CN106741961A - A kind of aircraft hanger - Google Patents
A kind of aircraft hanger Download PDFInfo
- Publication number
- CN106741961A CN106741961A CN201611180269.8A CN201611180269A CN106741961A CN 106741961 A CN106741961 A CN 106741961A CN 201611180269 A CN201611180269 A CN 201611180269A CN 106741961 A CN106741961 A CN 106741961A
- Authority
- CN
- China
- Prior art keywords
- axle
- hanger
- beam body
- back porch
- aircraft
- 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.)
- Pending
Links
- 238000009434 installation Methods 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 abstract description 9
- 239000000725 suspension Substances 0.000 abstract description 8
- 230000004927 fusion Effects 0.000 description 2
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Holders For Apparel And Elements Relating To Apparel (AREA)
Abstract
The invention discloses a kind of aircraft hanger, belong to airborne overall design technique field.Including crop axle, back porch axle, hanger beam body, hanging hook assembly and connecting bolt；Crop axle and back porch axle are separately fixed at the left and right two ends at the top of hanger beam body by connecting bolt, back porch axle can move forward and backward installation in hanger beam body, hanging hook assembly is arranged on the bottom beam body sidewall of the hanger beam body, hanger is connected by crop axle and back porch axle with airframe, and hanger is connected by hook groups with airframe；Because hanger employs integral design, make drop in beam in suspension, upper interface is connected by way of forward and backward shoulder axle connecting bolt and front and rear shoulder axle are connected with the structure of aircraft, solve the problems, such as too small because of the specific hanging point road clearance and use safe requirement；Technique is the first Application on type aircraft, is adapted to the design feature of feature hanging point demand, and the technical research and design that can be used for follow-up various aircraft types and hanger are supported.
Description
Technical field
The invention belongs to airborne overall design technique field, and in particular to a kind of aircraft hanger.
Background technology
At aircraft hanging point, if the design of suspension solutions does not use special design, design cannot be often met
It is required that the use requirement with hanger.
Hanger is a kind of suspension arrangement of airborne equipment, has important work in air weapon fire control overall design technique
With.
In the design of conventional each model, the hang of hanging point is generally and is resuspended respectively by transition beam or suspension intersection point
Type hanger mounts hanger to realize the suspension of hanger again.If being also adopted by this kind of setting at fuselage hanging point or at specific hanging point
Meter mode, although can also be realized on design form, but because suspension series is too many, cause the road clearance mistake of hanger
It is small, design requirement is unsatisfactory for, while also easily occurring flight safety problem during the use of aircraft.
The content of the invention
The purpose of the present invention：In order to solve the above problems, the present invention provides a kind of aircraft hanger designing technique, and hanger sets
Meter uses fusion type designing technique, solve it is above-mentioned because the specific hanging point road clearance it is too small and requirement using safety ask
Topic.
Technical scheme：A kind of aircraft hanger, it is adaptable between airframe and hanger, including crop axle,
Back porch axle, hanger beam body hanging hook assembly and connecting bolt；
The crop axle and back porch axle are separately fixed at the left and right two ends at the top of hanger beam body, institute by the connecting bolt
Stating back porch axle can move forward and backward installation in hanger beam body, and the hanging hook assembly is arranged on the bottom beam body of the hanger beam body
On the wall of side, the hanger is connected by crop axle and back porch axle with airframe, and hanger passes through hanging hook assembly and airframe
Connection.
Preferably, the crop axle and back porch axle bottom are respectively arranged with lug-mounted, and the lug-mounted is symmetrical
It is provided with the installation bushing of internal thread.
Preferably, described connecting bolt one end is connected through the bushing with airframe.
Preferably, the other end of the connecting bolt is provided with insurance hole, and the connecting bolt fixes institute by fuse
State in hanger beam body.
Preferably, the hanger beam body is provided with arc opening groove, and the arc opening groove coordinates with the lug-mounted.
Preferably, the back porch axle is provided with pin hole, and the side wall of the hanger beam body is provided with strip circular hole, described
Back porch axle is arranged in the strip circular hole by bearing pin.
Technique effect of the invention：The present invention employs integral design due to hanger, makes drop in beam in suspension, upper interface
It is connected with the structure of aircraft by crop axle, back porch axle and connecting bolt, is adapted to the design feature of feature hanging point demand, is can be used for
The technical research and design of follow-up various aircraft types and hanger are supported.
Brief description of the drawings
Fig. 1 is a kind of front view of a preferred embodiment of aircraft hanger of the invention；
Fig. 2 is a kind of top view of a preferred embodiment of aircraft hanger of the invention；
Fig. 3 is a kind of A-A sectional views of a preferred embodiment of aircraft hanger of the invention.
