JPS63127834A - Manufacture of mount member for optical equipment - Google Patents
Manufacture of mount member for optical equipmentInfo
- Publication number
- JPS63127834A JPS63127834A JP27144186A JP27144186A JPS63127834A JP S63127834 A JPS63127834 A JP S63127834A JP 27144186 A JP27144186 A JP 27144186A JP 27144186 A JP27144186 A JP 27144186A JP S63127834 A JPS63127834 A JP S63127834A
- Authority
- JP
- Japan
- Prior art keywords
- mount
- cutting
- fine hole
- lubricating oil
- hole
- 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
- 230000003287 optical effect Effects 0.000 title claims description 9
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- 238000005520 cutting process Methods 0.000 claims abstract description 22
- 238000000034 method Methods 0.000 claims abstract description 12
- 238000005553 drilling Methods 0.000 claims description 5
- 230000002093 peripheral effect Effects 0.000 claims 1
- 239000010687 lubricating oil Substances 0.000 abstract description 10
- 239000000463 material Substances 0.000 abstract description 6
- 239000003921 oil Substances 0.000 abstract description 3
- 238000005245 sintering Methods 0.000 abstract description 3
- 238000010894 electron beam technology Methods 0.000 abstract description 2
- 230000001133 acceleration Effects 0.000 abstract 1
- 238000003466 welding Methods 0.000 description 12
- 210000000078 claw Anatomy 0.000 description 7
- 239000000314 lubricant Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 238000003754 machining Methods 0.000 description 4
- 229910001220 stainless steel Inorganic materials 0.000 description 4
- UOCLXMDMGBRAIB-UHFFFAOYSA-N 1,1,1-trichloroethane Chemical compound CC(Cl)(Cl)Cl UOCLXMDMGBRAIB-UHFFFAOYSA-N 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 230000000750 progressive effect Effects 0.000 description 3
- 239000010935 stainless steel Substances 0.000 description 3
- 239000003990 capacitor Substances 0.000 description 2
- 230000004907 flux Effects 0.000 description 2
- 230000020169 heat generation Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 239000002253 acid Substances 0.000 description 1
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 238000000748 compression moulding Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 239000010730 cutting oil Substances 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000003672 processing method Methods 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は微細穴中に存在する油がマウント表面にしみ出
して生じる潤滑作用で、摺動耐久性を飛躍的に向上させ
た光学機器のマウント部材に関するものである。[Detailed Description of the Invention] [Industrial Application Field] The present invention is an optical device that dramatically improves sliding durability through the lubrication effect generated when oil present in minute holes seeps onto the mount surface. This relates to a mount member.
[従来の技術]
従来、光学機器のマウント部材はレンズマウント等との
着脱か行われるたび、金属同士か直接接触することによ
りマウント表面か摩耗するため特公昭56−15832
7公開公報に記載されている焼結含油ステンレス酸のマ
ウントか使用されていた。[Prior Art] Conventionally, each time a mount member of an optical device is attached or detached from a lens mount, etc., the mount surface is worn out due to direct contact between metals.
The sintered oil-impregnated stainless acid mount described in Publication No. 7 was used.
[発明が解決しようとしている問題点]しかしながら、
上記従来例てはステンレス製焼結材料を用いるため、引
張強さ25kg−f/■2伸び5%しか保証されず、本
発明で用いるステンレス冷間圧延材料のそれぞれ53k
g−f/mII!2.40%に比較して著しく劣るため
、例えばバヨネット爪部に衝撃力か加わると爪が欠損す
る場合もあった。また、ステンレス製焼結材料はその製
造において、高価な原料粉を使用する上粉末潤滑剤との
混合、圧縮成形、粉末潤滑剤除去、還元雰囲気中あるい
は真空中での焼成及びサイジンクと多工程を要するため
、製造コストか高価になる。また、粉じんや熱の発生が
さけられない悪環境の製造ラインになってしまうため、
安全衛生上も好ましくない。[Problem that the invention seeks to solve] However,
Since the above conventional example uses a stainless steel sintered material, the tensile strength is only 25 kg-f/■2 elongation 5%, and the stainless steel cold rolled material used in the present invention is guaranteed to have a tensile strength of only 53 kg.
g-f/mII! 2.40%, for example, when an impact force was applied to the bayonet claw, the claw could break off. In addition, the production of stainless steel sintered materials involves multiple steps such as mixing expensive raw material powder with a powder lubricant, compression molding, removing the powder lubricant, firing in a reducing atmosphere or vacuum, and sizing. Therefore, manufacturing costs are high. In addition, the production line becomes a bad environment where dust and heat generation cannot be avoided.
