CN107672810A - A kind of general hang flies nacelle device - Google Patents
A kind of general hang flies nacelle device Download PDFInfo
- Publication number
- CN107672810A CN107672810A CN201610616859.4A CN201610616859A CN107672810A CN 107672810 A CN107672810 A CN 107672810A CN 201610616859 A CN201610616859 A CN 201610616859A CN 107672810 A CN107672810 A CN 107672810A
- Authority
- CN
- China
- Prior art keywords
- lid
- target seeker
- antenna
- gps
- frock
- 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
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 37
- 239000002828 fuel tank Substances 0.000 claims abstract description 30
- 238000012544 monitoring process Methods 0.000 claims abstract description 24
- 238000001816 cooling Methods 0.000 claims abstract description 11
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 11
- 238000009434 installation Methods 0.000 claims description 10
- 230000005540 biological transmission Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 230000002787 reinforcement Effects 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 3
- 238000013500 data storage Methods 0.000 claims description 2
- 239000004744 fabric Substances 0.000 claims 1
- 238000013461 design Methods 0.000 description 4
- 238000002474 experimental method Methods 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- 239000008358 core component Substances 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 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
- B64D7/08—Arrangements of rocket launchers or releasing means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The invention discloses a kind of general hang to fly nacelle device, including：Auxiliary fuel tank main body（1）, antenna house mounting ring（2）, antenna house（3）, radio antenna（4）, lid A（5）, lid B（6）, lid C（7）, target seeker（8）, gps antenna（9）, lid B reinforcing frames（10）, lid C reinforcing frames（11）, gps antenna frock（12）, lid A reinforcing frames（13）, 56V batteries（14）, 27V batteries（15）, target seeker frock（16）, reinforcing frame（17）, inertial navigation installing plate（18）, inertial navigation（19）, GPS radio station（20）, GPS radio station installing plate（21）, monitoring and control unit support（22）, monitoring and control unit（23）, supporting plate（24）, water cooling plant（25）And support frame（26）.Cost of the present invention is cheap, is easy to implement, and can be applicable different aircraft models, versatile.
Description
Technical field
Hung the present invention relates to one kind and fly nacelle device, particularly a kind of general hang flies nacelle device.
Background technology
Target seeker is guided missile detection and the core component of guidance, directly affects the accuracy at target of guided missile, and it is checking to hang winged experiment
The most important experiment of target seeker tracking performance, it is to carry out hanging the necessary devices for flying experiment to hang winged gondola, and domestic existing extension flies to hang
Cabin is all to fly experiment and special Development and design to hang, not only costly, design, production cycle length, and versatility is not strong,
It can not be used on the aircraft of various types；Especially, the aerodynamic configuration of gondola directly affects the flight of aircraft, if design is not
Rationally, aeroplane performance is gently then influenceed, it is heavy then cause fatal crass.Therefore, there is an urgent need to a kind of versatile, and can be applicable not
Extension with aircraft model flies nacelle device, meets that different subject target seeker products are hung and flies test requirements document.
The content of the invention
Present invention aims at providing a kind of general hang to fly nacelle device, solution existing apparatus is costly, design production
The problem of cycle length and not strong versatility.
A kind of general hang flies nacelle device, including：Auxiliary fuel tank main body, in addition to：Antenna house mounting ring, antenna house, radio station
Antenna, lid A, lid B, lid C, target seeker, gps antenna, lid B reinforcing frames, lid C reinforcing frames, gps antenna frock, mouth
Cover A reinforcing frames, 56V batteries, 27V batteries, target seeker frock, reinforcing frame, inertial navigation installing plate, inertial navigation, GPS radio station, GPS radio station peace
Loading board, monitoring and control unit support, monitoring and control unit, supporting plate, water cooling plant and support frame.
The reinforcing frame is spirally connected by end face and is fixedly connected with side riveting two ways with the front end of auxiliary fuel tank main body, institute
The pyramidal structure that antenna house is bottom surface opening is stated, the openend of antenna house is fixed by the antenna house mounting ring of annular with reinforcing frame
Connection, the target seeker are located in antenna house cavity and are fixed on by target seeker frock on reinforcing frame, wherein target seeker
Frock is that one end carries four columnar structured parts for being uniformly distributed reinforcement with ring flange and side；The gps antenna leads to
Cross gps antenna frock to be fixed in target seeker frock, inertial navigation installing plate is placed on target seeker frock ring flange and passes through spiral shell
Nail is fixedly connected with target seeker frock, and inertial navigation is located on inertial navigation installing plate and inertial navigation coordinate system is consistent with missile coordinate system, described
Lid A and the ring-type lid A reinforcing frames being riveted at auxiliary fuel tank body surfaces corresponding opening are spirally connected installation, and lid B is with being riveted on
Ring-type lid B reinforcing frames at auxiliary fuel tank body surfaces corresponding opening are spirally connected installation, lid C and are riveted on auxiliary fuel tank body surfaces
Ring-type lid C reinforcing frames at corresponding opening are spirally connected installation.
