CN106184778B - A kind of gun pod waste gas flow guiding device - Google Patents
A kind of gun pod waste gas flow guiding device Download PDFInfo
- Publication number
- CN106184778B CN106184778B CN201610843732.6A CN201610843732A CN106184778B CN 106184778 B CN106184778 B CN 106184778B CN 201610843732 A CN201610843732 A CN 201610843732A CN 106184778 B CN106184778 B CN 106184778B
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- China
- Prior art keywords
- gun
- aircraft
- side wall
- exhaust gas
- gas flow
- 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.)
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Links
- 239000002912 waste gas Substances 0.000 title claims abstract description 21
- 239000007789 gas Substances 0.000 claims abstract description 27
- 238000010586 diagram Methods 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 210000001015 abdomen Anatomy 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Exhaust Silencers (AREA)
Abstract
A kind of gun pod waste gas flow guiding device, including the undercut shape structure being made of cambered surface and semi-open type flow-guiding channel, undercut shape structure is mounted on gun pod body front end and covers tampion, and undercut shape structure forms three face semi-open types to tampion and surrounds, and then aircraft gun exhaust gas is prevented to spread to the air intake duct direction of aircraft two sides；In front under the action of air incoming flow, aircraft gun exhaust gas is spread along aircraft gun exhaust gas flow-guiding channel to the back lower place.The present invention, to construct flow-guiding channel and then change the flow direction of aircraft gun exhaust gas, to realize the target for reducing the air intake duct aircraft gun exhausted air quantity for entering aircraft two sides with the smallest cost, guarantees the normal operation of engine by installing gun pod waste gas flow guiding device additional.
Description
Technical field
The present invention relates to the pneumatic diversion technology field of aircraft more particularly to a kind of gun pod waste gas flow guiding devices.
Background technique
The gun pod plug-in ability one of standing as fighter plane is mounted, when gun pod is mounted on aircraft belly air inlet
When in front of road, the exhaust gas that aircraft gun generates is back into aircraft side inlet.Aircraft gun exhaust gas into airplane intake reduces
The degree of purity of engine charge results even in engine and surge occurs to influence to influence the normal working performance of engine
Failure.
Summary of the invention
Technical problem solved by the invention is to provide a kind of gun pod waste gas flow guiding device, to solve above-mentioned background
Disadvantage in technology.
Technical problem solved by the invention is realized using following technical scheme:
A kind of gun pod waste gas flow guiding device, including the undercut shape knot being made of cambered surface and semi-open type flow-guiding channel
Structure, undercut shape structure are mounted on gun pod body front end and cover tampion, and undercut shape structure is to gun muzzle hat
It is surrounded at three face semi-open types, and then aircraft gun exhaust gas is prevented to spread to the air intake duct direction of aircraft two sides；The air incoming flow in front
Under effect, aircraft gun exhaust gas is spread along cambered surface and semi-open type flow-guiding channel to the back lower place, by installing gun pod exhaust gas water conservancy diversion
Device guides aircraft gun waste gas flow direction, so that the aircraft gun exhausted air quantity into aircraft side inlet is reduced, to guarantee engine just
Often work.
In the present invention, undercut shape structural openings are gradually reduced from front end to end, and first in undercut shape structure
Left side wall is longer than right side wall at section (I-I)；Left side wall is longer than right side wall at second section (II-II), while the first section (I-
I right side wall ratio left side wall thickness at), left side wall ratio right side wall thickness at the second section (II-II)；Semi-open type flow-guiding channel bottom is arc
Face constitutes aircraft gun exhaust gas flow-guiding channel with left side wall, the right side wall of undercut shape structure.
In the present invention, the undercut shape structure of gun pod waste gas flow guiding device prevents aircraft gun exhaust gas to aircraft two sides
The diffusion of air intake duct direction, the air incoming flow in front spread aircraft gun exhaust gas to the back lower place along aircraft gun exhaust gas flow-guiding channel；?