It is also unfavorable from a safety and health standpoint.
[問題点を解決するための手段]
本発明によれば、前記問題点を解決するために、焼結と
いうプロセスを経ずに、それ以上の強度及びそれと同等
の摺動耐久性を与える製造工程を提供する。すなわち順
送プレス加工工程て作製されたマウントリンク1とバヨ
ネットリンク2をスポット溶接で接合し、それを直接N
C旋盤てワンチャック仕上切削加工するという簡単明瞭
、清潔そして、自動化が容易な製造工程か基本になる。[Means for Solving the Problems] According to the present invention, in order to solve the above problems, a manufacturing process that provides greater strength and equivalent sliding durability without going through the sintering process is provided. I will provide a. In other words, the mount link 1 and the bayonet link 2, which were produced through a progressive press process, are joined by spot welding, and then directly connected to the N
The basic manufacturing process is one-chuck finish cutting using a C lathe, which is simple, clean, and easy to automate.
但し、この工程で製造されるマウントは着脱摺動回数2
00回において、相手方レンズマウント等の表面を損傷
させ、外観上見苦しくさせるばかりでなく、ひどい場合
はフランジバック量も変化して、カメラ機能上も損なわ
れる。そのため、本発明は、プレス加工したマウントリ
ングlにおいて、相手方マウントとの摺動部分にレーザ
あるいは電子ビームで微細穴15をあけ切削加工後そこ
に潤滑油な含ませることですぐれた着脱摺動耐久性を与
えている。この潤滑油はマウントの着脱摺動という行為
により、局部的な熱の発生あるいは負圧吸引作用により
、毛細管現象の促進がうながされて、マウント表面まで
潤滑油がしみ出してくると考えられる。However, the mount manufactured in this process has a sliding number of times of 2.
00 times, the surface of the other lens mount etc. is damaged and the appearance is not only unsightly, but in severe cases, the amount of flange back changes as well, impairing camera function. Therefore, the present invention provides excellent attachment/detachment and sliding durability by drilling a fine hole 15 with a laser or an electron beam in the pressed mount ring l at the sliding part with the other mount and impregnating it with lubricating oil after cutting. giving sex. It is thought that the action of sliding the mount on and off causes local heat generation or negative pressure suction to promote capillary action, causing the lubricant to seep out to the mount surface.
[実施例′]′ 以下にカメラ本体マウントの実施例を示す。[Example']' Examples of camera body mounts are shown below.
第1図(a)はマウントリング、(b)はバヨネット爪
リングで、ともにプレス加工で作成したものである。1
1Oトンクランクプレスを使用し、順送型で打ち抜いて
いるので加工サイクルは60 s、p、mすなわち1秒
間に1ケという高速度で図の部分が加工される。同時に
溶接用プロジェクション突起5も形成される。材質はと
もにJIS、5US304を使用したが、快削性を求め
るなら磁性は有るかJIS。FIG. 1(a) shows a mount ring, and FIG. 1(b) shows a bayonet claw ring, both of which were made by press working. 1
Since a 10-ton crank press is used and punching is performed using a progressive die, the processing cycle is 60 s, p, m, that is, the part shown in the figure is processed at a high speed of 1 piece per second. At the same time, welding projection projections 5 are also formed. We used JIS and 5US304 for both materials, but if you are looking for free machining properties, use JIS to see if it has magnetism.
Sυ5444の様なオーステナイト系と同等の耐食性を
Mo含有によりもたせたフェライト系ステンレス鋼を使
用しても良い。第2図は本発明の主旨であるレーザ穴開
工程を示している。A ferritic stainless steel, such as Sυ5444, which has corrosion resistance equivalent to austenitic stainless steel by containing Mo may also be used. FIG. 2 shows the laser drilling process which is the gist of the present invention.
