JPH0228033B2 - - Google Patents

Info

Publication number
JPH0228033B2
JPH0228033B2 JP60203207A JP20320785A JPH0228033B2 JP H0228033 B2 JPH0228033 B2 JP H0228033B2 JP 60203207 A JP60203207 A JP 60203207A JP 20320785 A JP20320785 A JP 20320785A JP H0228033 B2 JPH0228033 B2 JP H0228033B2
Authority
JP
Japan
Prior art keywords
ring
garter spring
seal
slit
tubular
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.)
Expired - Lifetime
Application number
JP60203207A
Other languages
Japanese (ja)
Other versions
JPS61211572A (en
Inventor
Esu Arison Robaato
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.)
JENERARU KONEKUTAASU CORP
Original Assignee
JENERARU KONEKUTAASU CORP
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 JENERARU KONEKUTAASU CORP filed Critical JENERARU KONEKUTAASU CORP
Publication of JPS61211572A publication Critical patent/JPS61211572A/en
Publication of JPH0228033B2 publication Critical patent/JPH0228033B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/02Sealings between relatively-stationary surfaces
    • F16J15/021Sealings between relatively-stationary surfaces with elastic packing
    • F16J15/022Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material
    • F16J15/024Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity
    • F16J15/027Sealings between relatively-stationary surfaces with elastic packing characterised by structure or material the packing being locally weakened in order to increase elasticity and with a hollow profile
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/32Component parts, details or accessories; Auxiliary operations
    • B29C43/36Moulds for making articles of definite length, i.e. discrete articles
    • B29C43/42Moulds for making articles of definite length, i.e. discrete articles for undercut articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
    • B29C66/114Single butt joints
    • B29C66/1142Single butt to butt joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/14Particular design of joint configurations particular design of the joint cross-sections the joint having the same thickness as the thickness of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/522Joining tubular articles
    • B29C66/5221Joining tubular articles for forming coaxial connections, i.e. the tubular articles to be joined forming a zero angle relative to each other
    • B29C66/52211Joining tubular articles for forming coaxial connections, i.e. the tubular articles to be joined forming a zero angle relative to each other for making endless tubular articles, e.g. endless inner tubes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/52Joining tubular articles, bars or profiled elements
    • B29C66/524Joining profiled elements
    • B29C66/5241Joining profiled elements for forming coaxial connections, i.e. the profiled elements to be joined forming a zero angle relative to each other
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/70Completely encapsulating inserts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0053Producing sealings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/16Sealings between relatively-moving surfaces
    • F16J15/32Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
    • F16J15/328Manufacturing methods specially adapted for elastic sealings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C2793/00Shaping techniques involving a cutting or machining operation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C53/00Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/36Bending and joining, e.g. for making hollow articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
    • B29C66/71General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/26Sealing devices, e.g. packaging for pistons or pipe joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/709Articles shaped in a closed loop, e.g. conveyor belts
    • B29L2031/7096Rings or ring-like articles
    • B29L2031/7102Toroidal articles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Gasket Seals (AREA)

Abstract

A tubular ring is formed from a suitable rubber like material. A circumferential slit 18 is formed on the periphery of the ring which communicates with the bore in the ring. Then the sides of the slit are spread apart far enough so a garter spring 22 can be inserted through the slit into the bore of the ring. The garter spring 22 is sized so it is movably mounted in the bore of the ring so it can exert the required compressive force on the finished seal. The sides of the slit are then cemented together and a fiberglass cloth 24 is cemented to the inner surface 28 of the ring to form a work contacting surface on the seal. <IMAGE>

Description

【発明の詳細な説明】 イ 産業上の利用分野 本発明は、シールの中央に配置された縦孔の中
に可動に取付けられたガーターばねを備えたリン
グ形シールの形成方法に関する。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to a method of forming a ring-shaped seal with a garter spring movably mounted in a vertical hole located in the center of the seal.

ロ 発明の構成 適当なゴム状物質から管状リングを作る。この
リングの縦孔に通じる円周スリツトをこのリング
の外周に作る。次に、このスリツトを通してリン
グの縦孔の中にガーターばねを挿入できるように
このスリツトの側面を十分に広げる。このガータ
ーばねは、リングの縦孔の中に可動に取付けられ
且つ完成シールに必要な圧縮力を働かせることが
できる大きさである。スリツトの側面は、それか
ら互いに接着し、そしてガラス繊維布をリングの
内面に接着してこのシールの工作物接触面を形成
する。
B. Structure of the invention A tubular ring is made from a suitable rubber-like material. A circumferential slit communicating with the vertical hole of this ring is made on the outer periphery of this ring. The sides of the slit are then widened sufficiently to allow the garter spring to be inserted through the slit and into the longitudinal hole of the ring. The garter spring is movably mounted within the ring well and is sized to exert the compressive force necessary for the completed seal. The sides of the slit are then glued together and a fiberglass cloth is glued to the inner surface of the ring to form the work contacting surface of the seal.

