CN209700948U - Sliding type multifunctional all-purpose suspended device - Google Patents
Sliding type multifunctional all-purpose suspended device Download PDFInfo
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- CN209700948U CN209700948U CN201822014894.6U CN201822014894U CN209700948U CN 209700948 U CN209700948 U CN 209700948U CN 201822014894 U CN201822014894 U CN 201822014894U CN 209700948 U CN209700948 U CN 209700948U
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- leading portion
- suspension
- back segment
- segment
- trailer
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Abstract
This application provides a kind of sliding type multifunctional all-purpose suspended devices, belong to airborne external hanging device design field, it includes the suspension leading portion of hollow structure, hang middle section and suspension back segment, the top for hanging middle section has the upper interface of plurality of specifications to be adapted to different aircraft platforms, hang the hanger that the lower part in middle section has a plurality of types of lower interfaces different with carry, suspension leading portion and suspension back segment are fixedly installed on the rear and front end in suspension middle section, wherein, hanging leading portion includes leading portion front, leading portion middle part and preceding segment trailer, leading portion front is for installing satellite signal receiving equipment and/or wireless antenna, for accommodating inertial navigation equipment in the middle part of leading portion, it is fixedly connected in the middle part of leading portion front and leading portion, it is slidably connected in the middle part of leading portion with preceding segment trailer.The application can be adapted to the different different types of hangers of aircraft platform and carry, and by using the mode being slidably connected two components for accommodating inertial navigation equipment are connected, and can quickly safeguard to inertial navigation equipment.
Description
Technical field
The application belongs to airborne external hanging device design field, in particular to a kind of sliding type multifunctional all-purpose suspended device.
Background technique
Suspension arrangement usually only designs one group of mechanical electric interface both at home and abroad at present, is exclusively used in the force with same-interface
Device/hanger, while each suspension arrangement has a single function, Universal and scalability is unable to satisfy many types of aircraft platform, different extensions
The suspension use demand of point and multiple types weapon.
And when suspension arrangement is hollow, inside can be used to accommodate equipment, but how can generate quickly to inside
The problem of equipment is safeguarded.
Summary of the invention
The purpose of the application is any of the above-described to solve the problems, such as there is provided a kind of sliding type multifunctional all-purpose suspended device.
The technical solution of the application is: a kind of sliding type multifunctional all-purpose suspended device comprising the suspension of hollow structure
The top of leading portion, suspension middle section and suspension back segment, the suspension middle section has the upper interface of plurality of specifications to be adapted to difference
Aircraft platform hanging point, it is described suspension middle section lower part have a plurality of types of lower interfaces with the suspension of carry different interface type
Object, the suspension leading portion and suspension back segment are fixedly installed on the rear and front end in the suspension middle section, wherein the suspension leading portion packet
Leading portion front, leading portion middle part and preceding segment trailer are included, the leading portion front is for installing satellite signal receiving equipment and/or wireless day
Line is fixedly connected in the middle part of the leading portion front and leading portion for accommodating inertial navigation equipment in the middle part of the leading portion, in the middle part of the leading portion and
The preceding segment trailer is slidably connected.
In embodiment itself, there is sliding rail in the middle part of the leading portion, the preceding segment trailer has sliding slot, the sliding rail
Cooperate with the sliding slot and is slidably connected with realizing.
In embodiment itself, the sliding slot is dovetail groove.
In embodiment itself, the width of the width of the suspension leading portion and the suspension back segment is all larger than described outstanding
Hang the width in middle section.
In embodiment itself, the interior positioning datum being equipped with for installing the inertial navigation equipment in the middle part of the leading portion
Face, the positioning reference plane are used to guarantee the operating accuracy of the inertial navigation equipment.
In embodiment itself, the suspension back segment includes back segment front and rear segment trailer, back segment front with it is described
Segment trailer is sequentially connected afterwards, and the back segment front is for accommodating Fire control calculation equipment and/or power-supply device, wherein the back segment
Lid is for safeguarding the Fire control calculation equipment and/or power-supply device after front side is equipped with back segment.
In embodiment itself, the tail end of the back segment front is equipped with groove, and the leading portion of the rear segment trailer is equipped with
Quick-detachable lock, the groove and the quick-detachable lock are coupled to be connected for realizing the back segment front and the fixed of rear segment trailer
It connects.
