CN207890007U - A kind of aircraft catapult launching apparatus - Google Patents
A kind of aircraft catapult launching apparatus Download PDFInfo
- Publication number
- CN207890007U CN207890007U CN201820178928.2U CN201820178928U CN207890007U CN 207890007 U CN207890007 U CN 207890007U CN 201820178928 U CN201820178928 U CN 201820178928U CN 207890007 U CN207890007 U CN 207890007U
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- plate
- catapult
- aircraft
- launching
- mounting plate
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Abstract
The utility model discloses a kind of aircraft catapult launching apparatus,Including the first catapult-launching gear,Second catapult-launching gear,The body of rod,Pedestal,First electromagnet and universal wheel,Fixation of the placement plate in mounting plate over top position is realized by the way that the first catapult-launching gear and the second catapult-launching gear is arranged,The body of rod is adjusted to stretch in cylinder,To drive mounting plate to be rotated along with the hinged one end of support plate,To realize the adjusting to mounting plate angle of inclination,The needs of when to meet in varied situations to aircraft progress catapult-assisted take-off to different take-off angles,Improve the practicability of equipment,By the way that the first electromagnet is arranged for being adsorbed to carry-on magnetic areas,To realize fixation of the aircraft in placement plate top position,It is fixed conveniently,It is used to move convenient for users to pushing equipment by the way that universal wheel is arranged,Improve the portability of equipment.
Description
Technical field
The utility model is related to a kind of catapult launcher, specifically a kind of aircraft catapult launching apparatus.
Background technology
Fixed wing aircraft (Fixed-wing plane) is referred to as aircraft (English：Plane), refer to being generated by power plant
The thrust or pulling force of advance generate lift, in the aircraft for overweighting air of endoatmosphere flight by the fixation wing of fuselage.It
It is one kind and the most common type of Fixed-Wing, another Fixed-Wing is aerodone.Aircraft makes according to it
Engine type can be divided into jet airplane and propeller aeroplane again；
Aircraft catapult launching apparatus is mainly used for carrying out auxiliary of taking off to fixed wing aircraft, and existing catapult-launching gear is not
Take-off angle different when carrying out catapult-assisted take-off to aircraft in varied situations and height requirement of taking off can be met, while existing
The movement of aircraft catapult launching apparatus it is inconvenient, portability is poor, while existing aircraft catapult launching apparatus is to flight
It is inconvenient that device is fixed, therefore using very inconvenient, so being badly in need of a kind of aircraft catapult launching apparatus to solve the problems, such as this.
Utility model content
The purpose of this utility model is to provide a kind of aircraft catapult launching apparatus, to solve to carry in above-mentioned background technology
The problem of going out.
To achieve the above object, the utility model provides the following technical solutions：
A kind of aircraft catapult launching apparatus, including launching apparatus, hydraulic stem, hydraulic cylinder and pedestal, the base top
It is installed with hydraulic cylinder, cylinder hydraulic connects hydraulic stem, and the hydraulic rod top is provided with launching apparatus, the dress that takes off
It sets including the first catapult-launching gear, support plate, bottom plate, placement plate, the first electromagnet, fixed plate, angle regulator and the second bullet
Injection device, the bottom plate are fixedly mounted on hydraulic rod top, and one end is installed with support plate, the bottom plate top at the top of bottom plate
Top is provided with mounting plate, and the side of the mounting plate is hinged by shaft and support plate top, the mounting plate over top
It is provided with placement plate, placement plate both sides are symmetrically arranged with the first catapult-launching gear and the second catapult-launching gear, first catapult-launching gear
Including sliding block, return spring, the first limiting plate, mounting plate, sliding bar, the second limiting plate, the second electromagnet and installation groove, institute
It states and is symmetrically installed with the first limiting plate and the second limiting plate at the top of mounting plate, mounting plate over top is located at the first limiting plate and the
It is provided with sliding bar on position between two limiting plates, the both ends of sliding bar are respectively and fixedly installed on the inside of the first limiting plate and the
It is slided on the inside of two limiting plates, on the sliding bar and is provided with sliding block, return spring, institute are provided between sliding block and the second limiting plate
It states return spring to be set on the outside of sliding bar, the sliding block is fixedly mounted on placement plate side, close to the at the top of the mounting plate
Installation groove is offered on the position of two limiting plates, the installation groove inside bottom is installed with the second electromagnet, described
One end at the top of placement plate close to the second limiting plate is installed with fixed plate, and fixed plate side corresponding with the first limiting plate is fixed
First electromagnet is installed, one end far from support plate is provided with angle regulator at the top of the bottom plate.