Support frame as described above includes multiple arcs sheet metal, and be arranged side by side and rivet the bottom surface for being fixed on auxiliary fuel tank body interior
On, supporting plate is fixed on support frame by screw connection manner, and the radio antenna is fixed on auxiliary fuel tank main body by screw
On support frame below front end, the monitoring and control unit support is each attached in supporting plate with water cooling plant, and monitoring and control unit is fixed on observing and controlling
The middle part of platform support, GPS radio station installing plate are fixed by screws on monitoring and control unit support, and GPS radio station are fixed on GPS radio station
Above installing plate, the 56V batteries share five pieces, and 27V batteries share two pieces, are installed in the support frame of auxiliary fuel tank body interior
On.
General hang flies nacelle device in use, subject target seeker is placed on the support frame of auxiliary fuel tank body interior, five
Block 56V batteries are connected into 280V power supplys, and the power supply of B groups is provided for subject target seeker；One piece of 27V battery provides A for subject target seeker
Group power supply；Another piece of 27V battery provides power supply for remaining equipment；Emitter and phased array day of the water cooling plant to subject target seeker
Line is cooled down；Inertial navigation is used for the posture for recording subject target seeker；Monitoring and control unit is used to carry out data storage and transmission, and provides and lead
The guiding data of leader；Radio antenna, which is used to realize with ground base station, to be communicated；Gps antenna is used to receive gps signal with GPS radio station
And target seeker is positioned.
Present apparatus cost is cheap, is easy to implement, and can meet that the outfield of different target seekers is hung and fly to test and can be applicable difference
Aircraft model, it is versatile.
Brief description of the drawings
A kind of general structure charts for hanging winged nacelle device of Fig. 1；
A kind of general local structural graphs for hanging winged nacelle device of Fig. 2；
A kind of general auxiliary fuel tank body interior structure charts for hanging winged nacelle device of Fig. 3.
1. 7. mouthfuls of 6. lid B of auxiliary fuel tank main body 2. antenna house mounting ring, 3. antenna house, 4. radio antenna, 5. lid A
Cover the lid A of 8. target seeker 9.GPS antennas of C, 10. lid B reinforcing frames, 11. lid C reinforcing frame 12.GPS antennas frock 13.
The inertial navigation of 18. inertial navigation installing plate of reinforcing frame 14.56V battery 15.27V battery 16. target seeker frock, 17. reinforcing frames 19.
The water cooling plant 26. of 20.GPS radio station 21.GPS radio station 24. supporting plate of installing plate 22. monitoring and control unit support, 23. monitoring and control unit 25.
Support frame.
Embodiment
A kind of general hang flies nacelle device, including：Auxiliary fuel tank main body 1, in addition to：Antenna house mounting ring 2, antenna house 3, electricity
Platform antenna 4, lid A 5, lid B 6, lid C 7, target seeker 8, gps antenna 9, lid B reinforcing frames 10, lid C reinforcing frames 11,
Gps antenna frock 12, lid A reinforcing frames 13,56V batteries 14,27V batteries 15, target seeker frock 16, reinforcing frame 17, inertial navigation peace
Loading board 18, inertial navigation 19, GPS radio station 20, GPS radio station installing plate 21, monitoring and control unit support 22, monitoring and control unit 23, supporting plate 24, water cooling dress
Put 25 and support frame 26.
