CN108423182A - Helicopter short limb with condenser assembly - Google Patents
Helicopter short limb with condenser assembly Download PDFInfo
- Publication number
- CN108423182A CN108423182A CN201810399623.9A CN201810399623A CN108423182A CN 108423182 A CN108423182 A CN 108423182A CN 201810399623 A CN201810399623 A CN 201810399623A CN 108423182 A CN108423182 A CN 108423182A
- Authority
- CN
- China
- Prior art keywords
- short limb
- shell
- condenser
- ontology
- air duct
- 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.)
- Granted
Links
- 238000005192 partition Methods 0.000 claims abstract description 9
- 238000009423 ventilation Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 abstract description 7
- 238000004378 air conditioning Methods 0.000 abstract description 5
- 238000009434 installation Methods 0.000 abstract description 4
- 238000012546 transfer Methods 0.000 abstract description 3
- 230000007613 environmental effect Effects 0.000 description 5
- 238000012913 prioritisation Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003507 refrigerant Substances 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Other Air-Conditioning Systems (AREA)
- Duct Arrangements (AREA)
Abstract
The invention discloses a kind of helicopter short limbs with condenser assembly, including short limb ontology, condenser, air duct, wind turbine and anti-collision net；It is equipped with cavity in short limb ontology and cavity is divided into the partition board of inner chamber body and outer chamber, partition board is equipped with through-hole；The shell of short limb ontology is equipped with the through-hole being connected with outer chamber；The through hole on short limb ontology shell is arranged in anti-collision net；Air duct is the cylinder for the both ends open being arranged in outer chamber, and the shell of one end and short limb ontology is connected, and the through-hole on short limb ontology shell is contained within；The other end and condenser are connected；Wind turbine setting is fixedly linked in air duct with the shell of short limb ontology, and for the air in outer chamber to be passed sequentially through condenser, air duct, the through-hole on short limb ontology shell are discharged outwardly.The configuration of the present invention is simple, intensity is reliable, good effect of heat exchange, easy for installation；Solve the problems, such as helicopter air-conditioning condenser sidewind tissue have some setbacks, heat transfer effect it is poor.
Description
Technical field
The present invention relates to helicopter air-conditioning system more particularly to a kind of helicopter short limbs with condenser assembly.
Background technology
In recent years, helicopter is more and more extensive in the application of rescue, law enforcement, agricultural, military affairs, communications and transportation etc..Companion
With the development of helicopter, airborne high-power electronic device is increasing, and driver and conductor requires the comfort of cabin and electricity
The requirement of sub- equipment cooling increasingly improves, and the importance of helicopter environmental control system is more and more prominent.And the external high performance people
With and military helicopter be equipped with the more perfect environmental control system of performance, therefore the helicopter environmental control system tool that domestic development is mating
It is significant.
Compared with fixed wing aircraft, helicopter flight height is relatively low, and flying speed is slower, and does not need cabin pressurization.Separately
Outside, helicopter environmental control system is generally installed to have designed and complete and on the type that has produced.And at the beginning of design, Duo Shuozhi
There is no the panelties for considering environmental control system for the machine of liter, and system weight and installation space are limited, therefore in design helicopter ring control
When system, system effectiveness should be improved while reducing system weight as far as possible.
It is reported that the existing existing air-conditioning refrigeration system of helicopter, there are refrigerating capacity deficiency, systems bulky, installation are complicated
The shortcomings of.It is that condenser side air current composition has some setbacks wherein to lead to one of the reason of refrigerating capacity deficiency, does not make full use of condenser
Heat exchange area, air and condenser heat transfer effect are poor.
Invention content
The technical problem to be solved by the present invention is to for defect involved in background technology, provide a kind of with cold
The helicopter short limb of condenser component.
The present invention uses following technical scheme to solve above-mentioned technical problem：
Helicopter short limb with condenser assembly, including short limb ontology, condenser, air duct, wind turbine and anti-collision net；
It is equipped with cavity in the short limb ontology and cavity is divided into the partition board of inner chamber body and outer chamber, is set on the partition board
It is useful for the through-hole of inner chamber body and outer chamber ventilation；
The shell of the short limb ontology is equipped with the through-hole being connected with the outer chamber；
The through hole on short limb ontology shell is arranged in the anti-collision net, for preventing foreign matter from entering short limb ontology；
The air duct is the cylinder for the both ends open being arranged in the outer chamber, and the shell of one end and the short limb ontology is solid
Even, the through-hole on short limb ontology shell is contained within；The other end and the condenser are connected；
The wind turbine setting is fixedly linked in the air duct with the shell of short limb ontology, is used for the sky in the outer chamber
Gas passes sequentially through condenser, air duct, the through-hole on short limb ontology shell are discharged outwardly.