As further program of the utility model：The structure of first catapult-launching gear and the second catapult-launching gear is identical.
As the utility model further scheme：The sliding block is iron material matter.
As the utility model further scheme：The angle regulator includes cylinder, the body of rod and rotation seat, institute
It states cylinder to be fixedly mounted at the top of bottom plate, is slided in cylinder and be provided with the body of rod, offered on cylinder for being connect with bolt thread
Tapped through hole, the rotation seat is fixedly mounted on the one end of mounting plate bottom far from support plate, and the top of the body of rod passes through
Shaft is rotatably installed on rotation seat.
As the utility model further scheme：The base bottom is symmetrically installed with universal wheel.
Compared with prior art, the utility model has the beneficial effects that：By the way that the first catapult-launching gear and the second ejection is arranged
Device realizes fixation of the placement plate in mounting plate over top position, adjusts the body of rod and stretches in cylinder, to drive installation
Plate is rotated along with the hinged one end of support plate, to realize the adjusting to mounting plate angle of inclination, is not being sympathized with to meet
Demand to different take-off angles when carrying out catapult-assisted take-off to aircraft under condition, improves the practicability of equipment, passes through setting the
One electromagnet is for adsorbing carry-on magnetic areas, to realize aircraft consolidating in placement plate top position
It is fixed, it is fixed conveniently, when carrying out catapult-assisted take-off, the electric current on the second electromagnet is broken first, to make sliding block in return spring bullet
It is fast moved towards the direction of the first limiting plate on sliding bar under the action of power, to be further driven to the flight at the top of placement plate
Device is moved towards the direction of the first limiting plate, when sliding block, which is moved to, to be contacted with the first limiting plate, rapidly on broken first electromagnet
Electric current, to make aircraft fly out at the top of the placement plate under the action of inertia, to be furthermore achieved to aircraft into
The purpose of row catapult-assisted take-off, it is easy to operate, it is flexible to realize the adjusting to bottom plate heights by Driven by Hydraulic Cylinder hydraulic stem,
To which the adjusting to placement plate height be furthermore achieved, when carrying out catapult-assisted take-off to aircraft in varied situations to meet
The demand for height of taking off to difference, improves the practicability of equipment, is used for convenient for users to pushing equipment by the way that universal wheel is arranged
It is mobile, improve the portability of equipment.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of aircraft catapult launching apparatus.
Fig. 2 is a kind of structural schematic diagram of catapult-launching gear in aircraft catapult launching apparatus.
Fig. 3 is a kind of vertical view of catapult-launching gear in aircraft catapult launching apparatus.