この穴の形状は開口部直径0.155m、深さ0.6■
である。使用したレーザ加工機はパルス発振Nd:YA
Gレーザで、ランプ入力電圧1.2KVでレーザ発振器
内のレーザ光路中にφ10のマスクを設置して、φ20
の光束を一度φlOにしてしぼりやすい光束にしている
。集光レンズ10の焦点距離は35mtaで焦点マウン
トリングlの表面上に合わせ、アシストガスは圧力1k
g−f/C1+2の空気を使用している。熱射時間はl
ll5.で1秒間に10回焦射した。マウントリングl
はマウント保持部材13を利用して、DCモータ14に
より10秒間で1回転させる間に第2図(b)の様にφ
64の同心円上に100ケの穴を開けている。レンズ側
マウントは巾1 mrB、高さ0.5mmでその中心が
φ64の円形状した突起を有しており、その部分だけが
実施例のカメラ本体側に接触する構造になっている。つ
まり、実施例ではレンズ側マウントとカメラ本体側マウ
ントが接触する部分の中心線上に一列等間隔で100ケ
の微細穴が開けられている。次にマウントリング1とバ
ヨネット爪リング2を接合するプロジェクションスポッ
ト溶接工程を第3図に示す。8個所のプロジェクション
突起5が中心になる様φ10のくし型電極16を設け、
コンデンサ型スポット溶接機を使用して溶接した。この
溶接機の電源容量は10KVAでコンデンサ容量は40
.500ルFである。溶接機付属の空気プレスにより8
個所のプロジェクション突起5に均一な荷重がかかる様
全体で1トンの加圧力をかけ、280Vの電圧て溶接し
た。この時、最終的な加圧力である鍛圧は1.5トンで
あった。また、プロジェクション突起5の高さは均一な
荷重を保証するため±0.3mmの範囲にはいる様、あ
らかじめプレス加工されである。この8個所のスポット
溶接により、ナゲツト17が形成され本マウントンの強
度が保たれている。すなわち、本発明のカメラ本体マウ
ントをカメラに設置し、150m+++望遠レンズを取
付、この望遠レンズ先端を力点として、光軸と直角な8
方向に7kg−fの力を与えた後、バヨネット爪6の光
軸方向への変形量を測定すると最大3gmとなり、スポ
ット溶接を行わないでマウントリングとバヨネット爪リ
ングを4個所のビス穴4で共にビス止めしただけの構造
のマウントての結果である最大35gmに比較して大巾
に変形量をおさえることがてきた。The shape of this hole is 0.155m in opening diameter and 0.6cm in depth.
It is. The laser processing machine used is pulse oscillation Nd:YA.
With a G laser, a φ10 mask is installed in the laser optical path in the laser oscillator with a lamp input voltage of 1.2 KV, and a φ20
Once the luminous flux is changed to φlO, it becomes a luminous flux that is easy to narrow down. The focal length of the condenser lens 10 is 35 mta and is aligned on the surface of the focal mount ring l, and the assist gas is at a pressure of 1 k.
Air of g-f/C1+2 is used. The heat radiation time is l
ll5. The beam was focused 10 times per second. mount ring l
is rotated once in 10 seconds by the DC motor 14 using the mount holding member 13, as shown in FIG. 2(b).
100 holes are drilled on 64 concentric circles. The lens side mount has a circular protrusion with a width of 1 mrB and a height of 0.5 mm with a diameter of 64 mm at the center, and only that part is in contact with the camera body side of the embodiment. That is, in this embodiment, 100 fine holes are made in a row at equal intervals on the center line of the area where the lens side mount and the camera body side mount come into contact. Next, FIG. 3 shows a projection spot welding process for joining the mount ring 1 and the bayonet claw ring 2. A comb-shaped electrode 16 with a diameter of 10 mm is provided so that the eight projection projections 5 are centered.
Welded using a capacitor spot welder. The power supply capacity of this welding machine is 10KVA and the capacitor capacity is 40KVA.
.. It is 500 leF. 8 by the air press attached to the welding machine
Welding was carried out at a voltage of 280V while applying a pressure of 1 ton to the entire projection projection 5 so that a uniform load was applied to each location. At this time, the final pressing force, or forging pressure, was 1.5 tons. Further, the height of the projection protrusion 5 is pressed in advance so that it is within a range of ±0.3 mm to ensure a uniform load. By spot welding at these eight locations, a nugget 17 is formed and the strength of this mount is maintained. That is, the camera body mount of the present invention is installed on the camera, a 150m+++ telephoto lens is attached, and the tip of this telephoto lens is used as the point of emphasis, and the 8-meter angle perpendicular to the optical axis is set.