The reinforcing frame 17 is spirally connected by end face rivets the front end fixation company of two ways and auxiliary fuel tank main body 1 with side
Connect, the antenna house 3 is the pyramidal structure of bottom surface opening, and the openend of antenna house 3 by annular antenna house mounting ring 2 and adds
Strong frame 17 is fixedly connected, and the target seeker 8 is located in the cavity of antenna house 3 and is fixed on reinforcing frame by target seeker frock 16
On 17, the gps antenna 9 is fixed in target seeker frock 16 by gps antenna frock 12, and the radio antenna 4 passes through
Screw is arranged on the support frame 26 below the front end of auxiliary fuel tank main body 1, and target seeker frock 16 is that one end carries ring flange and side
Cylindrical structure with four uniform reinforcements, inertial navigation installing plate 18 be placed on the ring flange of target seeker frock 16 and by screw with
Target seeker frock 16 is attached, and inertial navigation 19 is located on inertial navigation installing plate 18 and the coordinate system of inertial navigation 19 is consistent with missile coordinate system,
The lid A 5 and the ring-type lid A reinforcing frames 13 being riveted at the surface corresponding opening of auxiliary fuel tank main body 1 are spirally connected installation, lid B
6 are spirally connected installation with the ring-type lid B reinforcing frames 10 that are riveted at the surface corresponding opening of auxiliary fuel tank main body 1, and lid C 7 is with being riveted on
Ring-type lid C reinforcing frames 11 at the surface corresponding opening of auxiliary fuel tank main body 1 are spirally connected installation.
Support frame as described above 26 includes multiple arcs sheet metal, and being arranged side by side and riveting is fixed on inside auxiliary fuel tank main body 1
On bottom surface, supporting plate 24 is fixed on support frame 26 by screw connection manner, and the monitoring and control unit support 22 and water cooling plant 25 are solid
It is scheduled in supporting plate 24, monitoring and control unit 23 is fixed on the middle part of monitoring and control unit support 22, and GPS radio station installing plate 21 is screwed
On monitoring and control unit support 22, GPS radio station 20 are fixed on the top of GPS radio station installing plate 21, and the 56V batteries 14 share five pieces, 27V
Battery 15 shares two pieces, is arranged on by support frame 26 inside auxiliary fuel tank main body 1.
General hang flies nacelle device in use, subject target seeker 8 to be placed on to the support frame 26 inside auxiliary fuel tank main body 1
On, five pieces of 56V batteries 14 are connected into 280V power supplys, and the power supply of B groups is provided for subject target seeker 8；One piece of 27V battery 15 is led for subject
Leader 8 provides the power supply of A groups；Another piece of 27V battery 15 provides power supply for remaining equipment；Water cooling plant 25 is to subject target seeker 8
Emitter and phased array antenna are cooled down；Inertial navigation 19 is used for the posture for recording subject target seeker 8；Monitoring and control unit 23 is used for into line number
According to storage and transmission, and provide the guiding data of target seeker 8；Radio antenna 4, which is used to realize with ground base station, to be communicated；Gps antenna 9
It is used to receive gps signal with GPS radio station 20 and target seeker 8 is positioned.
Claims (1)
1. a kind of general hang flies nacelle device, including：Auxiliary fuel tank main body（1）, it is characterised in that also include：Antenna house mounting ring
（2）, antenna house（3）, radio antenna（4）, lid A（5）, lid B（6）, lid C（7）, target seeker（8）, gps antenna（9）, mouth
Cover B reinforcing frames（10）, lid C reinforcing frames（11）, gps antenna frock（12）, lid A reinforcing frames（13）, 56V batteries（14）、27V
Battery（15）, target seeker frock（16）, reinforcing frame（17）, inertial navigation installing plate（18）, inertial navigation（19）, GPS radio station（20）, GPS electricity
Platform installing plate（21）, monitoring and control unit support（22）, monitoring and control unit（23）, supporting plate（24）, water cooling plant（25）And support frame（26）；
The reinforcing frame（17）It is spirally connected by end face and rivets two ways and auxiliary fuel tank main body with side（1）Front end fix connect
Connect, the antenna house（3）For the pyramidal structure of bottom surface opening, antenna house（3）Openend pass through annular antenna house mounting ring
（2）With reinforcing frame（17）It is fixedly connected, the target seeker（8）Positioned at antenna house（3）Cavity is interior and passes through target seeker frock（16）
It is fixed on reinforcing frame（17）On, wherein target seeker frock（16）Uniformly divide with four with ring flange and side for one end
The columnar structured part of cloth reinforcement；The gps antenna（9）Pass through gps antenna frock（12）It is fixed on target seeker frock