As shown in the figure：Launching apparatus 1, hydraulic stem 2, hydraulic cylinder 3, pedestal 4, universal wheel 5, sliding block 6, return spring 7, first
Catapult-launching gear 8, support plate 9, installation groove 10, bottom plate 11, angle regulator 12, cylinder 13, the body of rod 14, rotation seat 15,
One limiting plate 16, mounting plate 17, sliding bar 18, placement plate 19, the first electromagnet 20, fixed plate 21, the second electromagnet 22, second
Catapult-launching gear 23, the second limiting plate 24.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
Please refer to Fig.1~3, in the utility model embodiment, a kind of aircraft catapult launching apparatus, including launching apparatus 1,
Hydraulic stem 2, hydraulic cylinder 3, pedestal 4 and universal wheel 5,4 top of the pedestal are installed with hydraulic cylinder 3,3 hydraulic connecting of hydraulic cylinder
Hydraulic stem 2,2 top of the hydraulic stem are provided with launching apparatus 1, and the launching apparatus 1 includes the first catapult-launching gear 8, support plate
9, bottom plate 11, placement plate 19, the first electromagnet 20, fixed plate 21, angle regulator 12 and the second catapult-launching gear 23, the bottom
Plate 11 is fixedly mounted on 2 top of hydraulic stem, and 11 top one end of bottom plate is installed with support plate 9,11 over top of the bottom plate
It is provided with mounting plate 17, the side of the mounting plate 17 is hinged by shaft and 9 top of support plate, on 17 top of the mounting plate
Side is provided with placement plate 19, and 19 both sides of placement plate are symmetrically arranged with the first catapult-launching gear 8 and the second catapult-launching gear 23, and described first
Catapult-launching gear 8 includes sliding block 6, return spring 7, the first limiting plate 16, mounting plate 17, sliding bar 18, the second limiting plate 24, second
Electromagnet 22 and installation groove 10,17 top of the mounting plate are symmetrically installed with the first limiting plate 16 and the second limiting plate 24, pacify
17 over top of loading board is provided with sliding bar 18, sliding bar on the position between the first limiting plate 16 and the second limiting plate 24
18 both ends are respectively and fixedly installed to 24 inside of 16 inside of the first limiting plate and the second limiting plate, slide and set on the sliding bar 18
It is equipped with sliding block 6, the sliding block 6 is iron material matter, and return spring 7, the return bullet are provided between sliding block 6 and the second limiting plate 24
Spring 7 is set in the outside of sliding bar 18, and the sliding block 6 is fixedly mounted on 19 side of placement plate, and 17 top of the mounting plate is close to the
Installation groove 10 is offered on the position of two limiting plates 24,10 inside bottom of the installation groove is installed with the second electromagnet
22；
First catapult-launching gear 8 is identical with the structure of the second catapult-launching gear 23, by the way that the first catapult-launching gear 8 and the is arranged
Two catapult-launching gears 23 realize fixation of the placement plate 19 in 17 over top position of mounting plate, and 19 top of the placement plate is close to the
One end of two limiting plates 24 is installed with fixed plate 21, and the side corresponding with the first limiting plate 16 of fixed plate 21 is installed with
One electromagnet 20,11 one end of top far from support plate 9 of the bottom plate are provided with angle regulator 12, the angular adjustment dress
It includes cylinder 13, the body of rod 14 and rotation seat 15 to set 12, and the cylinder 13 is fixedly mounted on 11 top of bottom plate, slides and set in cylinder 13
It is equipped with the body of rod 14, the tapped through hole for being connect with bolt thread is offered on cylinder 13, by bolt in tapped through hole inward turning
Turn to squeeze fixed core 14, to realize the control to 14 position of the body of rod, the rotation seat 15 is fixedly mounted on mounting plate 17
The top of the one end of bottom far from support plate 9, the body of rod 14 is rotatably installed in by shaft on rotation seat 15, and the body of rod 14 is adjusted
It stretches in cylinder 13, to drive mounting plate 17 to be rotated along with the hinged one end of support plate 9, to realize to mounting plate 17
The adjusting at angle of inclination, to the need of different take-off angles when to meet in varied situations to aircraft progress catapult-assisted take-off
It asks, improves the practicability of equipment, when needing to carry out catapult-assisted take-off to aircraft, push sliding block 6 on sliding bar 18 first
Direction towards the second limiting plate 24 is mobile and squeezes return spring 7, further the second electromagnet 22 is given to be powered, works as sliding block
6 when being moved to the second 22 top of electromagnet, the second electromagnet 22 and then is adsorbed to sliding block 6, to realize to sliding block 6
Aircraft is further placed on 19 top of placement plate, and further the first electromagnet 20 is given to be powered by the fixation set, and passes through setting
First electromagnet 20 is for adsorbing carry-on magnetic areas, to realize aircraft in 19 top position of placement plate
The fixation set when carrying out catapult-assisted take-off, breaks the electric current on the second electromagnet 22, to make sliding block 6 in 7 bullet of return spring first
It is fast moved towards the direction of the first limiting plate 16 on sliding bar 18 under the action of power, to be further driven to 19 top of placement plate
Aircraft moved towards the direction of the first limiting plate 16, when sliding block 6, which is moved to, to be contacted with the first limiting plate 16, break the rapidly
Electric current on one electromagnet 20, to make aircraft fly out under the action of inertia from 19 top of placement plate, to further real
Show the purpose that catapult-assisted take-off is carried out to aircraft, it is easy to operate, drive hydraulic stem 2 flexible to realize by hydraulic cylinder 3
Adjusting to 11 height of bottom plate, to which the adjusting to 19 height of placement plate be furthermore achieved, to meet in varied situations
The demand for height of taking off to difference when carrying out catapult-assisted take-off to aircraft, improves the practicability of equipment, 4 bottom pair of the pedestal
Title is equipped with universal wheel 5, is used to move convenient for users to pushing equipment by the way that universal wheel 5 is arranged, improves the portability of equipment.
