CN109720542A - A kind of mounting device of standard contained implement and the nonstandard track in military aircraft floor - Google Patents
A kind of mounting device of standard contained implement and the nonstandard track in military aircraft floor Download PDFInfo
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- CN109720542A CN109720542A CN201910075480.0A CN201910075480A CN109720542A CN 109720542 A CN109720542 A CN 109720542A CN 201910075480 A CN201910075480 A CN 201910075480A CN 109720542 A CN109720542 A CN 109720542A
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- China
- Prior art keywords
- column
- telescopic mast
- compression spring
- telescopic column
- base
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- 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.)
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- Pallets (AREA)
- Connection Of Plates (AREA)
Abstract
本发明公开了一种标准集装单元与军用飞机地板非标地轨的安装装置，包括基座、第一T型柱、第一伸缩柱、第二伸缩柱、端盖、拉环、转动轴、联动杆、第一压簧、第二压簧和第二T型柱，所述基座的一端与第一T型柱固定连接；所述基座的另一端与第二T型柱固定连接；所述基座的上设置有第一伸缩柱和第二伸缩柱；所述第一伸缩柱内部设置有第一压簧；所述第二伸缩柱内部设置有第二压簧；所述第一压簧和第二压簧的另一端连接有联动杆；所述联动杆的另一端连接有转动轴；所述转动轴的另一端连接有端盖。该发明的有益效果是操作比较方便，安装比较方便，有效提高飞机的货运能力，提升货盘的兼容性。
The invention discloses an installation device of a standard container unit and a non-standard ground rail of a military aircraft floor, comprising a base, a first T-shaped column, a first telescopic column, a second telescopic column, an end cover, a pull ring and a rotating shaft , linkage rod, first compression spring, second compression spring and second T-shaped column, one end of the base is fixedly connected with the first T-shaped column; the other end of the base is fixedly connected with the second T-shaped column a first telescopic column and a second telescopic column are arranged on the base; a first compression spring is arranged inside the first telescopic column; a second compression spring is arranged inside the second telescopic column; The other ends of the first compression spring and the second compression spring are connected with a linkage rod; the other end of the linkage rod is connected with a rotating shaft; the other end of the rotating shaft is connected with an end cover. The beneficial effects of the invention are that the operation is relatively convenient, the installation is relatively convenient, the cargo capacity of the aircraft is effectively improved, and the compatibility of the pallet is improved.
Description
Technical field
The present invention relates to aircraft shippings to load field, in particular to a kind of standard contained implement and military aircraft floor are nonstandard
The mounting device of track.
Background technique
Packaging is realized by the devices such as installing all kinds of restraints additional on the sliding rail of floor, being oriented to, be tethered at, transmit in airfreighter
The air transportion of unit.Currently, the civil aviation shipping contained implement through certification has formed standardisation requirements.To adapt to tray
Size, civil aviaton's airfreighter track are all made of the standard pitch of 25.4mm.And demand, pitch are military transport aircraft depending on the application
Nonstandard size.When these aircrafts load civil aviaton's contained implement, due to the difference of dimensional standard, it will lead to and be arranged in tray surrounding
Guiding restraint device configuration it is very more, be not easy to aircraft quick configuration conversion.Tray made in Great Britain is as the general packaging list of aviation
Member, it is larger using difficulty on the military aircraft of nonstandard size, reduce the utilization rate of tray.
According to standard pitch size and the nonstandard pitch size of military aircraft, a kind of coordination mounting device is formulated, is made minimum
Tray reasonable layout made in Great Britain, to effectively improve the freight-transport capacity of aircraft, is promoted into tray in metric system track under product configuration
Compatibility.
Summary of the invention
The present invention provides the mounting device of a kind of standard contained implement and the nonstandard track in military aircraft floor, can solve existing
Have in technology, installing and dismounting is inconvenient, inconvenient for operation, the problem of reducing the utilization rate of tray.