Under the conditions of meeting aircraft gun routine use, requirement light-weight, that structure is simple and at low cost is combined, by gun pod
Installing waste gas flow guiding device additional just can be reduced the air intake duct aircraft gun exhausted air quantity into aircraft two sides.
The utility model has the advantages that the present invention, which passes through, installs gun pod waste gas flow guiding device additional, with building " aircraft gun exhaust gas flow-guiding channel "
And then change the flow direction of aircraft gun exhaust gas, the air intake duct aircraft gun exhausted air quantity for entering aircraft two sides is reduced to realize with the smallest cost
Target, guarantee the normal operation of engine.
Detailed description of the invention
Fig. 1 is traditional gun pod schematic diagram.
Fig. 2 is traditional aircraft gun exhaust gas discharge schematic diagram.
Fig. 3 is that gun pod waste gas flow guiding device and the installation of gun pod main body are illustrated in presently preferred embodiments of the present invention
Figure.
Fig. 4 is the structural schematic diagram of presently preferred embodiments of the present invention.
Fig. 5 is cross-sectional view at I in Fig. 4.
Fig. 6 is cross-sectional view at II in Fig. 4.
Fig. 7 is the side view of Fig. 3.
Fig. 8 is tampion and semi-open type flow-guiding channel scheme of installation in presently preferred embodiments of the present invention.
Fig. 9 is the aircraft gun exhaust gas discharge schematic diagram in presently preferred embodiments of the present invention.
In attached drawing, 1, tampion, 2, gun pod main body, 3, air intake duct, 4, gun pod waste gas flow guiding device, 5, half-open
Formula flow-guiding channel, " → " indicate aircraft gun waste gas flow direction.
Specific embodiment
In order to be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, tie below
Conjunction is specifically illustrating, and the present invention is further explained.
As shown in FIG. 1 to FIG. 2, the tampion 1 of common aircraft gun is mounted on outside gun pod main body 2, part aircraft gun when setting off firecrackers
Exhaust gas is discharged in the horizontal direction to two sides, easily enters the air intake duct 3 of aircraft two sides, to influence engine work.
Referring to a kind of gun pod waste gas flow guiding device of Fig. 3~Fig. 9, including by cambered surface and 5 structure of semi-open type flow-guiding channel
At undercut shape structure gun pod is installed in 2 front end of gun pod main body to reduce influence of the aircraft gun exhaust gas to engine
Waste gas flow guiding device 4, and gun pod waste gas flow guiding device 4 covers tampion 1, to avoid aircraft gun exhaust gas to aircraft two sides
The diffusion of 3 direction of air intake duct.As shown in figure 9, the undercut shape structure of gun pod waste gas flow guiding device 4 forms three to tampion 1
Face semi-open type is surrounded, and then aircraft gun exhaust gas is prevented to spread to 3 direction of air intake duct of aircraft two sides；In the effect of front air incoming flow
Under, aircraft gun exhaust gas is spread along cambered surface and semi-open type flow-guiding channel 5 to the back lower place, by installing gun pod waste gas flow guiding device
4 guidance aircraft gun waste gas flow directions, so that the 3 aircraft gun exhausted air quantity of air intake duct into aircraft two sides is reduced, to guarantee the normal of engine
Work.
In the present embodiment, undercut shape structural openings are gradually reduced from front end to end, take wherein at two section I-I and
II-II is as shown in Figure 5,6, wherein at the section I-I, the left side wall of undercut shape structure is longer than right side wall；At the section II-II,
The left side wall of concave-shaped structure is longer than right side wall, and right side wall ratio left side wall thickness at the section I-I, left side wall ratio at the section II-II
Right side wall thickness；5 bottom of semi-open type flow-guiding channel is cambered surface simultaneously, constitutes aircraft gun with left side wall, the right side wall of undercut shape structure
Exhaust gas flow-guiding channel.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention.The technology of the industry
Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the above embodiments and description only describe this
The principle of invention, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these changes
Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its
Equivalent thereof.
