CN111605632A - A kuppe for turbine engine convenient to installation - Google Patents
A kuppe for turbine engine convenient to installation Download PDFInfo
- Publication number
- CN111605632A CN111605632A CN202010336825.6A CN202010336825A CN111605632A CN 111605632 A CN111605632 A CN 111605632A CN 202010336825 A CN202010336825 A CN 202010336825A CN 111605632 A CN111605632 A CN 111605632A
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- CN
- China
- Prior art keywords
- sets
- air guide
- kuppe
- turbine engine
- 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.)
- Pending
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D35/00—Vehicle bodies characterised by streamlining
- B62D35/001—For commercial vehicles or tractor-trailer combinations, e.g. caravans
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D46/00—Filters or filtering processes specially modified for separating dispersed particles from gases or vapours
- B01D46/10—Particle separators, e.g. dust precipitators, using filter plates, sheets or pads having plane surfaces
- B01D46/12—Particle separators, e.g. dust precipitators, using filter plates, sheets or pads having plane surfaces in multiple arrangements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K11/00—Arrangement in connection with cooling of propulsion units
- B60K11/06—Arrangement in connection with cooling of propulsion units with air cooling
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a convenient-to-install air guide sleeve for a turbine engine, which belongs to the technical field of turbine engines and comprises a fixed plate, wherein the top of the fixed plate is provided with a base, the bottom of an inner cavity of the base is provided with a cushion pad, the top of the cushion pad is provided with an outer casing, the inner cavity of the outer casing is provided with an engine body, the bottom of the outer casing, the cushion pad, the bottom of the base and the fixed plate are all provided with consistent through holes in a penetrating manner, the tops of left and right end faces are all provided with L-shaped plates, and the top of the outer casing is sleeved with a detachable air guide sleeve.
Description
Technical Field
The invention relates to the technical field of turbine engines, in particular to a guide cover for a turbine engine, which is convenient to install.
Background
A turbine engine is a form of engine that uses rotating parts to extract kinetic energy from a fluid passing through it, one type of internal combustion engine.
The engine kuppe generally refers to the air guiding device at truck or the driver's cabin top of pulling the car, the top of engine generally all has similar guiding device, mainly used protection engine, current kuppe is mostly through the bolt fastening, it is very troublesome that the later maintenance is changed, thereby reduce maintenance efficiency, and simultaneously, kuppe that present engine was used is because the top surface with the engine is too laminated, lead to the unable effectual heat dissipation that dispels of engine, serious still can make the inside high emergence danger of temperature of engine, therefore, a kuppe for turbine engine convenient to install has practical value very much.
Disclosure of Invention
It is an object of the present invention to provide a nacelle for a turbine engine that is easy to install to solve the problems set forth in the background above.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a kuppe for turbine engine convenient to installation includes the fixed plate, the fixed plate top is provided with the base, base inner chamber bottom is provided with the blotter, the blotter top is provided with outer protecting casing, outer protecting casing inner chamber is provided with the engine body, outer protecting casing bottom, blotter and base bottom, fixed plate all run through and are provided with unanimous through-hole, it all is provided with the L template to control the terminal surface top, outer protecting casing top cup joints and is provided with the dismantlement kuppe.
Preferably, dismantle the kuppe and include the kuppe body, kuppe body central authorities run through and are provided with the air guide hole, the left and right sides in kuppe body top all is provided with fan groove, and is two sets of fan tank inner chamber all is provided with the fan of breathing in, and is two sets of fan tank bottom portion all runs through and is provided with the mounting hole, and is two sets of the mounting hole inner chamber all is provided with the air duct, kuppe body top and two sets of fan groove corresponding position all are provided with the dust removal net.
Preferably, spring grooves are transversely formed in the bottoms of the left side and the right side of the air guide sleeve body, inner cavities of the spring grooves are transversely connected with one ends of springs, the other ends of the springs are connected with arc heads, and holes communicated with the air guide pipes are uniformly formed in the bottoms of the inner cavities of the fan grooves.
Preferably, the two groups of L-shaped plates are transversely provided with buckling holes matched with the arc heads in a penetrating mode, and the two groups of arc heads are respectively movably inserted into the inner cavities of the two groups of matched buckling holes.
Preferably, the two groups of dust removing nets are made of stainless steel materials and are movably connected with the top of the air guide sleeve body through screws.
Preferably, base and fixed plate are the metal material, just the fixed plate and the base inside and outside wall all brushed the anti-rust paint layer, outer protecting shell top is uncovered setting.