After applying a force of 7 kg-f in the direction, the amount of deformation of the bayonet claw 6 in the optical axis direction was measured to be a maximum of 3 gm, and the mount ring and bayonet claw ring could be attached to the four screw holes 4 without spot welding. The amount of deformation has been greatly suppressed compared to the maximum of 35 gm which is the result of a mount with a structure that is simply fixed with screws.
次に切削工程について第4図で説明する。第4図(A)
は切削方向を示したもので、図の下部面をつき当てにし
て最外周をチャックして切削した。取り代は内外径部分
が片側0.3mm、上端面が0.1mmである。切削条
件はNC旋盤を用いて、主軸回転数75or−p−m送
り 0.07mmでバイトは超硬を使用した。第4図(
B)(C)は切削前後の微細穴部の拡大断面図であり、
第4図(D)(E)は同じく微細穴部のマウントのラジ
アル方向にみた拡大断面図である。この図の様にレーザ
穴開は加工を行った開口部は溶融残渣18か突起物とし
て存在しているか、これは切削によって取り去られる。Next, the cutting process will be explained with reference to FIG. Figure 4 (A)
The figure shows the cutting direction, and the outermost circumference was chucked and cut with the bottom surface in the figure as the butt. The machining allowance is 0.3 mm on one side for the inner and outer diameter portions and 0.1 mm for the upper end surface. The cutting conditions were as follows: An NC lathe was used, the spindle rotation speed was 75 or-pm, the feed was 0.07 mm, and the cutting tool was made of carbide. Figure 4 (
B) and (C) are enlarged cross-sectional views of the microhole before and after cutting,
FIGS. 4(D) and 4(E) are enlarged cross-sectional views of the mount having the minute holes as seen in the radial direction. As shown in this figure, the laser-drilled openings are either left with a melted residue 18 or a protrusion, which is removed by cutting.
そして、切削後は微細穴の一部をおおう様に封止部分1
9か発生し、これか外観上穴の存在を視認しずらくする
ことに寄与し、また潤滑油を穴に含ませた後も潤滑油の
保持に役立っている。こうして切削を終えたマウントは
第5図に示されているかこれをトリクロルエタンにより
切削油を除去し、規定の潤滑油を微細穴に含油する工程
に移る。すなわち、含油工程は100℃に加熱した潤滑
油中にマウントを浸せきし真空で行った。After cutting, the sealing part 1 is placed so as to cover part of the fine hole.
9 is generated, which contributes to making it difficult to visually recognize the existence of the hole in terms of appearance, and also helps to retain the lubricant even after the hole is impregnated with lubricant. The mount that has been cut in this manner is shown in FIG. 5, and the cutting oil is removed using trichloroethane, and the process proceeds to the step of impregnating the minute holes with a specified lubricating oil. That is, the oil impregnation step was performed by immersing the mount in lubricating oil heated to 100° C. and under vacuum.
そして最後に再びトリクロルエタンにより表面付着潤滑
油の脱脂洗節を行なった。ここで使用した潤滑油は40
°Cにおける粘度か9.58 cstの流動性のある潤
滑油であった。この潤滑油の代わりに粘度30.3cs
tの高粘度のものを使用すると、潤滑効果が現われるま
で200回の着脱摺動を行なわなければならず、その間
にレンズ側マウント面が損傷してしまった。逆に粘度2
.02cstの低粘度潤滑油を使用した時は、入念なト
リクロルエタンによる脱脂洗浄を行なうと潤滑油か抜き
取られ効果が出なかった。Finally, the lubricating oil adhering to the surface was removed again using trichloroethane. The lubricant used here is 40
It was a fluid lubricating oil with a viscosity of 9.58 cst at °C. Instead of this lubricating oil, the viscosity is 30.3 cs.