Wherein, 1- crops axle, 2- back porch axles, 3- hanger beam bodies, 4- hanging hook assemblies, 5- connecting bolts, 6- lug-mounteds, 7-
Bushing, 31- arc opening grooves are installed.
Specific embodiment
To make the purpose, technical scheme and advantage of present invention implementation clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from start to finish or class
As label represent same or similar element or the element with same or like function.Described embodiment is the present invention
A part of embodiment, rather than whole embodiments.Embodiment below with reference to Description of Drawings is exemplary, it is intended to used
It is of the invention in explaining, and be not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under the premise of creative work is not made, belongs to the scope of protection of the invention.Under
Face is described in detail with reference to accompanying drawing to embodiments of the invention.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward " are based on accompanying drawing institute
The orientation or position relationship for showing, are for only for ease of the description present invention and simplify description, rather than the dress for indicating or implying meaning
Put or element with specific orientation, with specific azimuth configuration and operation, therefore it is not intended that must be protected to the present invention
The limitation of scope.
Embodiments of the invention are described in detail below in conjunction with the accompanying drawings, refer to Fig. 1 to Fig. 3；
A kind of aircraft hanger, it is adaptable between airframe and hanger, including crop axle 1, back porch axle 2, hanger beam body
3rd, hanging hook assembly 4 and connecting bolt 5；
Crop axle 1 and the bottom of back porch axle 2 are respectively arranged with lug-mounted 6, and lug-mounted 6 is symmetrical set with interior spiral shell
The installation bushing 7 of line, installs bushing 7 and coordinates with connecting bolt 5；
The one end of back porch axle 2 is provided with pin hole, and the side wall of hanger beam body 3 is provided with strip circular hole, and back porch axle 2 passes through pin
Axle is arranged in the strip circular hole, and back porch axle 2 can select installation site and by pin by bearing pin in strip circular hole
The nut screwing clamping of axle one end, so as to fixedly mount back porch axle 2, the front and rear mounting distance for realizing back porch axle 2 is adjustable, can hang
Set a roof beam in place front and rear motion compensation alignment error on body 3.
Hanger beam body 3 is provided with arc opening groove 31, and arc opening groove 31 coordinates with lug-mounted 6, ensure that connection
The installation site of bolt 5 is adjustable, convenient to install, while can also meet the installation site regulation of back porch axle 2.
The left and right two ends for being separately fixed at the top of hanger beam body 3 that crop axle 1 and back porch axle 2 pass through connecting bolt 5, connection
The one end of bolt 5 is provided with insurance hole, and connecting bolt 5 is fixed in hanger beam body 3 by fuse, connecting bolt 5 it is another
End coordinates through bushing and airframe installs, and so as to realize crop axle 1 and back porch axle 2, hanger beam body 3 is respectively by connecting spiral shell
Bolt 5, crop axle 1 and back porch axle 2 are realized installing and fixed with airframe, it is ensured that the intensity and precision of installation.
Hanging hook assembly 4 is arranged on the bottom beam body sidewall of hanger beam body 3 by fastener, hanger by crop axle 1 and
Back porch axle 2 is connected with airframe, and hanger is connected by hanging hook assembly 4 with airframe.
A kind of aircraft hanger design of the present invention uses fusion type designing technique, because hanger employs integral design, makes
In suspension, upper interface connects drop in beam by way of forward and backward shoulder axle connecting bolt and front and rear shoulder axle are connected with the structure of aircraft
Connect, solve the problems, such as too small because of the specific hanging point road clearance and use safe requirement；Technique is in type aircraft
Upper first Application, is adapted to the design feature of feature hanging point demand, can be used for the technical research of follow-up various aircraft types and hanger
Supported with design.
It is last it is to be noted that：The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations.To the greatest extent
Pipe has been described in detail to the present invention with reference to the foregoing embodiments, it will be understood by those within the art that：It is still
Technical scheme described in foregoing embodiments can be modified, or which part technical characteristic is equally replaced
Change；And these modifications or replacement, do not make the essence of the essence disengaging various embodiments of the present invention technical scheme of appropriate technical solution
God and scope.
Claims (6)
1. a kind of aircraft hanger, it is adaptable between airframe and hanger, it is characterised in that；Including crop axle (1), back porch axle
(2), hanger beam body (3), hanging hook assembly (4) and connecting bolt (5)；
The crop axle (1) and back porch axle (2) are separately fixed at the left side at the top of hanger beam body (3) by the connecting bolt (5)
Right two ends, the back porch axle (2) can move forward and backward installation in hanger beam body (3), and the hanging hook assembly (4) is installed in described
On the bottom beam body sidewall of hanger beam body (3), the hanger is connected by crop axle (1) and back porch axle (2) with airframe, is hanged
Thing is hung to be connected with airframe by hanging hook assembly (4).