The further prioritization scheme of helicopter short limb of condenser assembly is carried as the present invention, the air duct passes through several
The shell of mounting bracket and the short limb ontology, condenser are connected；
The mounting bracket includes a root long arm and two galianconism, and two galianconism are separately positioned on long-armed both ends, and equal and institute
It states long-armed vertical；The outer wall in the described long-armed and described air duct is connected, and the shell of a galianconism and short limb ontology is connected, another short
Arm and the condenser are connected.
The further prioritization scheme of helicopter short limb of condenser assembly, of the mounting bracket are carried as the present invention
Number is 4.
The further prioritization scheme of helicopter short limb of condenser assembly is carried as the present invention, the air duct is two side ends
The square prism in face.
The present invention has the following technical effects using above technical scheme is compared with the prior art：
1. simple in structure, intensity is reliable, good effect of heat exchange, easy for installation；
2. solve the problems, such as helicopter air-conditioning condenser sidewind tissue have some setbacks, heat transfer effect it is poor.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the setting schematic diagram of anti-collision net in the present invention.
In figure, 1- short limb ontologies, 2- condensers, the air ducts 3-, 4- wind turbines, 5- mounting brackets, 6- anti-collision nets.
Specific implementation mode
Technical scheme of the present invention is described in further detail below in conjunction with the accompanying drawings：
The present invention can be embodied in many different forms, and should not be assumed that be limited to the embodiments described herein.On the contrary, providing
These embodiments will give full expression to the scope of the present invention to keep the disclosure thoroughly and complete to those skilled in the art.
In the accompanying drawings, for the sake of clarity it is exaggerated component.
As shown in Figure 1, the invention discloses a kind of helicopter short limb with condenser assembly, including short limb ontology 1, cold
Condenser 2, air duct 3, wind turbine 4 and anti-collision net 6；
It is equipped with cavity in the short limb ontology 1 and cavity is divided into the partition board of inner chamber body and outer chamber, is set on the partition board
It is useful for the through-hole of inner chamber body and outer chamber ventilation；
The shell of the short limb ontology 1 is equipped with the through-hole being connected with the outer chamber；
The through hole on 1 shell of short limb ontology is arranged in the anti-collision net 6, for preventing foreign matter from entering short limb ontology 1；
The air duct 3 is the cylinder for the both ends open being arranged in the outer chamber, the shell of one end and the short limb ontology 1
It is connected, the through-hole on 1 shell of short limb ontology is contained within；The other end and the condenser 2 are connected；
The setting of the wind turbine 4 is fixedly linked in the air duct 3 with the shell of short limb ontology 1, and being used for will be in the outer chamber
Air passes sequentially through condenser 2, air duct 3, the through-hole on 1 shell of short limb ontology are discharged outwardly.
The air duct 3 is connected by the shell of several mounting brackets 5 and the short limb ontology 1, condenser 2；
Several mounting brackets 5 are uniformly arranged on 3 outer wall of the air duct；
The mounting bracket 5 includes a root long arm and two galianconism, and two galianconism are separately positioned on long-armed both ends, and equal and institute
It states long-armed vertical；The outer wall in the described long-armed and described air duct 3 is connected, and the shell of a galianconism and short limb ontology 1 is connected, Ling Yigen
Galianconism and the condenser 2 are connected.
The air duct 3 could be provided as the square prism of both sides of the face, and the number of mounting bracket 5 is preferentially set as 4
It is a, it is separately positioned in the two side walls in air duct.
As shown in Fig. 2, the through hole on 1 shell of short limb ontology is arranged in anti-collision net 6, it is connected by screw in the short limb
On the shell of ontology 1.
Cavity in short limb ontology 1 is divided into inner chamber body and outer chamber two parts by partition board, can be used for installing air-conditioning system, every
Plate is equipped with ventilation hole.The present invention installs condenser component on the shell of the short limb ontology 1, and condenser assembly is mainly by condensing
Device 2, air duct 3, wind turbine 4, mounting bracket 5 form.
Cooling air is under the swabbing action of wind turbine, after the through-hole on intermediate bulkhead, blows to the condenser 2, and
It exchanges heat with the condenser 2, the refrigerant in the condenser 2 is cooled down；Air after heating flows successively through wind
After road 3, wind turbine 4, anti-collision net 6, outside discharge machine.
Those skilled in the art of the present technique are it is understood that unless otherwise defined, all terms used herein（Including skill
Art term and scientific terminology）With meaning identical with the general understanding of the those of ordinary skill in fields of the present invention.Also
It should be understood that those terms such as defined in the general dictionary should be understood that with in the context of the prior art
The consistent meaning of meaning, and unless defined as here, will not be explained with the meaning of idealization or too formal.
Above-described specific implementation mode has carried out further the purpose of the present invention, technical solution and advantageous effect
It is described in detail, it should be understood that the foregoing is merely the specific implementation mode of the present invention, is not limited to this hair
Bright, all within the spirits and principles of the present invention, any modification, equivalent substitution, improvement and etc. done should be included in the present invention
Protection domain within.