When a high viscosity material of t was used, it was necessary to perform 200 attachment/detachment slides until the lubricating effect appeared, and the lens side mount surface was damaged during this time. On the other hand, viscosity 2
.. When 02cst low viscosity lubricating oil was used, the lubricating oil was removed even after careful degreasing with trichloroethane and no effect was obtained.
[発明の効果]
本発明により作製したカメラ本体マウントは順送プレス
加工という高精度加工可能でかつスピーディ−な加工手
段を採用出来る様になったので、焼結に比べて原料が安
価な圧延板を使用できる上、後切削工程はNC旋盤によ
るワンチャック切削だけで済み、全加工を通しても著し
く加工時間か短くなった。そのため加工コストは焼結に
比べて約半分になった。さらに加工設備を見ても、清潔
な環境下で安定した製品を供給できるものばかりである
。[Effects of the Invention] The camera body mount manufactured according to the present invention can now be processed using progressive press processing, which is a speedy and high-precision processing method. In addition, the post-cutting process requires only one-chuck cutting using an NC lathe, and the machining time is significantly shortened even through the entire machining process. As a result, processing costs are approximately half that of sintering. Furthermore, looking at the processing equipment, all of them are capable of supplying stable products in a clean environment.
第1図(a)はプレス加工されたマウントリング2示す
目、
第1図(b)は同じくバヨネットリングを示す図、
第2図(a)はレーザによる穴あけの方法を示す図。
第2図(b)は穴あけされたマウントリング正面図、
第2図(c)は穴あけ部分のマウントリンク断面図、
第3図(a)はスポット溶接方法を示す図、第3図(b
)はスポット溶接前の拡大断面図。
第3図(C)はスポット溶接直後の拡大断面図、
第3図(d)はスポット溶接後の拡大断面図。
第4図(a)は切削方法を示す図、
第4図(b)は穴あけ部分の切削剪断面図、第4図(c
)は穴あけ部分の切削後断面図、第4図(d)は穴あけ
部分の切削前ラジアル方向拡大断面図、
第4図(e)は穴あけ部分の切削後ラジアル1、マウン
トリング
2、バヨネットリンク
3、座グリ
4、ビス穴
5、プロジェクション突起
6.爪
7、レーザ発振器
8、反射鏡
9、レーザ光路
10、集光レンズ
11、加工用ノズル
12、圧縮ガス流路
13、マウント保持部材
14、モータ
15、穴
16、電極チップ
17、ナゲツト
1B、溶融残渣
19、封止部分
躬
(Q)
1 口
(t))
=層=t==堀;〒=
π 3 口
(F))
(乙)
■ LF 口
↓
(し)
(q
鴬 h−回
<C)
宕 LF 口
(d)
Ce)FIG. 1(a) shows the eye of a pressed mount ring 2, FIG. 1(b) shows a bayonet ring, and FIG. 2(a) shows a method of drilling with a laser. Figure 2(b) is a front view of the mount ring with the hole drilled, Figure 2(c) is a sectional view of the mount link with the hole drilled, Figure 3(a) is a diagram showing the spot welding method, Figure 3(b)
) is an enlarged cross-sectional view before spot welding. FIG. 3(C) is an enlarged sectional view immediately after spot welding, and FIG. 3(d) is an enlarged sectional view after spot welding. Fig. 4(a) is a diagram showing the cutting method, Fig. 4(b) is a cutting shear cross-section diagram of the drilling part, and Fig. 4(c) is a diagram showing the cutting method.