2. a kind of aircraft hanger according to claim 1, it is characterised in that the crop axle (1) and back porch axle (2) bottom
Lug-mounted (6) is respectively arranged with, the lug-mounted (6) is symmetrical set with female installation bushing (7).
3. a kind of aircraft hanger according to claim 1, it is characterised in that described connecting bolt (5) one end is through described
Bushing (7) is installed to be connected with airframe.
4. a kind of aircraft hanger according to claim 1, it is characterised in that the other end of the connecting bolt (5) is set
There is insurance hole, the connecting bolt (5) is fixed in the hanger beam body (3) by fuse.
5. a kind of aircraft hanger according to claim 1, it is characterised in that the hanger beam body (3) is provided with arc and opens
Mouth groove (31), the arc opening groove (31) and the lug-mounted (6) coordinate.
6. a kind of aircraft hanger according to claim 1, it is characterised in that the back porch axle (2) is provided with pin hole, institute
The side wall for stating hanger beam body (3) is provided with strip circular hole, and the back porch axle (2) is arranged on the strip circular hole by bearing pin
It is interior.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2016110925775 | 2016-11-30 | ||
| CN201611092577 | 2016-11-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106741961A true CN106741961A (en) | 2017-05-31 |
Family
ID=58890817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611180269.8A Pending CN106741961A (en) | 2016-11-30 | 2016-12-19 | A kind of aircraft hanger |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106741961A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367788A (en) * | 2018-12-03 | 2019-02-22 | 中航技进出口有限责任公司 | Multifunctional universal suspension arrangement |
| CN109606686A (en) * | 2018-12-10 | 2019-04-12 | 彩虹无人机科技有限公司 | A kind of universal unmanned plane emitter switching beam |
| RU199505U1 (en) * | 2020-01-20 | 2020-09-04 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | MOUNTING DEVICE TO AIRCRAFT BUNKER |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3438304A (en) * | 1966-05-18 | 1969-04-15 | Matra Engins | Device for mounting a gun beneath the wing of an airplane |
| US4412475A (en) * | 1980-05-27 | 1983-11-01 | Northrop Corporation | Aircraft rocket and missile launcher |
| CN201329958Y (en) * | 2008-12-11 | 2009-10-21 | 中航天水飞机工业有限责任公司 | Switching beam |
| CN103995955A (en) * | 2014-04-17 | 2014-08-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Method for analyzing bearing capacity of airplane external store connection structure |
| US20150021436A1 (en) * | 2013-07-22 | 2015-01-22 | Sikorsky Aircraft Corporation | Wing mount adjustment |
| CN105486484A (en) * | 2014-10-11 | 2016-04-13 | 中国航空工业集团公司西安飞机设计研究所 | Pylon pitching modal simulation device suitable to be used for flutter wind tunnel model |
-
2016
- 2016-12-19 CN CN201611180269.8A patent/CN106741961A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3438304A (en) * | 1966-05-18 | 1969-04-15 | Matra Engins | Device for mounting a gun beneath the wing of an airplane |
| US4412475A (en) * | 1980-05-27 | 1983-11-01 | Northrop Corporation | Aircraft rocket and missile launcher |
| CN201329958Y (en) * | 2008-12-11 | 2009-10-21 | 中航天水飞机工业有限责任公司 | Switching beam |
| US20150021436A1 (en) * | 2013-07-22 | 2015-01-22 | Sikorsky Aircraft Corporation | Wing mount adjustment |
| CN103995955A (en) * | 2014-04-17 | 2014-08-20 | 中国航空工业集团公司沈阳飞机设计研究所 | Method for analyzing bearing capacity of airplane external store connection structure |
| CN105486484A (en) * | 2014-10-11 | 2016-04-13 | 中国航空工业集团公司西安飞机设计研究所 | Pylon pitching modal simulation device suitable to be used for flutter wind tunnel model |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367788A (en) * | 2018-12-03 | 2019-02-22 | 中航技进出口有限责任公司 | Multifunctional universal suspension arrangement |
| CN109367788B (en) * | 2018-12-03 | 2023-08-22 | 中航技进出口有限责任公司 | Multifunctional universal suspension device |
| CN109606686A (en) * | 2018-12-10 | 2019-04-12 | 彩虹无人机科技有限公司 | A kind of universal unmanned plane emitter switching beam |
| RU199505U1 (en) * | 2020-01-20 | 2020-09-04 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | MOUNTING DEVICE TO AIRCRAFT BUNKER |
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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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170531 |
|
| RJ01 | Rejection of invention patent application after publication |