Claims (1)
1. a kind of gun pod waste gas flow guiding device, which is characterized in that fallen including what is be made of cambered surface and semi-open type flow-guiding channel
Concave-shaped structure, undercut shape structure are mounted on gun pod body front end and cover tampion, and undercut shape structure is to big gun
Mouth cap forms three face semi-open types and surrounds, and then aircraft gun exhaust gas is prevented to spread to the air intake duct direction of aircraft two sides；And undercut shape
Structural openings are gradually reduced from front end to end, and left side wall is longer than right side wall at the first section (I-I) in undercut shape structure, the
Left side wall is longer than right side wall at two sections (II-II), while right side wall ratio left side wall thickness at the first section (I-I), the second section
(II-II) left side wall ratio right side wall thickness at；Semi-open type flow-guiding channel bottom is cambered surface, left side wall, the right side with undercut shape structure
Side wall constitutes aircraft gun exhaust gas flow-guiding channel, and in front under the action of air incoming flow, aircraft gun exhaust gas is along aircraft gun exhaust gas flow-guiding channel
It is spread to the back lower place.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610843732.6A CN106184778B (en) | 2016-09-23 | 2016-09-23 | A kind of gun pod waste gas flow guiding device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610843732.6A CN106184778B (en) | 2016-09-23 | 2016-09-23 | A kind of gun pod waste gas flow guiding device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106184778A CN106184778A (en) | 2016-12-07 |
| CN106184778B true CN106184778B (en) | 2019-03-29 |
Family
ID=58067138
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610843732.6A Active CN106184778B (en) | 2016-09-23 | 2016-09-23 | A kind of gun pod waste gas flow guiding device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184778B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB787722A (en) * | 1955-02-24 | 1957-12-11 | North American Aviation Inc | Improvements in or relating to gun installation in aircraft |
| GB803906A (en) * | 1956-01-20 | 1958-11-05 | Chance Vought Aircraft Inc | Improvements relating to means for controlling release of blast gases from armament on aircraft |
| US4619182A (en) * | 1983-01-31 | 1986-10-28 | Saab-Scania Aktiebolag | Arrangement for deflecting powder gases from an aircraft weapon |
| US5485775A (en) * | 1994-12-16 | 1996-01-23 | The United States Of America As Represented By The Secretary Of The Air Force | Gun gas control system for multi-barrel weapons |
| CN104401494A (en) * | 2014-11-19 | 2015-03-11 | 中国航空工业集团公司沈阳飞机设计研究所 | Ventilation structure for aircraft gun |
| CN206125444U (en) * | 2016-09-23 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Boat big gun nacelle waste gas guiding device |
-
2016
- 2016-09-23 CN CN201610843732.6A patent/CN106184778B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB787722A (en) * | 1955-02-24 | 1957-12-11 | North American Aviation Inc | Improvements in or relating to gun installation in aircraft |
| GB803906A (en) * | 1956-01-20 | 1958-11-05 | Chance Vought Aircraft Inc | Improvements relating to means for controlling release of blast gases from armament on aircraft |
| US4619182A (en) * | 1983-01-31 | 1986-10-28 | Saab-Scania Aktiebolag | Arrangement for deflecting powder gases from an aircraft weapon |
| US5485775A (en) * | 1994-12-16 | 1996-01-23 | The United States Of America As Represented By The Secretary Of The Air Force | Gun gas control system for multi-barrel weapons |
| CN104401494A (en) * | 2014-11-19 | 2015-03-11 | 中国航空工业集团公司沈阳飞机设计研究所 | Ventilation structure for aircraft gun |
| CN206125444U (en) * | 2016-09-23 | 2017-04-26 | 江西洪都航空工业集团有限责任公司 | Boat big gun nacelle waste gas guiding device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106184778A (en) | 2016-12-07 |
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