Compared with the prior art, the invention has the beneficial effects that: a convenient-to-mount air guide sleeve for a turbine engine is provided, wherein the device realizes the buffer and shock absorption of bumping vibration generated in the driving process through a buffer pad arranged at the bottom of an inner cavity of a base, so that the air guide sleeve has the buffer protection effect on an engine body;
the outer protective shell, the cushion pad, the base and the fixing plate are provided with consistent through holes in a penetrating manner, so that heat inside the outer protective shell can be conveniently radiated;
the two groups of L-shaped plates are provided with buckling holes matched with the arc heads, the arc heads are quickly buckled into the matched buckling hole inner cavities through the spring action of the arc heads, so that the quick installation between the air guide sleeve body and the two groups of L-shaped plates is realized, and when the air guide sleeve is disassembled, the two groups of arc heads are pressed to respectively take out the two groups of arc heads from the matched buckling hole inner cavities, so that the air guide sleeve body and the two groups of L-shaped plates can be disassembled, and compared with a bolt disassembling mode, the disassembling method is high in efficiency;
the air guide hole penetrating through the air guide sleeve body is used for guiding the flow of the engine, the air suction fan conducts heat dissipation and ventilation treatment on the heat inside the outer protective shell, and external dust is prevented from entering the inner cavity of the fan groove through the dust removal net.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic structural view of the detachable air guide sleeve of the present invention.
In the figure: 1. a fixing plate; 2. a base; 3. a cushion pad; 4. an outer protective shell; 5. an engine body; 6. an L-shaped plate; 7. disassembling the air guide sleeve; 71. a pod body; 72. a fan groove; 73. an air suction fan; 74. an air duct; 75. a spring slot; 76. a spring; 77. an arc head; 78. an air vent; 79. a dust removal net; 8. and a through hole.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, the present invention provides a technical solution: a convenient-to-mount air guide sleeve for a turbine engine comprises a fixed plate 1, a base 2 is arranged at the top of the fixed plate 1, a cushion pad 3 is arranged at the bottom of an inner cavity of the base 2, the bumping and vibration generated in the driving process can be buffered and damped through the buffer pad 3 arranged at the bottom of the inner cavity of the base 2, thereby having the buffering and protecting function on the engine body 5, the top of the cushion pad 3 is provided with the outer protective shell 4, the inner cavity of the outer protective shell 4 is provided with the engine body 5, the bottom of the outer protective shell 4, the cushion pad 3, the bottom of the base 2 and the fixing plate 1 are all provided with consistent through holes 8, run through on outer protecting crust 4, blotter 3 and base 2 and fixed plate 1 and be provided with unanimous through-hole 8 and conveniently carry out the heat dissipation treatment to the inside heat of outer protecting crust 4, control the terminal surface top and all be provided with L template 6, outer protecting crust 4 top is cup jointed and is provided with dismantlement kuppe 7.
Referring to fig. 2, the detachable dome 7 includes a dome body 71, engine air guiding is realized through an air guide hole 78 penetrating through the dome body 71, the air guide hole 78 penetrates through the center of the dome body 71, fan grooves 72 are formed on the left and right sides of the top of the dome body 71, air suction fans 73 are arranged in the inner cavities of the two fan grooves 72, the air suction fans 73 dissipate heat and ventilate heat inside the outer casing 4, mounting holes penetrate through the bottoms of the two fan grooves 72, air guide tubes 74 are arranged in the inner cavities of the two mounting holes, dust removal nets 79 are arranged at positions of the top of the dome body 71 corresponding to the two fan grooves 72, and external dust is prevented from entering the inner cavities of the fan grooves 72 through the dust removal nets 79.
Referring to fig. 2, spring grooves 75 are transversely formed in the bottoms of the left side and the right side of the dome body 71, one ends of springs 76 are transversely connected to the inner cavities of the two groups of spring grooves 75, the other ends of the two groups of springs 76 are connected to arc heads 77, and holes communicated with air ducts 74 are uniformly formed in the bottoms of the inner cavities of the fan grooves 72, so that air flow circulation is facilitated.
Referring to fig. 1 and 2, two sets of L-shaped plates 6 are transversely provided with fastening holes matching with the circular arc heads 77 in a penetrating manner, and the two sets of circular arc heads 77 are respectively movably inserted into the two sets of matching fastening holes, the two sets of L-shaped plates 6 are provided with fastening holes matching with the circular arc heads 77, the circular arc heads 77 are quickly fastened into the matching fastening holes through the circular arc heads 77 under the action of the springs 76, so that the dome body 71 and the two sets of L-shaped plates 6 can be quickly mounted, and when the dome is dismounted, the two sets of circular arc heads 77 are pressed, so that the two sets of circular arc heads 77 are respectively taken out from the matching fastening holes, and the dome body 71 and the two sets of L-shaped plates 6 can be dismounted.
Referring to fig. 2, the two sets of dust removing nets 79 are made of stainless steel, and the two sets of dust removing nets 79 are movably connected to the top of the air guide sleeve body 71 through screws.