The present invention provides the mounting devices of a kind of standard contained implement and the nonstandard track in military aircraft floor, including base
Seat, the first T-type column, the first telescopic mast, the second telescopic mast, end cap, pull ring, rotation axis, interlocking bar, the first pressure spring, the second pressure spring
With the second T-type column, one end of the pedestal is fixedly connected with the first T-type column；The other end of the pedestal is fixed with the second T-type column
Connection；The first telescopic mast and the second telescopic mast are provided on the pedestal；First telescopic mast is internally provided with the first pressure
Spring；Second telescopic mast is internally provided with the second pressure spring；The other end of first pressure spring and the second pressure spring is connected with linkage
Bar；The other end of the interlocking bar is connected with rotation axis；The other end of the rotation axis is connected with end cap；It is arranged on the end cap
There is pull ring；First telescopic mast, the second telescopic mast, the first pressure spring, the second pressure spring, interlocking bar are fixed on pedestal by end cap
On.
Preferably, be provided on the end cap the first groove adaptable with the first telescopic mast and the second telescopic mast respectively and
Second groove.
Preferably, one end of the pedestal is fixedly connected by nut with the first T-type column.
Preferably, the other end of the pedestal is fixedly connected by nut with the second T-type column.
Preferably, to be provided with the third being adapted with interlocking bar recessed for first telescopic mast and the second flexible column bottom
Slot.
The mounting device of a kind of standard contained implement and the nonstandard track in military aircraft floor provided by the invention, is being installed
When, pull-up pull ring, pull ring drive universal driving shaft and interlocking bar to run up counterclockwise manually, and interlocking bar drives the first telescopic mast, the
Two telescopic masts move simultaneously, pull ring pull-up to upright position, and the first telescopic mast and the second telescopic mast are retracted into pedestal and pedestal
Ground is concordant.Due to being provided with the groove with interlocking bar cooperation in bottom in the first telescopic mast and the second telescopic mast, linking
When bar moves upwards, the first telescopic mast and the second telescopic mast can be driven to move simultaneously.When interlocking bar moves downward, will not cause
The movement of first telescopic mast and the second telescopic mast, two telescopic masts move downward under the action of therein pressure spring, by this
First T-type column of device and the second T-type column alignment aircraft track round hole (axis A), device is embedded in track, guarantees pedestal bottom
After face is bonded with floor, a quarter track pitch is translate forward.At this point, the first T-type column and the second T-type column have half
Cylinder and sliding rail cooperate, and realize that vertical restraint, the first telescopic mast are aligned (axis B) with track circular trough, the second telescopic mast and aircraft
Floor contact.Pull ring is rotated clockwise, universal driving shaft and interlocking bar move downward, it is disengaged with the first telescopic mast, the second telescopic mast, the
One telescopic mast extends downwardly under the action of the first pressure spring to the sliding rail circular trough of floor, and the second telescopic mast is limited by floor, protects
It staying in pedestal, the installation of first installation position of finishing device, operation is more convenient, similarly, when installing another installation position,
After in first T-type column and the second T-type column insertion track, translating device, makes the second telescopic mast alignment track circle in the opposite direction
Second telescopic mast is pushed into base track by shape slot by the second pressure spring, and the first telescopic mast is contacted with airplane floor, is retained in pedestal
It is interior.In device disassembly, operated according to opposite step, installing and dismounting is more convenient, is threaded with first on the base and stretches
Contracting column and the second telescopic mast, by adjusting the size between two telescopic masts, may be implemented civil standards contained implement with it is military
The coordination installation that isomorphism type equipment is installed in multiposition when aircraft nonstandard size matches, effectively improves the freight-transport capacity of aircraft, mentions
Rise the compatibility of tray.
Detailed description of the invention
Fig. 1 is a kind of mounting device structure of standard contained implement and the nonstandard track in military aircraft floor provided by the invention
Schematic diagram；
Fig. 2 is the preceding installation of the mounting device of a kind of standard contained implement provided by the invention and the nonstandard track in military aircraft floor
Side view；
Fig. 3 is the telescopic mast of the mounting device of a kind of standard contained implement provided by the invention and the nonstandard track in military aircraft floor
Retract side view；
Fig. 4 is the telescopic mast of the mounting device of a kind of standard contained implement provided by the invention and the nonstandard track in military aircraft floor
Retraction operation structure chart；
Fig. 5 is the telescopic mast of the mounting device of a kind of standard contained implement provided by the invention and the nonstandard track in military aircraft floor
With the fit structure schematic diagram of interlocking bar；
Fig. 6 is that the installation of a kind of standard contained implement provided by the invention and the mounting device of the nonstandard track in military aircraft floor is shown
It is intended to；
Before Fig. 7 is the device of the mounting device of a kind of standard contained implement provided by the invention and the nonstandard track in military aircraft floor
Move schematic diagram；
Fig. 8 is that the mounting device of a kind of standard contained implement provided by the invention and the nonstandard track in military aircraft floor puts down drawing
Ring structure schematic diagram；
Fig. 9 is that a kind of standard contained implement provided by the invention is stretched with the first of the mounting device of the nonstandard track in military aircraft floor
Contracting column is installed in place schematic diagram.