The operation principle of the utility model is：It realizes and puts by the way that the first catapult-launching gear 8 and the second catapult-launching gear 23 is arranged
Fixation of the plate 19 in 17 over top position of mounting plate is set, the body of rod 14 is adjusted and stretches in cylinder 13, to drive mounting plate 17
It rotates along with the hinged one end of support plate 9, to realize the adjusting to 17 angle of inclination of mounting plate, is not sympathizing with to meet
Demand when under condition to aircraft progress catapult-assisted take-off to different take-off angles, improves the practicability of equipment, when needs are to flying
When row device carries out catapult-assisted take-off, push sliding block 6 mobile towards the direction of the second limiting plate 24 on sliding bar 18 first and to return
Spring 7 is squeezed, and further the second electromagnet 22 is given to be powered, when sliding block 6 is moved to the second 22 top of electromagnet, the second electricity
Magnet 22 in turn adsorbs sliding block 6, to realize the fixation to 6 position of sliding block, is further placed on aircraft
19 top of plate is set, and further the first electromagnet 20 is given to be powered, is used for carry-on magnetic by the way that the first electromagnet 20 is arranged
Property position adsorbed, to realize fixation of the aircraft in 19 top position of placement plate, be fixed conveniently, carry out catapult-assisted take-off
When, the electric current on the second electromagnet 22 is broken first, to make sliding block 6 under the action of 7 elastic force of return spring in sliding bar 18
On fast moved towards the direction of the first limiting plate 16, to be further driven to the aircraft at the top of placement plate 19 towards the first limiting plate
16 direction movement, when sliding block 6, which is moved to, to be contacted with the first limiting plate 16, the electric current on rapid broken first electromagnet 20,
To make aircraft fly out under the action of inertia from 19 top of placement plate, aircraft is launched to be furthermore achieved
The purpose taken off, it is easy to operate, drive hydraulic stem 2 flexible to realize the adjusting to 11 height of bottom plate by hydraulic cylinder 3, from
And the adjusting to 19 height of placement plate is furthermore achieved, when carrying out catapult-assisted take-off to aircraft in varied situations to meet
The demand for height of taking off to difference, improves the practicability of equipment, is used for convenient for users to pushing equipment by the way that universal wheel 5 is arranged
It is mobile, improve the portability of equipment.
Although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art is come
Say, still can with technical scheme described in the above embodiments is modified, or to which part technical characteristic into
Row equivalent replacement, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on should all
It is included within the scope of protection of this utility model.