Referring to fig. 1, the base 2 and the fixing plate 1 are made of metal, and the inner and outer walls of the fixing plate 1 and the base 2 are both brushed with anti-rust paint layers, so that the inner and outer walls of the base 2 and the fixing plate 1 are brushed with anti-rust paint to enable the base 2 and the fixing plate 1 to have certain anti-rust capability, the service life of the base 2 and the fixing plate can be prolonged, and the top of the outer protective shell 4 is open.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. An easy-to-install air guide sleeve for a turbine engine, comprising a fixed plate (1), characterized in that: fixed plate (1) top is provided with base (2), base (2) inner chamber bottom is provided with blotter (3), blotter (3) top is provided with outer protecting crust (4), outer protecting crust (4) inner chamber is provided with engine body (5), outer protecting crust (4) bottom, blotter (3) and base (2) bottom, fixed plate (1) all run through and are provided with unanimous through-hole (8), it all is provided with L template (6) to control the terminal surface top, outer protecting crust (4) top is cup jointed and is provided with dismantlement kuppe (7).
2. The easy-to-install nacelle for a turbine engine of claim 1, wherein: dismantle kuppe (7) including kuppe body (71), kuppe body (71) central authorities run through and are provided with air guide hole (78), kuppe body (71) top left and right sides all is provided with fan groove (72), and is two sets of fan groove (72) inner chamber all is provided with air suction fan (73), and is two sets of fan groove (72) bottom all runs through and is provided with the mounting hole, and is two sets of the mounting hole inner chamber all is provided with air duct (74), kuppe body (71) top all is provided with dust removal net (79) with two sets of fan groove (72) corresponding position.
3. The easy-to-install nacelle for a turbine engine of claim 2, wherein: the air guide sleeve is characterized in that spring grooves (75) are transversely formed in the bottom of the left side and the right side of the air guide sleeve body (71), inner cavities of the two groups of spring grooves (75) are transversely connected with one ends of springs (76), the other ends of the two groups of springs (76) are connected with arc heads (77), and holes communicated with air guide pipes (74) are uniformly formed in the bottom of the inner cavities of the fan grooves (72).
4. The easy-to-install nacelle for a turbine engine of claim 2, wherein: two sets of L template (6) all transversely run through and are provided with the lock joint hole that matches with arc head (77), and two sets of arc head (77) activity grafting respectively sets up at the lock joint hole inner chamber that two sets of match.
5. The easy-to-install nacelle for a turbine engine of claim 2, wherein: the two groups of dust removing nets (79) are made of stainless steel materials, and the two groups of dust removing nets (79) are movably connected with the top of the air guide sleeve body (71) through screws.
6. The easy-to-install nacelle for a turbine engine of claim 1, wherein: base (2) and fixed plate (1) are the metal material, just fixed plate (1) and base (2) inside and outside wall have all brushed the anti-rust paint layer, outer protecting sheathing (4) top is uncovered setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010336825.6A CN111605632A (en) | 2020-04-26 | 2020-04-26 | A kuppe for turbine engine convenient to installation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010336825.6A CN111605632A (en) | 2020-04-26 | 2020-04-26 | A kuppe for turbine engine convenient to installation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111605632A true CN111605632A (en) | 2020-09-01 |
Family
ID=72196068
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010336825.6A Pending CN111605632A (en) | 2020-04-26 | 2020-04-26 | A kuppe for turbine engine convenient to installation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111605632A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08164756A (en) * | 1994-10-12 | 1996-06-25 | Toyota Motor Corp | Inlet system cooling device in transverse engine |
| US20050211487A1 (en) * | 2004-03-29 | 2005-09-29 | Kubota Corporation | Work vehicle |
| CN101905677A (en) * | 2010-01-29 | 2010-12-08 | 浙江吉利汽车研究院有限公司 | Sound-insulation structure of engine compartment |
| CN207173493U (en) * | 2017-08-02 | 2018-04-03 | 杭州电子科技大学 | A kind of dust cover of automobile engine |
| CN210174786U (en) * | 2019-04-03 | 2020-03-24 | 王棕庆 | Automobile engine protection cover |
-
2020
- 2020-04-26 CN CN202010336825.6A patent/CN111605632A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08164756A (en) * | 1994-10-12 | 1996-06-25 | Toyota Motor Corp | Inlet system cooling device in transverse engine |
| US20050211487A1 (en) * | 2004-03-29 | 2005-09-29 | Kubota Corporation | Work vehicle |
| CN101905677A (en) * | 2010-01-29 | 2010-12-08 | 浙江吉利汽车研究院有限公司 | Sound-insulation structure of engine compartment |
| CN207173493U (en) * | 2017-08-02 | 2018-04-03 | 杭州电子科技大学 | A kind of dust cover of automobile engine |
| CN210174786U (en) * | 2019-04-03 | 2020-03-24 | 王棕庆 | Automobile engine protection cover |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20200901 |
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| RJ01 | Rejection of invention patent application after publication |