Claims (4)
1. the helicopter short limb with condenser assembly, which is characterized in that include short limb ontology（1）, condenser（2）, air duct
（3）, wind turbine（4）And anti-collision net（6）；
The short limb ontology（1）It is interior equipped with cavity and cavity to be divided into the partition board of inner chamber body and outer chamber, on the partition board
Equipped with the through-hole for inner chamber body and outer chamber ventilation；
The short limb ontology（1）Shell be equipped with the through-hole that is connected with the outer chamber；
The anti-collision net（6）It is arranged in short limb ontology（1）Through hole on shell, for preventing foreign matter from entering short limb ontology（1）；
The air duct（3）For the cylinder of the both ends open in the outer chamber, one end and the short limb ontology is arranged（1）'s
Shell is connected, by short limb ontology（1）Through-hole on shell is contained within；The other end and the condenser（2）It is connected；
The wind turbine（4）It is arranged in the air duct（3）Interior and short limb ontology（1）Shell be fixedly linked, for by the exocoel
Internal air passes sequentially through condenser（2）, air duct（3）, short limb ontology（1）Through-hole on shell is discharged outwardly.
2. the helicopter short limb according to claim 1 with condenser assembly, which is characterized in that the air duct（3）It is logical
Cross several mounting brackets（5）With the short limb ontology（1）Shell, condenser（2）It is connected；
The mounting bracket（5）Including a root long arm and two galianconism, two galianconism are separately positioned on long-armed both ends, and and
It is described long-armed vertical；The described long-armed and described air duct（3）Outer wall be connected, a galianconism and short limb ontology（1）Shell be connected,
Another galianconism and the condenser（2）It is connected.
3. the helicopter short limb according to claim 2 with condenser assembly, which is characterized in that the mounting bracket
（5）Number be 4.
4. the helicopter short limb according to claim 1 with condenser assembly, which is characterized in that the air duct（3）For
The square prism of both sides of the face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810399623.9A CN108423182B (en) | 2018-04-28 | 2018-04-28 | Helicopter winglet with condenser assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810399623.9A CN108423182B (en) | 2018-04-28 | 2018-04-28 | Helicopter winglet with condenser assembly |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108423182A true CN108423182A (en) | 2018-08-21 |
| CN108423182B CN108423182B (en) | 2023-09-26 |
Family
ID=63162075
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810399623.9A Active CN108423182B (en) | 2018-04-28 | 2018-04-28 | Helicopter winglet with condenser assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108423182B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625286A (en) * | 2018-12-13 | 2019-04-16 | 石家庄飞机工业有限责任公司 | A kind of Small General Aircraft condenser exhaust gas device |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11324672A (en) * | 1998-05-13 | 1999-11-26 | Toyota Motor Corp | Cooling device for aircraft |
| US20040165986A1 (en) * | 2002-03-30 | 2004-08-26 | Parker Danny S. | High efficiency air conditioner condenser fan with performance enhancements |
| CN103847968A (en) * | 2014-03-05 | 2014-06-11 | 北京航空航天大学 | Novel wing icing prevention system using airborne waste heat |
| CN203704209U (en) * | 2013-12-19 | 2014-07-09 | 广州精益汽车空调有限公司 | Concealed vehicle air conditioner |
| CN206155080U (en) * | 2016-10-27 | 2017-05-10 | 河源市力王实业有限公司 | Integral type electric vehicle air conditioning |
| CN107901725A (en) * | 2017-10-31 | 2018-04-13 | 珠海格力电器股份有限公司 | A kind of condenser air concentrator device and vehicle air conditioner |
-
2018
- 2018-04-28 CN CN201810399623.9A patent/CN108423182B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11324672A (en) * | 1998-05-13 | 1999-11-26 | Toyota Motor Corp | Cooling device for aircraft |
| US20040165986A1 (en) * | 2002-03-30 | 2004-08-26 | Parker Danny S. | High efficiency air conditioner condenser fan with performance enhancements |
| CN203704209U (en) * | 2013-12-19 | 2014-07-09 | 广州精益汽车空调有限公司 | Concealed vehicle air conditioner |
| CN103847968A (en) * | 2014-03-05 | 2014-06-11 | 北京航空航天大学 | Novel wing icing prevention system using airborne waste heat |
| CN206155080U (en) * | 2016-10-27 | 2017-05-10 | 河源市力王实业有限公司 | Integral type electric vehicle air conditioning |
| CN107901725A (en) * | 2017-10-31 | 2018-04-13 | 珠海格力电器股份有限公司 | A kind of condenser air concentrator device and vehicle air conditioner |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625286A (en) * | 2018-12-13 | 2019-04-16 | 石家庄飞机工业有限责任公司 | A kind of Small General Aircraft condenser exhaust gas device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108423182B (en) | 2023-09-26 |
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