Claims (5)
1. a kind of aircraft catapult launching apparatus, including launching apparatus (1), hydraulic stem (2), hydraulic cylinder (3) and pedestal (4),
It is characterized in that, hydraulic cylinder (3), hydraulic cylinder (3) hydraulic connecting hydraulic stem (2), the liquid is installed at the top of the pedestal (4)
Launching apparatus (1) is provided at the top of compression bar (2), the launching apparatus (1) includes the first catapult-launching gear (8), support plate (9), bottom
Plate (11), placement plate (19), the first electromagnet (20), fixed plate (21), angle regulator (12) and the second catapult-launching gear
(23), the bottom plate (11) is fixedly mounted at the top of hydraulic stem (2), and one end is installed with support plate (9) at the top of bottom plate (11),
Bottom plate (11) over top is provided with mounting plate (17), and the side of the mounting plate (17) passes through shaft and support plate (9)
Top is hinged, and mounting plate (17) over top is provided with placement plate (19), and placement plate (19) both sides are symmetrically arranged with first
Catapult-launching gear (8) and the second catapult-launching gear (23), first catapult-launching gear (8) include sliding block (6), return spring (7), first
Limiting plate (16), mounting plate (17), sliding bar (18), the second limiting plate (24), the second electromagnet (22) and installation groove (10),
It is symmetrically installed with the first limiting plate (16) and the second limiting plate (24), mounting plate (17) over top at the top of the mounting plate (17)
It is provided with sliding bar (18) on position between the first limiting plate (16) and the second limiting plate (24), the two of sliding bar (18)
End is respectively and fixedly installed on the inside of the first limiting plate (16) and on the inside of the second limiting plate (24), slide and set on the sliding bar (18)
It is equipped with sliding block (6), return spring (7) is provided between sliding block (6) and the second limiting plate (24), the return spring (7) is arranged
On the outside of the sliding bar (18), the sliding block (6) is fixedly mounted on placement plate (19) side, close to the at the top of the mounting plate (17)
Installation groove (10) is offered on the position of two limiting plates (24), installation groove (10) inside bottom is installed with second
Electromagnet (22), placement plate (19) top are installed with fixed plate (21) close to one end of the second limiting plate (24), Gu
Fixed board (21) side corresponding with the first limiting plate (16) is installed with the first electromagnet (20), and bottom plate (11) top is separate
One end of support plate (9) is provided with angle regulator (12).
2. a kind of aircraft catapult launching apparatus according to claim 1, which is characterized in that first catapult-launching gear
(8) identical with the structure of the second catapult-launching gear (23).
3. a kind of aircraft catapult launching apparatus according to claim 1, which is characterized in that the sliding block (6) is iron material
Matter.
4. a kind of aircraft catapult launching apparatus according to claim 1, which is characterized in that the angle regulator
(12) include cylinder (13), the body of rod (14) and rotation seat (15), the cylinder (13) is fixedly mounted at the top of bottom plate (11), cylinder
(13) sliding is provided with the body of rod (14) in, offers the tapped through hole for being connect with bolt thread on cylinder (13), described turn
Dynamic seat (15) is fixedly mounted on the one end of mounting plate (17) bottom far from support plate (9), and the top of the body of rod (14) is by turning
Axis is rotatably installed on rotation seat (15).
5. a kind of aircraft catapult launching apparatus according to claim 1, which is characterized in that pedestal (4) bottom pair
Title is equipped with universal wheel (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820178928.2U CN207890007U (en) | 2018-02-01 | 2018-02-01 | A kind of aircraft catapult launching apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820178928.2U CN207890007U (en) | 2018-02-01 | 2018-02-01 | A kind of aircraft catapult launching apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207890007U true CN207890007U (en) | 2018-09-21 |
Family
ID=63543543
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820178928.2U Expired - Fee Related CN207890007U (en) | 2018-02-01 | 2018-02-01 | A kind of aircraft catapult launching apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207890007U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229414A (en) * | 2018-10-17 | 2019-01-18 | 中卫航空科技发展有限公司 | A kind of small miniature drone operation emitter |
| CN111924123A (en) * | 2020-06-24 | 2020-11-13 | 耿新利 | Agricultural thing networking fixed wing unmanned aerial vehicle jettison device |
| CN114180108A (en) * | 2021-11-29 | 2022-03-15 | 中国航天科工集团八五一一研究所 | Air spring-based casting and separating device |
-
2018
- 2018-02-01 CN CN201820178928.2U patent/CN207890007U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229414A (en) * | 2018-10-17 | 2019-01-18 | 中卫航空科技发展有限公司 | A kind of small miniature drone operation emitter |
| CN111924123A (en) * | 2020-06-24 | 2020-11-13 | 耿新利 | Agricultural thing networking fixed wing unmanned aerial vehicle jettison device |
| CN111924123B (en) * | 2020-06-24 | 2022-05-03 | 耿新利 | Agricultural thing networking fixed wing unmanned aerial vehicle jettison device |
| CN114180108A (en) * | 2021-11-29 | 2022-03-15 | 中国航天科工集团八五一一研究所 | Air spring-based casting and separating device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180921 Termination date: 20190201 |