In embodiment itself, it is described after segment trailer along course direction include back segment upper side and back segment downside,
The back segment upper side and back segment downside are symmetrical above and below.
In embodiment itself, the rear segment trailer further includes back segment arc surface, and back segment arc surface is round and smooth excessively to be connected
Back segment upper side and back segment downside are connect, forms sinuous flow for preventing or mitigating suspension arrangement tail portion.
It is different that there is the multifunctional universal suspension arrangement of the application the upper interface of composite general can be adapted on the whole
Aircraft platform hanging point and with a plurality of types of lower interfaces constitute hanging point with the hanger of carry different interface type, and
It realizes with special streamlined structure to satellite signal receiving equipment, wireless antenna, inertial navigation equipment, Fire control calculation equipment, electricity
The installation of source device etc. and integrated, general structure platform is provided for external fire control system, is that a kind of collection hangs
It hangs, delivery, launch the suspension arrangement that function and antenna/power supply/control management equipment installation function etc. are integrated, greatly improve dress
The availability and expansion set.It is designed by the end to suspension front end, resistance of the suspension arrangement in flight is greatly decreased
Power.
Detailed description of the invention
In order to illustrate more clearly of technical solution provided by the present application, attached drawing will be briefly described below.It is aobvious and easy
Insight, drawings discussed below are only some embodiments of the present application.
Fig. 1 is the sliding type multifunctional all-purpose suspended apparatus structure schematic diagram of one embodiment of the application.
Fig. 2 is the suspension front segment structure schematic diagram of one embodiment of the application.
Leading portion middle part and preceding segment trailer slide construction schematic diagram of the Fig. 3 for one embodiment of the application.
Fig. 4 is the suspension rear section structure schematic diagram of one embodiment of the application.
Appended drawing reference:
10- hangs leading portion, 11- leading portion front, in the middle part of 12- leading portion, segment trailer before 13-, and 14- inertial navigation equipment, 15- satellite letter
Number receiving device, 16- wireless antenna, 111- leading portion front flap, hatch door in the middle part of 121-, 1121- front left face, the front 1122-
Right side, 1123- diversion trench, 122- sliding rail, the tail portion 131- interface, 132- sliding slot；
20- hangs middle section, interface front on 211- first, interface rear portion on 212- first, interface front on 221- second,
Interface rear portion on 222- second, interface front in 231- third, interface rear portion in 232- third, 241- lower interface front, 242-
Lower interface rear portion supports forearm on 251-, postbrachium, 26- bomb shackle is supported on 252-；
30- hangs back segment, 31- back segment front, segment trailer after 32-, 311- Fire control calculation equipment, 312- power-supply device,
313- card slot, 314- pivot pin, lid after 315- back segment, 321- quick-detachable lock, the tail portion 3221- upper side, the tail portion 3222- downside,
The tail portion 3223- arc surface.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application implementation clearer, below in conjunction in the embodiment of the present application
Attached drawing, technical solutions in the embodiments of the present application is further described in more detail.
In the description of the present application, term " center ", " longitudinal direction ", " transverse direction ", "front", "rear", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "top", "bottom", "inner", "outside" is that orientation based on the figure or position are closed
System is merely for convenience of description the application and simplifies description, rather than the device or element of indication or suggestion meaning must have
Specific orientation is constructed and operated in a specific orientation, therefore should not be understood as the limitation to the application protection scope.
In order to solve in the prior art, it is flat that the suspension arrangement of the single model hanger of carry can only adapt to single aircraft
Platform not only allows to also greatly drop with versatility present applicant proposes a kind of sliding type multifunctional all-purpose suspended device
The low windage of suspension arrangement in use.
As shown in Figures 1 to 4, the sliding type multifunctional all-purpose suspended device of the application includes the suspension leading portion of hollow structure
10, middle section 20 and suspension back segment 30 are hung, the top in suspension middle section 20 has the upper interface of plurality of specifications to be adapted to different fly
Machine platform hanging point, the lower part in suspension middle section 20 have a plurality of types of lower interfaces with the hanger of carry different interface type, hang
Extension leading portion 10 and suspension back segment 30 are fixedly installed on the rear and front end in suspension middle section 20, wherein suspension leading portion 10 is including before leading portion
Portion 11, leading portion middle part 12 and preceding segment trailer 13, leading portion front 11 is for installing satellite signal receiving equipment 15 and/or wireless day
Line 16,12 for accommodating inertial navigation equipment 14 in the middle part of leading portion, and leading portion front 11 is fixedly connected in the middle part of leading portion 12, in the middle part of leading portion 12 and
Preceding segment trailer 13 is slidably connected.