（16）On, inertial navigation installing plate（18）It is placed in target seeker frock（16）On ring flange and pass through screw and target seeker frock（16）It is fixed
Connection, inertial navigation（19）Positioned at inertial navigation installing plate（18）Upper and inertial navigation coordinate system is consistent with missile coordinate system, the lid A（5）With
It is riveted on auxiliary fuel tank main body（1）Ring-type lid A reinforcing frames at the corresponding opening of surface（13）Be spirally connected installation, lid B（6）With riveting
In auxiliary fuel tank main body（1）Ring-type lid B reinforcing frames at the corresponding opening of surface（10）Be spirally connected installation, lid C（7）With being riveted on pair
Fuel tank main body（1）Ring-type lid C reinforcing frames at the corresponding opening of surface（11）Be spirally connected installation；
Support frame as described above（26）Including multiple arcs sheet metal, being arranged side by side and riveting is fixed on auxiliary fuel tank main body（1）Internal
On bottom surface, supporting plate（24）Support frame is fixed on by screw connection manner（26）On, the radio antenna（4）It is solid by screw installation
It is scheduled on auxiliary fuel tank main body（1）Support frame below front end（26）On, the monitoring and control unit support（22）With water cooling plant（25）It is solid
It is scheduled on supporting plate（24）On, monitoring and control unit（23）It is fixed on monitoring and control unit support（22）Middle part, GPS radio station installing plate（21）It is logical
Cross screw and be fixed on monitoring and control unit support（22）On, GPS radio station（20）It is fixed on GPS radio station installing plate（21）Top, the 56V electricity
Pond（14）Five pieces are shared, 27V batteries（15）Two pieces are shared, is installed in auxiliary fuel tank main body（1）Internal support frame（26）On；
General hang flies nacelle device in use, target seeker will be tested（8）It is placed on auxiliary fuel tank main body（1）Internal support frame（26）
On, five pieces of 56V batteries（14）280V power supplys are connected into, to be tested target seeker（8）The power supply of B groups is provided；One piece of 27V battery（15）For
It is tested target seeker（8）The power supply of A groups is provided；Another piece of 27V battery（15）Power supply is provided for remaining equipment；Water cooling plant（25）To quilt
Try target seeker（8）Emitter and phased array antenna cooled down；Inertial navigation（19）Target seeker is tested for recording（8）Posture；
Monitoring and control unit（23）For carrying out data storage and transmission, and provide target seeker（8）Guiding data；Radio antenna（4）For with
Ground base station realizes communication；Gps antenna（9）With GPS radio station（20）For receiving gps signal and to target seeker（8）Positioned.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610616859.4A CN107672810A (en) | 2016-08-01 | 2016-08-01 | A kind of general hang flies nacelle device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610616859.4A CN107672810A (en) | 2016-08-01 | 2016-08-01 | A kind of general hang flies nacelle device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107672810A true CN107672810A (en) | 2018-02-09 |
Family
ID=61132954
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610616859.4A Pending CN107672810A (en) | 2016-08-01 | 2016-08-01 | A kind of general hang flies nacelle device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107672810A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367800A (en) * | 2018-08-28 | 2019-02-22 | 郑州郑飞机电技术有限责任公司 | A kind of novel gondola for aviation loading |
| CN109449591A (en) * | 2018-10-25 | 2019-03-08 | 湖北航天技术研究院总体设计所 | Active radar and passive radar seeker antenna cover and aircraft |
| CN111661349A (en) * | 2020-05-21 | 2020-09-15 | 北京爱思达航天科技有限公司 | Fuel tank for fixed-wing aircraft |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103728140A (en) * | 2013-12-04 | 2014-04-16 | 中国飞行试验研究院 | Flight test pod for small-sized turbojet engine |
-
2016
- 2016-08-01 CN CN201610616859.4A patent/CN107672810A/en active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103728140A (en) * | 2013-12-04 | 2014-04-16 | 中国飞行试验研究院 | Flight test pod for small-sized turbojet engine |
Non-Patent Citations (1)
| Title |
|---|
| 张铁军: "某机载雷达模拟吊舱结构设计", 《电子机械工程》 * |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109367800A (en) * | 2018-08-28 | 2019-02-22 | 郑州郑飞机电技术有限责任公司 | A kind of novel gondola for aviation loading |
| CN109367800B (en) * | 2018-08-28 | 2021-10-15 | 郑州郑飞机电技术有限责任公司 | Novel nacelle for aerial cargo |
| CN109449591A (en) * | 2018-10-25 | 2019-03-08 | 湖北航天技术研究院总体设计所 | Active radar and passive radar seeker antenna cover and aircraft |
| CN111661349A (en) * | 2020-05-21 | 2020-09-15 | 北京爱思达航天科技有限公司 | Fuel tank for fixed-wing aircraft |
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|---|---|---|---|
| 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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180209 |