Description of symbols: 1- pedestal；2- the first T-type column；The first telescopic mast of 3-；The second telescopic mast of 4-；5- end cap；6- is drawn
Ring；7- rotation axis；8- interlocking bar；The first pressure spring of 9-；The second pressure spring of 10-；11- the second T-type column.
Specific embodiment
With reference to the accompanying drawing, the specific embodiment of the present invention is described in detail, it is to be understood that of the invention
Protection scope be not limited by the specific implementation.
As shown in Figures 1 to 9, a kind of standard contained implement provided in an embodiment of the present invention and military aircraft floor are nonstandard
The mounting device of rail, including pedestal 1, the first T-type column 2, the first telescopic mast 3, the second telescopic mast 4, end cap 5, pull ring 6, rotation axis
7, interlocking bar 8, the first pressure spring 9, the second pressure spring 10 and the second T-type column 11, one end of the pedestal 1 and the first T-type column 2 are fixed to be connected
It connects；The other end of the pedestal 1 is fixedly connected with the second T-type column 11；The first telescopic mast 3 and are provided on the pedestal 1
Two telescopic masts 4；First telescopic mast 3 is internally provided with the first pressure spring 9；Second telescopic mast 4 is internally provided with the second pressure
Spring 10；The other end of first pressure spring 9 and the second pressure spring 10 is connected with interlocking bar 8；The other end of the interlocking bar 8 is connected with
Rotation axis 7；The other end of the rotation axis 7 is connected with end cap 5；Pull ring 6 is provided on the end cap 5；First telescopic mast
3, the second telescopic mast 4, the first pressure spring 9, the second pressure spring 10, interlocking bar 8 are fixed on pedestal 1 by end cap 5.
Preferably, it is recessed to be provided with first be adapted respectively with the first telescopic mast 3 and the second telescopic mast 4 on the end cap 5
Slot and the second groove.
Preferably, one end of the pedestal 1 is fixedly connected by nut with the first T-type column 2.
Preferably, the other end of the pedestal 1 is fixedly connected by nut with the second T-type column 11.
Preferably, first telescopic mast 3 and 4 bottom of the second telescopic mast are provided with the third being adapted with interlocking bar 8
Groove.
Working principle: during installation, pull-up pull ring 6, pull ring 6 drive universal driving shaft 7 and interlocking bar 8 to transport upwards counterclockwise manually
Row, interlocking bar 8 drive the first telescopic mast 3, the second telescopic mast 4 to move simultaneously, 6 pull-up of pull ring to upright position, the first telescopic mast 3
It is retracted into the second telescopic mast 4 concordant with 1 ground of pedestal in pedestal 1.Due in the first telescopic mast 3 and the second telescopic mast 4 bottom of at
Portion is provided with the groove cooperated with interlocking bar 8 can drive the first telescopic mast 3 and second when interlocking bar moves upwards simultaneously
Telescopic mast 4 moves.When interlocking bar 8 moves downward, the movement of the first telescopic mast 3 and the second telescopic mast 4 will not be caused, two are stretched
Contracting column moves downward under the action of therein pressure spring, and the first T-type column 2 of the device and the second T-type column 11 are aligned and flown
Device is embedded in track 20 by 20 round hole (axis A) of machine track, after guaranteeing that 1 bottom surface of pedestal is bonded with floor, translates forward four points
One of track pitch.At this point, the first T-type column 2 and the second T-type column 11 have half cylinder and sliding rail to cooperate, realize vertical
Restraint, the first telescopic mast 3 are aligned (axis B) with track circular trough, and the second telescopic mast 4 is contacted with airplane floor.Rotate clockwise drawing
Ring 6, universal driving shaft 7 and interlocking bar 8 move downward, and disengage with the first telescopic mast 3, the second telescopic mast 4, the first telescopic mast 3 is first
Under the action of pressure spring 9, extending downwardly to the sliding rail circular trough of floor, the second telescopic mast 4 is limited by floor, it is retained in pedestal 1,
The installation of first installation position of finishing device, operation is more convenient, similarly, when installing another installation position, the first T-type column 2
After in the second T-type column 11 insertion track, translating device, makes the second telescopic mast 4 be directed at track circular trough in the opposite direction, by
Second telescopic mast 4 is pushed into base track by the second pressure spring 10, and the first telescopic mast 3 is contacted with airplane floor, is retained in pedestal 1.