It is illustrated in figure 3 the schematic diagram that is slidably connected of an embodiment, 12 are equipped with sliding rail 122, preceding segment trailer 13 in the middle part of leading portion
Equipped with sliding slot 132, when sliding rail 122 and sliding slot 132 are used cooperatively, leading portion middle part 12 may be implemented and the sliding of preceding segment trailer 13 connects
It connects.12 connect with the slidingtype of preceding segment trailer 13 in the middle part of leading portion, convenient, quickly can set to the inertial navigation inside in the middle part of leading portion 12
Standby 14 are safeguarded, can be by preceding segment trailer 13 along the reversed pull-out of course H when installing or safeguarding.
It should be noted that in the above-described embodiments, removing and sliding rail 122 being arranged on 12 in the middle part of leading portion and in preceding segment trailer 13
Upper setting sliding slot 132, by the way of can also sliding slot be set in the middle part of leading portion 12 and sliding rail is set on preceding segment trailer 13.
In the embodiment of the present application, sliding slot 132 preferentially can while guaranteeing sliding stability using dovetail groove type
To guarantee the accuracy for the inertial navigation equipment 14 being arranged on preceding segment trailer 13.
In the present embodiment, upper interface shares three types, respectively by connecing on interface front 211 and first on first
Interface on the first of 212 the first length specification constituted after mouthful, by interface rear portion on interface front 221 and second on second
Interface and by 232 structure of interface rear portion in interface front 231 in third and third on the second of 222 second of the length specification constituted
At the third length specification third on interface.
Interface is identical lifting lug type in interface and third on second, when in use, aircraft platform stretches out hook suspension
Interface on second, interface is sealed condition in third at this time, but when needing to adjust spacing, can be by the lifting lug of interface on second
(front and rear) is replaced to interface in third, and the closure of interface is replaced to interface on second in third, then is passed through
The hook that aircraft platform stretches out is matching, and the change of spacing can be completed.
Interface is slotting ear type on first, when in use, passing through the structures and first such as the convex sheet being arranged on aircraft platform
Mating, the i.e. fixation of completion fastening aircraft and suspension arrangement of upper interface.
For example, the extension of interface is away from can be 1150mm on first, the extension of interface is away from can be 762mm on second, in third
The extension of interface is away from that can be 355.6mm, by the way that different extensions is arranged away from suspension arrangement can be adapted to different aircraft platforms.
In addition, hanging the branch that the top in middle section 20 is also made of support forearm 251 and support postbrachium 252 in the application
Arm configuration, support arm structure, which can play, keeps suspension arrangement holding horizontal or the effect of reduction suspension arrangement vibration.
The lower interface of suspension arrangement in the application includes being made of lower interface front 241 and lower interface rear portion 242
Second lower interface of the first lower interface of the first specification and second of specification being made of the bomb shackle 260 of single-point type, two
The lower interface of person's different size can on the downside of suspension arrangement carry different size or length/weight hanger.
It should be noted that the upper interface and lower interface in the application are multiple types or specification, and in embodiment
Three kinds of specifications schematically only are given to upper interface and two kinds of specifications are given to lower interface, so it is a variety of in the application
Refer to no less than two kinds.
In one embodiment of the application, the width of the width and suspension back segment 30 that hang leading portion 10 is all larger than suspension middle section 20
Width.Suspension leading portion 10 and the inside for hanging back segment 30 are used to accommodate some electrical equipments or electronic equipment, hang middle section 20
It then realizes function pipeline, realize suspension leading portion 10 and hangs the route connection of the electrical equipment or electronic equipment between back segment 30,
Therefore, the shape for hanging leading portion 10 and suspension back segment 30 need to be larger compared to suspension middle section 20.
Further, since suspension arrangement has windage in aircraft flight, the width and suspension back segment of leading portion 10 are hung
The width that 30 width is all larger than suspension middle section 20 can also effectively reduce windage.
It should be noted that width described in the present embodiment can for exhibition Xiang Kuandu, or pitching to width, or
The combination of both persons.
