JPS5847197A - Turbofan - Google Patents
TurbofanInfo
- Publication number
- JPS5847197A JPS5847197A JP14550881A JP14550881A JPS5847197A JP S5847197 A JPS5847197 A JP S5847197A JP 14550881 A JP14550881 A JP 14550881A JP 14550881 A JP14550881 A JP 14550881A JP S5847197 A JPS5847197 A JP S5847197A
- Authority
- JP
- Japan
- Prior art keywords
- disk
- washer
- holes
- disc
- boss
- 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
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は遠心形ターボファンの基台となる円板の開発に
関し、その目的とするF″JTは狂いを生じない強靭な
円板を設け、耐永久的な理想的ターボファンを得んとし
たものである。[Detailed Description of the Invention] The present invention relates to the development of a disk that serves as the base of a centrifugal turbo fan. I was trying to get a turbo fan.
即ち一例である図面について説明すると、基台となる円
板il+の周縁を下方に折曲げ又はプレス加工等による
収り出し状態の加工法等により、曲線(21に成形した
ことを特徴としたもので、このように成形した円板(1
)の上面に多数の翼片(X3)を中心から外方へ放射状
に裏側でかしめ(81によって植設し、中心部にボス孔
+41 ff:打抜き、このボス孔の上下に適当厚さの
座金(5)ヲ当がい、この座金と円板とをボス(6)の
嵌挿がしめによって固定したものである。尚座金(51
と円板(1)とは円板に一個所又は数個所の透孔又は凹
陥部を設け。That is, to explain the drawing which is an example, the peripheral edge of the disc il+ serving as the base is bent downward or pressed, etc., and the shape is formed into a curved line (21). The disk formed in this way (1
) A large number of wing pieces (X3) are caulked radially outward from the center on the back side (planted by 81, with a boss hole in the center + 41 ff: punched, and washers of appropriate thickness are placed above and below this boss hole) (5) This washer and the disk are fixed by fitting and tightening the boss (6).
And disc (1) is a disc with one or several holes or recesses.
座金には円板の透孔個所に合せて下方に嵌合用の突出部
(71ヲ設け、この座金の突出部と円板の透孔又は凹陥
部とklli合し、ボスかしめによって圧着すれは円板
中央部は更に強固となり円板の曲げ周縁と中央部の上記
加工によって将来変形を生じない真平な円板を保持する
ものである。The washer is provided with a protrusion (71) for fitting downwardly in line with the through-hole of the disc, and the protrusion of the washer and the through-hole or concave part of the disc fit together, and the crimping is done in a circular manner by caulking the boss. The central portion of the plate is further strengthened, and the bending of the peripheral edge and the center portion of the disk as described above maintains a flat disk that will not be deformed in the future.
本発明は上記の如く遠心形ターボファンに於て、使用中
性能が低下することの原因は、この円板の変形によるこ
とが多い。即′ち従来のターボファンの円板はコストダ
ウンの点モするカ一般に子機は抜きっばなしのものを使
用していることが通例で、そのため便用中又は使用前に
於ても円板にひづみが出やすく変ヤするので翼片がケー
シング等に対応し゛なくなり、その結果性能不良となる
ことが多い。このような点を研死し且つ解消するため本
発明の如く基台となる円板の周#sを同程度に折曲げ加
工を施したので薄板に拘らず補強され長く使用しても狂
いか生ずることなく理想的なターボファンが得られたも
のである。As described above, in the present invention, in a centrifugal turbo fan, the deterioration in performance during use is often caused by deformation of the disk. In other words, in order to reduce costs, it is common for conventional turbofan discs to be used as cordless units. As the blades are prone to distortion and deformation, the blades cannot accommodate the casing, etc., which often results in poor performance. In order to eliminate this problem, the circumference #s of the disc serving as the base is bent to the same extent as in the present invention, so it is reinforced regardless of the thickness of the plate and will not go out of order even if used for a long time. An ideal turbo fan was obtained without this problem.
図面゛は本発明実施の一例を示したもので、第1図は平
面図、第2図は同上の半面を断面とした側面図で翼片は
省略した@第3図は第1図の底面図で上面の翼片をかし
めによって殖設した状態を示す。
尚図面に於てfi+・・・円板
(21・・・同上周縁の折曲げによる曲縁(:31・・
・翼片
(41・・・ボスの取付孔
(51・・・座金
(61・・・ボス
(7)・・・座金に設けた嵌合用突出部(81・・・翼
片のかしめThe drawings show an example of the implementation of the present invention; Fig. 1 is a plan view, and Fig. 2 is a side view of the same half-section, with the wing pieces omitted; Fig. 3 is the bottom view of Fig. 1. The figure shows the state in which the upper wing pieces have been installed by caulking. In the drawings, fi+...Disc (21...Curved edge due to bending of the same periphery (:31...
- Wing piece (41...Boss mounting hole (51...Washer (61...Boss (7)...Protrusion for fitting provided on the washer (81...Caulking of the wing piece)
Claims (1)
ターボファンに於て、該円板の周縁部を少し下方に折曲
げ又は絞り加工等によって曲縁に成形し上面に翼片を略
放射状にかしめ、その他の方法によって植設し、その中
央部に設けたボス取付孔に上下から適当厚さの座金を当
がい、これをボスによって該座金と円板とを下面に於て
かしめて固定したことを特徴とするターボファン。In a centrifugal turbo fan constructed by installing blades radially on a single disc, the peripheral edge of the disc is bent slightly downward or drawn into a curved edge, and the top surface is shaped into a curved edge. The wing pieces are swaged approximately radially and installed using other methods, and washers of appropriate thickness are applied from above and below to the boss mounting hole provided in the center, and the bosses are used to attach the washers and the disk to the bottom surface. A turbo fan characterized by being fixed by caulking.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14550881A JPS5847197A (en) | 1981-09-17 | 1981-09-17 | Turbofan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14550881A JPS5847197A (en) | 1981-09-17 | 1981-09-17 | Turbofan |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5847197A true JPS5847197A (en) | 1983-03-18 |
Family
ID=15386867
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14550881A Pending JPS5847197A (en) | 1981-09-17 | 1981-09-17 | Turbofan |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5847197A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6125999A (en) * | 1984-07-16 | 1986-02-05 | Akaishi Kinzoku Kogyo Kk | Turbofan |
JPS6259798U (en) * | 1986-10-13 | 1987-04-14 | ||
JPS62223496A (en) * | 1986-03-25 | 1987-10-01 | Akaishi Kinzoku Kogyo Kk | Turbo fan |
-
1981
- 1981-09-17 JP JP14550881A patent/JPS5847197A/en active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6125999A (en) * | 1984-07-16 | 1986-02-05 | Akaishi Kinzoku Kogyo Kk | Turbofan |
JPS62223496A (en) * | 1986-03-25 | 1987-10-01 | Akaishi Kinzoku Kogyo Kk | Turbo fan |
JPS6259798U (en) * | 1986-10-13 | 1987-04-14 |
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