It in device disassembly, is operated according to opposite step, installing and dismounting is more convenient, and it is flexible that first is threaded on pedestal 1
Column 3 and the second telescopic mast 4, by adjusting the size between two telescopic masts, may be implemented civil standards contained implement with it is military
The coordination installation that isomorphism type equipment is installed in multiposition when aircraft nonstandard size matches, effectively improves the freight-transport capacity of aircraft, mentions
Rise the compatibility of tray.
Disclosed above is only specific embodiments of the present invention, and still, the embodiment of the present invention is not limited to this, Ren Heben
What the technical staff in field can think variation should all fall into protection scope of the present invention.
Claims (5)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910075480.0A CN109720542B (en) | 2019-01-25 | 2019-01-25 | A device for installing a standard container unit and a non-standard ground rail on a military aircraft floor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910075480.0A CN109720542B (en) | 2019-01-25 | 2019-01-25 | A device for installing a standard container unit and a non-standard ground rail on a military aircraft floor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109720542A true CN109720542A (en) | 2019-05-07 |
| CN109720542B CN109720542B (en) | 2025-05-16 |
Family
ID=66301149
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910075480.0A Active CN109720542B (en) | 2019-01-25 | 2019-01-25 | A device for installing a standard container unit and a non-standard ground rail on a military aircraft floor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109720542B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0900727A2 (en) * | 1997-09-04 | 1999-03-10 | VS Guss AG | Sliding element with safety plate |
| US20050008443A1 (en) * | 2001-06-12 | 2005-01-13 | Berthold Eitzenberger | Method and device for positioning freight containers on a loading surface |
| US20110176903A1 (en) * | 2010-01-19 | 2011-07-21 | Goodrich Corporation | Method and apparatus for converting aircraft from commercial to military freight service |
| US20120119026A1 (en) * | 2009-06-22 | 2012-05-17 | Telair International Gmbh | Locking element |
| US20140367515A1 (en) * | 2013-06-17 | 2014-12-18 | Airbus Operations Gmbh | Cargo handling system |
| US20180022437A1 (en) * | 2007-10-17 | 2018-01-25 | 1281329 Alberta Ltd. | Aircraft based non-dedicated special mission pod mounting apparatus |
| CN209634712U (en) * | 2019-01-25 | 2019-11-15 | 西安飞豹科技有限公司 | A kind of mounting device of standard contained implement and the nonstandard track in military aircraft floor |
-
2019
- 2019-01-25 CN CN201910075480.0A patent/CN109720542B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0900727A2 (en) * | 1997-09-04 | 1999-03-10 | VS Guss AG | Sliding element with safety plate |
| US20050008443A1 (en) * | 2001-06-12 | 2005-01-13 | Berthold Eitzenberger | Method and device for positioning freight containers on a loading surface |
| US20180022437A1 (en) * | 2007-10-17 | 2018-01-25 | 1281329 Alberta Ltd. | Aircraft based non-dedicated special mission pod mounting apparatus |
| US20120119026A1 (en) * | 2009-06-22 | 2012-05-17 | Telair International Gmbh | Locking element |
| US20110176903A1 (en) * | 2010-01-19 | 2011-07-21 | Goodrich Corporation | Method and apparatus for converting aircraft from commercial to military freight service |
| US20140367515A1 (en) * | 2013-06-17 | 2014-12-18 | Airbus Operations Gmbh | Cargo handling system |
| CN209634712U (en) * | 2019-01-25 | 2019-11-15 | 西安飞豹科技有限公司 | A kind of mounting device of standard contained implement and the nonstandard track in military aircraft floor |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109720542B (en) | 2025-05-16 |
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