In one embodiment of the application, the side of leading portion front 11 is additionally provided with leading portion front flap 111, for safeguarding that satellite is believed
12 side is also additionally provided with middle section front flap 121 for safeguarding in the middle part of number receiving device 15 and/or wireless antenna 16 and leading portion
Inertial navigation equipment 14.
In the present embodiment, satellite signal receiving equipment 15 and wireless antenna 16 be installed on the upside of leading portion front 11 with
The problems such as preventing it to be set to bring signal shielding in suspension arrangement.Leading portion front flap is equipped in the side of leading portion front 11
111, although satellite signal receiving equipment 15 and wireless antenna 16 are installed on the upside of leading portion front 11, its line related is then
It is placed in the space of leading portion front 11, satellite signal receiving equipment 15 can easily be safeguarded by the leading portion front flap 111 opened up
And/or the route of wireless antenna 16.
In one embodiment of the application, since inertial navigation equipment 14 needs precisely to guide, in order to improve the system of inertial navigation equipment 14
Lead accuracy, 12 in the middle part of the leading portion in be provided with multiple positioning reference planes, inertial navigation equipment 14 is installed with positioning reference plane, is thus come
Guarantee the operating accuracy of inertial navigation equipment 14.
In one embodiment of the application, suspension back segment 30 include back segment front 31 and rear segment trailer 32, back segment front 31 with
Segment trailer 32 is sequentially connected afterwards, and back segment front 31 is for accommodating Fire control calculation equipment 311 and/or power-supply device 312, wherein after
Lid 315 is for safeguarding Fire control calculation equipment 311 and/or power-supply device 312 after section 31 side of front is equipped with back segment.
In the present embodiment, power-supply device 312 can be fixed by pin shaft 314 and back segment front 31, Fire control calculation equipment
311 can complete to fix by power-supply device 312 to its extruding, using bonding or can also be fixed on back segment by connector
On front 31.
The lid 315 after the side of back segment front 31 is equipped with back segment, safeguards back segment front 31 by lid 315 after back segment
Interior Fire control calculation equipment 311 or power-supply device 312.
In one embodiment of the application, the tail end of back segment front 31 is equipped with groove 313, and the leading portion of rear segment trailer 32 is equipped with
The quick-detachable lock 321 of protrusion, groove 313 and quick-detachable lock 321 are coupled consolidating for realizing back segment front 31 and rear segment trailer 32
Fixed connection.When needing that power-supply device 312 is installed or safeguarded, by being rapidly separated for groove 313 and quick-detachable lock 321,
It realizes that back segment front 31 and dividing for rear segment trailer 32 are come, and then power-supply device 312 can be safeguarded, it is convenient and efficient.
In an embodiment of the present invention, rear segment trailer 32 includes on the downside of back segment upper side 3221 and back segment along the course direction H
Face 3222, the setting symmetrical above and below of back segment upper side 3221 and back segment downside 3222 form wake structure, and wake structure is used for can
So that the wake flow for flowing through suspension arrangement not will form sinuous flow and negative pressure etc. in tail portion, the stability of suspension arrangement is improved.
In addition, in an embodiment of the present invention, rear segment trailer 32 further includes back segment arc surface 3223, back segment arc surface 3223
It is round and smooth to be excessively connected to back segment upper side 3221 and back segment downside 3222, suspension arrangement tail portion can be prevented or mitigated and form unrest
Stream.
It is different that there is the multifunctional universal suspension arrangement of the application the upper interface of composite general can be adapted on the whole
Aircraft platform and with a plurality of types of lower interfaces constitute hanging point with the different types of hanger of carry, and have it is special
Streamlined structure is realized to satellite signal receiving equipment, wireless antenna, inertial navigation equipment, Fire control calculation equipment, power-supply device etc.
Installation and integrated, general structure platform is provided for external fire control system, be a kind of collection hang, deliver,
The suspension arrangement that function and antenna/power supply/control management equipment installation function etc. are integrated is launched, the available of device is greatly improved
Property and expansion.By can be convenient, efficiently safeguarding leading portion to being connected between preceding segment trailer using slidingtype in the middle part of leading portion
Inertial navigation equipment in middle part.
The above, the only specific embodiment of the application, but the protection scope of the application is not limited thereto, it is any
Within the technical scope of the present application, any changes or substitutions that can be easily thought of by those familiar with the art, all answers
Cover within the scope of protection of this application.Therefore, the protection scope of the application should be with the scope of protection of the claims
It is quasi-.