) is a sectional view of the drilled part after cutting, Figure 4(d) is an enlarged cross-sectional view of the drilled part in the radial direction before cutting, and Figure 4(e) is the radial 1, mount ring 2, bayonet link 3 after cutting of the drilled part. , counterbore 4, screw hole 5, projection protrusion 6. Claw 7, laser oscillator 8, reflector 9, laser optical path 10, condenser lens 11, processing nozzle 12, compressed gas flow path 13, mount holding member 14, motor 15, hole 16, electrode chip 17, nugget 1B, melting Residue 19, sealing part (Q) 1 mouth (t)) = layer = t = = moat; C) 宕LF 口(d) Ce)
Claims (1)
部材の外周端面の光軸同心円上に 微細穴をあける穴開工程と (ii)前記第1及び第2マウント部材を固定後に前記
微細穴を設けた面を含む面を切削し 寸法出しをする工程 (iii)前記寸法出ししたマウント部材の微細穴中に
含油する工程 上記(i)(ii)(iii)を含むことを特徴とする
光学機器のマウント部材の製造方法。[Scope of Claims] (i) A step of forming a two-piece mount member and drilling a fine hole on an optical axis concentric circle on the outer peripheral end surfaces of the first and second mount members; and (ii) the first and second mounts. After fixing the member, a step of cutting the surface including the surface with the micro-holes to determine the dimensions (iii) A step of impregnating the micro-holes of the mount member with the dimensions described in (i), (ii), and (iii) above. A method of manufacturing a mount member for an optical device, the method comprising:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP27144186A JPS63127834A (en) | 1986-11-14 | 1986-11-14 | Manufacture of mount member for optical equipment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP27144186A JPS63127834A (en) | 1986-11-14 | 1986-11-14 | Manufacture of mount member for optical equipment |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS63127834A true JPS63127834A (en) | 1988-05-31 |
Family
ID=17500065
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP27144186A Pending JPS63127834A (en) | 1986-11-14 | 1986-11-14 | Manufacture of mount member for optical equipment |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63127834A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2658309A1 (en) * | 1990-02-14 | 1991-08-16 | Asahi Optical Co Ltd | ASSEMBLY FOR MOUNTING OPTICAL DEVICES. |
US5274413A (en) * | 1990-02-14 | 1993-12-28 | Asahi Kogaku Kogyo Kabushiki Kaisha | Mount assembly of optical devices |
-
1986
- 1986-11-14 JP JP27144186A patent/JPS63127834A/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2658309A1 (en) * | 1990-02-14 | 1991-08-16 | Asahi Optical Co Ltd | ASSEMBLY FOR MOUNTING OPTICAL DEVICES. |
US5274413A (en) * | 1990-02-14 | 1993-12-28 | Asahi Kogaku Kogyo Kabushiki Kaisha | Mount assembly of optical devices |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20230191543A1 (en) | System and method to perform dissimilar operations in a single machine | |
US20070246372A1 (en) | Electrochemical Machining Tool and Method for Machining a Product Using the Same | |
US20070029290A1 (en) | Method for the plasma, laser or electron beam welding of identical or different materials with a tendency for excessive hardening, with copper or a copper alloy as a filler material | |
CN108057952B (en) | Electron beam welding method for thin-wall part with large length-diameter ratio | |
CN101143402A (en) | Screw plunger welding composite connecting method for adhesive joint repair | |
JP3305735B2 (en) | Manufacturing method of high strength brazing joint | |
CN108817646A (en) | A method of using linear friction welding technique welding austenitic alloy steel and preparing non magnetic drill collar | |
CN108161000A (en) | A kind of large complicated metal component increases material and machining joint preparation process | |
JPS63127834A (en) | Manufacture of mount member for optical equipment | |
CN110788465A (en) | Electron beam welding method for TA15 and TC31 dissimilar titanium alloy materials | |
JP2020011276A (en) | Dissimilar material joint structure manufacturing method and dissimilar material joint structure | |
CN115570291A (en) | Micro-distance high-frequency vibration collision welding method | |
CN108857033A (en) | The electron beam single face welding and double face shaping process of class component is led in a kind of 1Cr18Ni9Ti, TA2 space flight | |
CN111390386B (en) | Laser stitch welding method compatible with material pressing gap | |
JPH09159025A (en) | Through hole boring method for deformed wire member with groove for ol ring in internal combustion engine | |
CN115055908A (en) | Repair method for thin-wall revolving body structure | |
CN112475808B (en) | Process suitable for industrial production of aluminum alloy/steel composite structural member and application | |
Olowinsky et al. | Laser beam microwelding in the watch industry | |
JPH05285739A (en) | Manufacture of in-place mated part | |
KR100290572B1 (en) | Lightweight Ram for Improved Bodybuilders | |
JPH01113189A (en) | Manufacture of ceramic part having fine hole | |
US5254831A (en) | Method of manufacturing bobbins for sewing machine | |
KR100869416B1 (en) | Method of manufacturing sintered oil-retaining bearing | |
JPH02251391A (en) | Laser beam machining method for ceramics | |
JPH0428490A (en) | Laser beam hole machining method for ceramics |