direction, wing wing abdomen（3）Plate back plate edge, which hauls, reels line（6）And drive reel motor（21）Rotation
Turn, lengthens and reel line（6）；Inflatable bladder（5）Deflation fold by reel motor（21）Drive reels line（6）Fold wing wing abdomen
（3）The back plate edge of plate is carried on the back to the wing wing（2）The movement of plate back plate edge is completed, reel motor（21）It is carried on the back mounted on the wing wing（2）After plate
On the inside of plate edge, more reel line（6）One end wound on reel motor（21）Spool on, more reel line（6）The other end
Evenly distributedly it is fixed on wing wing abdomen（3）On the inside of plate back plate edge, reel motor is opened（21）Rotation, opens simultaneously motor-driven valve and opens
Logical appendix（19）, reel motor（21）Winding reels line（6）Pull wing wing abdomen（3）Plate back plate edge is carried on the back to the wing wing（2）Plate
Back plate edge moves, and squeezes inflatable bladder（5）Make inflatable bladder（5）Interior air is through appendix（19）It is discharged with open motor-driven valve
Inflatable bladder（5）Outside.
2. the wing wing is carried on the back（2）The foreboard edge and wing wing abdomen of plate（3）The multiple axis connected devices of back plate cause of plate（13）Connection, each axis
Connected device（13）Curved boom is connected by axis（15）, axis connect straight-arm（16）Connect shaft with axis（17）Composition, axis connect curved boom（15）Mounted on wing
The wing is carried on the back（2）The wing outside plate of plate（11）On the inside of foreboard edge, axis connects straight-arm（16）Mounted on wing wing abdomen（3）The wing outside plate of plate
（11）On the inside of foreboard edge, axis connects curved boom（15）Connect straight-arm with axis（16）Shaft is connected by axis（17）Connection, makes axis connect curved boom（15）With
Axis connects straight-arm（16）It can connect shaft around axis（17）Rotation, in axis connected device（13）Neighbouring wing wing abdomen（3）The wing outside plate of plate
（11）It is carried on the back with the wing wing on the outside of foreboard edge（2）The wing outside plate of plate（11）It is installed with a block length bar shaped between on the inside of foreboard edge
It is soft even water-impermeable piece（18）, soft even water-impermeable piece）18（Effect be that water is prevented to enter the wing outside plate of wing（11）It is interior, soft company every
Water piece（18）For rubberized fabric or the line with rubber cloth of nylon cloth.
3. wing outside plate（11）With wing inner panel（12）Between be installed with more support steels（10）, make wing outside plate（11）、
Wing inner panel（12）, support steel（10）Three is composed of a fixed connection wing（9）The wing wing back of the body（2）Plate and wing wing abdomen（3）Plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810268203.7A CN108357663A (en) | 2018-03-29 | 2018-03-29 | The gas compressor expander wing of seaplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810268203.7A CN108357663A (en) | 2018-03-29 | 2018-03-29 | The gas compressor expander wing of seaplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108357663A true CN108357663A (en) | 2018-08-03 |
Family
ID=63001288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810268203.7A Withdrawn CN108357663A (en) | 2018-03-29 | 2018-03-29 | The gas compressor expander wing of seaplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108357663A (en) |
-
2018
- 2018-03-29 CN CN201810268203.7A patent/CN108357663A/en not_active Withdrawn
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2658321C (en) | Retracting air cushioned landing system for air vehicles | |
| CN105905298B (en) | A kind of swing-wing seaplane | |
| US3711039A (en) | Pneumatic leading edge flap for an aircraft wing | |
| US3184187A (en) | Retractable airfoils and hydrofoils | |
| US2886265A (en) | Light weight pneumatic airplane | |
| CN109229342A (en) | A kind of foldable retractable buffer air bag landing gear and landing concept | |
| US20040188567A1 (en) | Inflatable wing with manifold | |
| CN108357663A (en) | The gas compressor expander wing of seaplane | |
| US2463351A (en) | Aircraft and undercarriage therefor | |
| CZ353199A3 (en) | Set of expandable/retractable supporting surface for aircraft with fixed wing | |
| US10676172B1 (en) | Deployable wing for an aircraft | |
| CN108263611A (en) | Water takeoff and landing aircraft | |
| US1375055A (en) | Ship-salvaging device | |
| CN108657428A (en) | Zither parafoil | |
| US2193029A (en) | Safety device for aircraft | |
| CN208576725U (en) | A kind of hydrofoil and air bag combined type water surface lifting gear | |
| CN207617941U (en) | A kind of novel and multifunctional deliverance apparatus waterborne | |
| WO2018224033A1 (en) | Aircraft with imitation beetle elytron wings | |
| WO2010051685A1 (en) | Flying car | |
| US1866942A (en) | Refueling equipment | |
| CN115303433A (en) | Carrier-borne inflation recovery platform of fixed-wing unmanned aerial vehicle, unfolding and recovery method | |
| US3352519A (en) | Parachute assembly for aircraft | |
| CN209274890U (en) | A kind of folding and retraction gasbag-type landing gear | |
| US1686130A (en) | Aircraft | |
| CN110576970A (en) | Hydrofoil and air bag combined type water surface lifting device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180803 |
|
| WW01 | Invention patent application withdrawn after publication |