Claims (7)
1. a kind of sliding type multifunctional all-purpose suspended device, which is characterized in that the suspension arrangement includes the suspension of hollow structure
Leading portion (10), suspension middle section (20) and suspension back segment (30), it is described suspension middle section (20) top have plurality of specifications on connect
Mouthful to be adapted to different aircraft platform hanging points, the lower part of suspension middle section (20) have a plurality of types of lower interfaces with carry not
With the hanger of interface type, suspension leading portion (10) and suspension back segment (30) are fixedly installed on suspension middle section (20)
Rear and front end, wherein the suspension leading portion (10) includes leading portion front (11), leading portion middle part (12) and preceding segment trailer (13), institute
Leading portion front (11) are stated for installing satellite signal receiving equipment (15) and/or wireless antenna (16), in the middle part of the leading portion (12)
For accommodating inertial navigation equipment (14), the leading portion front (11) is fixedly connected with (12) in the middle part of leading portion, in the middle part of the leading portion (12)
It is slidably connected with the preceding segment trailer (13).
2. sliding type multifunctional all-purpose suspended device as described in claim 1, which is characterized in that (12) tool in the middle part of the leading portion
Have sliding rail (122), the preceding segment trailer (13) has sliding slot (132), the sliding rail (122) and the sliding slot (132) cooperate with
Realization is slidably connected.
3. sliding type multifunctional all-purpose suspended device as claimed in claim 2, which is characterized in that the sliding slot (132) is swallow
Stern notch.
4. sliding type multifunctional all-purpose suspended device as described in claim 1, which is characterized in that suspension leading portion (10)
Width and the width of suspension back segment (30) are all larger than the width of suspension middle section (20).
5. sliding type multifunctional all-purpose suspended device as described in claim 1, which is characterized in that in the middle part of the leading portion in (12)
Equipped with the positioning reference plane for installing the inertial navigation equipment (14), the positioning reference plane is for guaranteeing the inertial navigation equipment
(14) operating accuracy.
6. sliding type multifunctional all-purpose suspended device as described in claim 1, which is characterized in that suspension back segment (30) packet
Back segment front (31) and rear segment trailer (32) are included, back segment front (31) are sequentially connected with the rear segment trailer (32), the back segment
Front (31) is for accommodating Fire control calculation equipment (311) and/or power-supply device (312), wherein back segment front (31) side
Equipped with lid after back segment (315) for safeguarding the Fire control calculation equipment (311) and/or power-supply device (312).
7. sliding type multifunctional all-purpose suspended device as claimed in claim 6, which is characterized in that the back segment front (31)
Tail end is equipped with groove (313), it is described after the leading portion of segment trailer (32) be equipped with quick-detachable lock (321), the groove (313) and described fast
Unload lock (321) be coupled for realizing the back segment front (31) with it is described after segment trailer (32) be fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822014894.6U CN209700948U (en) | 2018-12-03 | 2018-12-03 | Sliding type multifunctional all-purpose suspended device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822014894.6U CN209700948U (en) | 2018-12-03 | 2018-12-03 | Sliding type multifunctional all-purpose suspended device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209700948U true CN209700948U (en) | 2019-11-29 |
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ID=68635767
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822014894.6U Active CN209700948U (en) | 2018-12-03 | 2018-12-03 | Sliding type multifunctional all-purpose suspended device |
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| Country | Link |
|---|---|
| CN (1) | CN209700948U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020114360A1 (en) * | 2018-12-03 | 2020-06-11 | 中航技进出口有限责任公司 | Multifunctional universal suspension device |
-
2018
- 2018-12-03 CN CN201822014894.6U patent/CN209700948U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020114360A1 (en) * | 2018-12-03 | 2020-06-11 | 中航技进出口有限责任公司 | Multifunctional universal suspension device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Shenyang Aircraft Design Institute Yangzhou Collaborative Innovation Research Institute Co.,Ltd. Assignor: AVIC SHENYANG AIRCRAFT DESIGN & Research Institute|CHINA NATIONAL AERO-TECHNOLOGY IMPORT & EXPORT Corp. Contract record no.: X2022990000101 Denomination of utility model: Sliding multifunctional universal suspension device Granted publication date: 20191129 License type: Common License Record date: 20220222 |
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| EE01 | Entry into force of recordation of patent licensing contract |