CN205330746U - Eccentric blast pipe that local gas -bearing rotor power device used - Google Patents

Eccentric blast pipe that local gas -bearing rotor power device used Download PDF

Info

Publication number
CN205330746U
CN205330746U CN201521037561.5U CN201521037561U CN205330746U CN 205330746 U CN205330746 U CN 205330746U CN 201521037561 U CN201521037561 U CN 201521037561U CN 205330746 U CN205330746 U CN 205330746U
Authority
CN
China
Prior art keywords
eccentric
blast pipe
bearing rotor
power device
device used
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.)
Active
Application number
CN201521037561.5U
Other languages
Chinese (zh)
Inventor
徐亮
孙伟
刘峰
海磊
王鹏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jincheng Nanjing Electromechanical Hydraulic Pressure Engineering Research Center Aviation Industry Corp of China
AVIC Jincheng Nanjing Engineering Institute of Aircraft Systems
Original Assignee
AVIC Jincheng Nanjing Engineering Institute of Aircraft Systems
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AVIC Jincheng Nanjing Engineering Institute of Aircraft Systems filed Critical AVIC Jincheng Nanjing Engineering Institute of Aircraft Systems
Priority to CN201521037561.5U priority Critical patent/CN205330746U/en
Application granted granted Critical
Publication of CN205330746U publication Critical patent/CN205330746U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Wind Motors (AREA)

Abstract

The utility model belongs to the auxiliary power system technology relates to an eccentric blast pipe that local gas -bearing rotor power device used, an eccentric blast pipe that local gas -bearing rotor power device used, and it includes: eccentric gas vent (1), baffle (2) and flange (3), characterized by, the central point that blast pipe is deviated in eccentric gas vent (1) puts, just to local gas -bearing rotor's work blade, using the exhaust orientation to lie in the upper reaches of eccentric gas vent (1) as positive direction, baffle (2), covering other inoperative blades, eccentric blast pipe passes through flange limit (3) and is connected with the volute end. The utility model discloses the local gas -bearing rotor power device gas vent size of creating of beneficial effect reducible to enough reduce the exhaust loss.

Description

A kind of eccentric exhaustor of partial admission turbine power plant
Technical field
This utility model belongs to accessory power system technology, it is possible to for aircraft emergency power plant。
Background technology
Development along with aircraft the second dynamical system synthesization, it is desirable to work turbine can work under multiple inlet air conditions, and partial admission's turbine is the effective way realizing multi-mode working。The discharge characteristic of partial admission's turbine is different from conventional full admission turbine, and air-flow accumulates near working-blade, and traditional in line structure is unfavorable for the abundant development of air-flow, thus adding discharge loss。
Summary of the invention
The purpose of the present invention: the invention provides a simple in construction, is suitable for the eccentric exhaust pipe structure of partial admission's turbine power plant。
Technical scheme: the eccentric exhaustor of a kind of partial admission turbine power plant, comprising: eccentric air vent 1, baffle plate 2 and flange 3, eccentric air vent 1 deviates the center of exhaustor, is right against the working-blade of partial admission's turbine;With discharge directions for positive direction, baffle plate 2 is positioned at the upstream of eccentric air vent 1, covers other inoperative blades, and eccentric exhaustor is connected with volute end by flange 3。
Preferably, the aperture area of eccentric air vent 1 is less than exhaustor。
The beneficial effect of the invention
Partial admission's turbine power plant air vent size can be reduced, and enough drop discharge loss。
Accompanying drawing explanation
Fig. 1 is the gas generator structure chart of this reality invention。
Wherein, 1-bias air vent, 2-baffle plate, 3-flange。
Detailed description of the invention
A kind of eccentric exhaustor sectional view such as Fig. 1 of partial admission turbine power plant。Exhaustor is connected with volute end by flange (3), and air-flow flows into from flange (3), flows out from eccentric air vent (1)。Eccentric air vent (1), not in the center of exhaustor, is right against partial admission's moving turbine blade part, is only capable of so that partial admission's moving turbine blade tail gas is discharged。Baffle plate (2) is positioned at eccentric air vent (1) upstream, covers other inoperative blades, reduces the air-flow flowing at inoperative leaf area。

Claims (2)

1. the eccentric exhaustor of partial admission's turbine power plant, comprising: eccentric air vent (1), baffle plate (2) and flange (3), it is characterized in that, the center of eccentric air vent (1) deviation exhaustor, is right against the working-blade of partial admission's turbine;With discharge directions for positive direction, baffle plate (2) is positioned at the upstream of eccentric air vent (1), covers other inoperative blades, and eccentric exhaustor is connected with volute end by flange (3)。
2. eccentric exhaustor as claimed in claim 1, it is characterised in that: the aperture area of eccentric air vent (1) is less than exhaustor。
CN201521037561.5U 2015-12-14 2015-12-14 Eccentric blast pipe that local gas -bearing rotor power device used Active CN205330746U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521037561.5U CN205330746U (en) 2015-12-14 2015-12-14 Eccentric blast pipe that local gas -bearing rotor power device used

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521037561.5U CN205330746U (en) 2015-12-14 2015-12-14 Eccentric blast pipe that local gas -bearing rotor power device used

Publications (1)

Publication Number Publication Date
CN205330746U true CN205330746U (en) 2016-06-22

Family

ID=56212780

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201521037561.5U Active CN205330746U (en) 2015-12-14 2015-12-14 Eccentric blast pipe that local gas -bearing rotor power device used

Country Status (1)

Country Link
CN (1) CN205330746U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108499232A (en) * 2017-02-24 2018-09-07 松下知识产权经营株式会社 Separator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108499232A (en) * 2017-02-24 2018-09-07 松下知识产权经营株式会社 Separator

Similar Documents

Publication Publication Date Title
NZ579817A (en) Wind turbine with inlet shroud with mixing lobes extending downstream of rotor blades, and downstream ejector shroud
CN205190327U (en) Centrifugal fan impeller of adjustable splitterr vanes
EP2685065A3 (en) A gas turbine engine
CN102673793A (en) Exhaust ejector system of airplane auxiliary power unit
CN103403298B (en) Turbine wheel, turbo machine and use thereof
EP3483395A3 (en) Inter-turbine ducts with flow control mechanisms
CN105332945A (en) Centrifugal fan impeller capable of adjusting splitting vanes
WO2015130384A3 (en) Fan nacelle inlet flow control
CN205823738U (en) Vane diffuser for centrifugal compressor
CN205330746U (en) Eccentric blast pipe that local gas -bearing rotor power device used
CN105298921B (en) U-shaped mixing diffuser between two-stage centrifugal compressor stage
CN107109960A (en) The profile portion of the guide vane of guider in turbomachinery, especially in compressor
GB201204339D0 (en) A wind turbine assembly
CN201582215U (en) Width adjusting mechanism of vaneless diffuser of turbocharger
CN208763989U (en) A kind of outlet flow-guiding structure of gas turbine blower
CN204250376U (en) A kind of Submerged Inlet structure of aircraft
US20110164966A1 (en) Method and apparatus to improve wake flow and power production of wind and water turbines
CN203285736U (en) Impeller structure installed on side hung type air blower
CN209261914U (en) Impeller wind guide chamber bypass recycling turbocharger air compressor
CN108119281A (en) A kind of new twin-jet nozzle inclined-jet turbine
CN203674837U (en) Improved generating set structure
CN107624150A (en) Guide vane for the diffuser of radial flow compressor
RU2721743C2 (en) Tunnel wind-driven power plant with rotor horizontal axis of rotation
CN205779897U (en) Centrifugal blower
CN205578349U (en) Wind structure is got to spiral case

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant