JPS6125999A - Turbofan - Google Patents
TurbofanInfo
- Publication number
- JPS6125999A JPS6125999A JP14595784A JP14595784A JPS6125999A JP S6125999 A JPS6125999 A JP S6125999A JP 14595784 A JP14595784 A JP 14595784A JP 14595784 A JP14595784 A JP 14595784A JP S6125999 A JPS6125999 A JP S6125999A
- Authority
- JP
- Japan
- Prior art keywords
- plate
- boss
- base plate
- underside
- circular
- 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
Abstract
Description
【発明の詳細な説明】
改良に関し、その目的とする所は極度に軽量化し、しか
も強度に於ては従来の相当厚さの構成のものに匹敵、或
はそれ以上の強度のものを安価に提供せんとしたもので
ある。[Detailed Description of the Invention] The purpose of the improvement is to extremely reduce the weight, and to produce a product at a low cost that is comparable in strength to, or even stronger than, the conventional construction with a considerable thickness. This is what we intended to provide.
即ち一例である図面に付いて説明すると、下側の基板(
11及び上側の円径環状板(2)をSPG鋼板厚さ0.
.3m/mとし、その間に同じ<SPG鋼板厚さ0.3
%の翼片(3)を多数上下板に各2個所又は3個所取
付ける。その取付法は各翼片(3)の上下両側に差込み
片(4)を設け、この差込み片を上下板(II +21
に設けた差込み孔に差込み、その先を突出せしめ、その
突出部(5)を上下板にかしめて固着したものである。In other words, to explain the drawing as an example, the lower substrate (
11 and the upper circular annular plate (2) are SPG steel plates with a thickness of 0.
.. 3m/m, and the same < SPG steel plate thickness 0.3
% wing pieces (3) are attached to the upper and lower plates in two or three places each. The installation method is to provide insert pieces (4) on both the upper and lower sides of each wing piece (3), and attach these insert pieces to the upper and lower plates (II +21
It is inserted into an insertion hole provided in the holder, the tip thereof is made to protrude, and the protruding part (5) is caulked and fixed to the upper and lower plates.
尚アルミニウム板の場合でも基板と環状板は05〜06
%翼片は06〜08%程度で満足すべきものが得られる
。In addition, even in the case of an aluminum plate, the substrate and annular plate are 05 to 06.
Satisfactory results can be obtained with a percentage of wing pieces of about 06 to 08%.
本案は上記の如く上下板tll +21及び翼片(3)
とも、その構成に要するSPG鋼板は総て厚さ03m/
mのものを使用して、従来のものに比し極度に軽量化し
たものであるが、強度を得るため下側の基板の外縁を円
形又は半円形のカール(6)を設けると共にボス(7)
の周辺に1重又は2重のビード(8)を同一方向又は反
対方向へ突設するか、或は又中央部に第4図の如くビー
ド(8)と補強板(9)を共用し、該補強板は基板と重
ねてボス(7)によりかしめて強度を出したもので、薄
板にも拘らず、その強度は従来一般に製作されていた基
板及び環状板厚さ1.2%、翼片1,0%のものによる
構成のファンに匹敵する以上で極薄板に拘らず基板外−
周にカールを施したため板材−全体に張力を与えると共
にビード等の附加効果により、ひずみ発生も解消され、
強靭且つ軽快なものと成り、従って材料節約等により安
価にして、しかも性能良好な実用性のあるターボファン
が得られるものである。As mentioned above, the main plan is the upper and lower plates tll +21 and wing pieces (3)
In both cases, the SPG steel plates required for the configuration are all 03m thick.
This is extremely lightweight compared to the conventional one, but in order to obtain strength, the outer edge of the lower board is provided with a circular or semicircular curl (6) and a boss (7). )
A single or double bead (8) is provided around the periphery in the same direction or in the opposite direction, or a bead (8) and a reinforcing plate (9) are shared in the center as shown in Fig. 4, The reinforcing plate is stacked with the board and caulked with a boss (7) to give it strength.Although it is a thin plate, its strength is higher than that of the conventionally manufactured board, annular plate with a thickness of 1.2%, and a wing piece. It is more than comparable to a fan with a configuration of 1.0%, and even though it is an ultra-thin board, there is no outside of the board.
The curling around the periphery gives tension to the entire plate material, and the additional effects of beads etc. eliminate the occurrence of distortion.
This makes it possible to obtain a practical turbo fan that is strong and light, and can therefore be made inexpensive by saving materials and has good performance.
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図は同上の正面図で半面を断面にて示す。第3
図及び第4図はビード又は補強板及びカールの設は方等
を示した一部の断面図である。
尚図面に於て(1)・・・基 板
(2)・・・環状板
(3)・・・翼 片
(4)・・翼片の差込み片
(5)・・・差込み片の突出部
(6)・・・カール
(7)・・・ボ ス
(8)・・ビード
(9)・補強板The drawings show an example of the implementation of the present invention, and FIG. 1 is a plan view, and FIG. 2 is a front view of the same, with half of the surface shown in cross section. Third
This figure and FIG. 4 are partial cross-sectional views showing the arrangement of beads or reinforcing plates and curls. In the drawings, (1)...Substrate (2)...Annular plate (3)...Blade piece (4)...Blade piece insertion piece (5)...Protrusion part of insertion piece (6)...Curl (7)...Boss (8)...Bead (9)/Reinforcement plate
Claims (1)
射状に固着成形した遠心形ターボファンに於て、下側の
基板の中央部に軸受ボスを取付け板の厚さ0.3m/m
とし、外周縁を円形又は半円形のカールを施し、該ボス
の外側には一重又は二重の環状ビードを同一方向又は反
対方向に突設或は補強板をボスと一体に固着し、上下板
の間に多数の厚さ0.3m/mの翼片を等間隔にて放射
状に各上下2個所又は3個所を上下板にかしめて固定構
成したことを特徴とする薄板構成によるターボファン。In a centrifugal turbo fan in which a large number of blades are fixed and molded radially between the lower board and the upper annular plate, a bearing boss is attached to the center of the lower board and the thickness of the plate is 0. .3m/m
The outer periphery of the boss is curled in a circular or semicircular manner, and a single or double annular bead is provided on the outside of the boss in the same direction or in the opposite direction, or a reinforcing plate is fixed integrally with the boss, and there is a space between the upper and lower plates. A turbo fan having a thin plate structure, characterized in that a large number of blades having a thickness of 0.3 m/m are radially fixed at equal intervals by caulking two or three upper and lower points to the upper and lower plates.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14595784A JPS6125999A (en) | 1984-07-16 | 1984-07-16 | Turbofan |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP14595784A JPS6125999A (en) | 1984-07-16 | 1984-07-16 | Turbofan |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6125999A true JPS6125999A (en) | 1986-02-05 |
Family
ID=15396940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP14595784A Pending JPS6125999A (en) | 1984-07-16 | 1984-07-16 | Turbofan |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6125999A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10500427B2 (en) | 2014-06-27 | 2019-12-10 | Anvil International, Llc | Adjustable bracket and hub for flexible hose support |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5669498A (en) * | 1979-10-22 | 1981-06-10 | Hitachi Ltd | Cooling fan for rotary motor |
JPS5847197A (en) * | 1981-09-17 | 1983-03-18 | Akaishi Kinzoku Kogyo Kk | Turbofan |
-
1984
- 1984-07-16 JP JP14595784A patent/JPS6125999A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5669498A (en) * | 1979-10-22 | 1981-06-10 | Hitachi Ltd | Cooling fan for rotary motor |
JPS5847197A (en) * | 1981-09-17 | 1983-03-18 | Akaishi Kinzoku Kogyo Kk | Turbofan |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10500427B2 (en) | 2014-06-27 | 2019-12-10 | Anvil International, Llc | Adjustable bracket and hub for flexible hose support |
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