ハ 従来の技術と問題点 米国特許第4453723号に更に詳しく説明したよ
うに、航空機に於いてシールの中央に配置された
縦孔の中に可動に取付けられたガーターばねを有
するリング形ゴムシールを使う必要があり、そこ
ではこの縦孔とガーターばねはこのシールの内部
工作物接触面と離れた関係にある。この配列でシ
ールの有効寿命は長くなるだろう。
C. Prior Art and Problems As described in more detail in U.S. Pat. No. 4,453,723, an aircraft uses a ring-shaped rubber seal having a garter spring movably mounted within a vertical hole located in the center of the seal. It is necessary that the well and the garter spring be in a remote relationship with the internal workpiece contacting surface of the seal. This arrangement will increase the useful life of the seal.

しかし、従来のシール形成方法は、米国特許第
4453723号で述べたように、完成シールの公差及
び物理的特性が十分均一でないので不満足であつ
た。
However, traditional seal-forming methods are
As noted in No. 4,453,723, the tolerances and physical properties of the finished seal were unsatisfactory because they were not uniform enough.

従来のシール形成方法は、米国特許第4453723
号で述べたように、普通の押出機で成形されるべ
き管状の半硬化ゴム又はゴム状インサートを必要
とした。このインサートは必要な長さに切断し
た。次に、これも必要な長さに切つたガーターば
ねをこのインサートの縦孔の中に挿入した。この
ガーターばねの両端は、この技術分野でよく知ら
れた方法でそれらを互いに結合できるように設計
されていて、この管状リングの縦孔の中に可動に
取付けられたガーターばねを備えたリング形イン
サートを形成した。
A conventional seal forming method is described in U.S. Patent No. 4,453,723.
As mentioned in the above issue, it required a tubular semi-cured rubber or rubbery insert to be formed in a conventional extruder. This insert was cut to the required length. Next, a garter spring, also cut to the required length, was inserted into the vertical hole of the insert. The ends of the garter spring are ring shaped with the garter spring movably mounted within the longitudinal bore of the tubular ring, the ends being designed to allow them to be joined together in a manner well known in the art. An insert was formed.

次に、シリコン含浸ガラス繊維布の層を金型キ
ヤビテイの中に挿入した。それからこのリング形
管状インサートをこのガラス繊維布の上に置い
た。その後、未硬化ゴムのリング形片をこの金型
キヤビテイに挿入し、この金型を閉じた。最後
に、このゴムを硬化しシールを作るに十分の長さ
だけこの金型をオーブンの中に入れた。
A layer of silicone-impregnated fiberglass cloth was then inserted into the mold cavity. The ring-shaped tubular insert was then placed on top of the fiberglass cloth. A ring-shaped piece of uncured rubber was then inserted into the mold cavity and the mold was closed. Finally, the mold was placed in an oven long enough to cure the rubber and create a seal.

この方法は、硬化工程中、期待に反して、半硬
化ゴムインサートがガーターばねの周に無差別の
方法で収縮し、それでガーターばねがこのシール
の縦孔の中を必ずしも自由に動けないので満足で
なかつた。従つて、この方法によつて作られたシ
ールは性能特性が均一ではなかつた。
This method is unsatisfactory because during the curing process, contrary to expectations, the semi-cured rubber insert shrinks around the garter spring in an indiscriminate manner, so that the garter spring cannot necessarily move freely within the wells of this seal. It wasn't. Therefore, seals made by this method did not have uniform performance characteristics.

ニ 発明の目的 従つて、必要とされ且つ本発明の重要な目的を
含むものは、シールの中央に配置された縦孔の中
に可動に取付けられたガーターばねを備えたシー
ルの形成方法であつて、実行簡単且つ性能特性が
均一なシールを生産する方法を提供することであ
る。
D. OBJECTS OF THE INVENTION What is needed, therefore, and which comprises an important object of the present invention, is a method of forming a seal with a garter spring movably mounted within a vertical hole located centrally in the seal. The object of the present invention is to provide a method for producing seals that are easy to implement and have uniform performance characteristics.

本発明のこれやその他の目的は、以下の説明及
び図面を参照してより良く理解するとき、より明
白となろう。
These and other objects of the invention will become more apparent when better understood with reference to the following description and drawings.

ホ 実施例 第1図を参照すると、シールに適したゴム状物
質が、従来の装置の何れかによつて硬化状態で管
状に押出され、適当な長さに切断されている。次
にこの各本の材料10の両端12に接着剤をつ
け、それらを接合して中央に縦孔20が形成され
ている管状リング10を作る(第2図参照)。
EXAMPLE 1 Referring to FIG. 1, a rubber-like material suitable for sealing is extruded in the cured state into tubular shapes by any conventional apparatus and cut to the appropriate length. Next, adhesive is applied to both ends 12 of each book material 10, and these are joined to form a tubular ring 10 with a vertical hole 20 formed in the center (see FIG. 2).

次に、このリングを動力駆動回転スピンドル1
4に取付け、縦孔20に通じる円周スリツト18
ができるまでナイフ15をこのリング10の外周
16に押しつける(第3図及び第4図参照)。そ
の後、スリツト18の側面を開き、このスリツト
18の開いた側面から適当な形のリング状ガータ
ーばね22を入れる(第5図及び第6図参照)。
このガーターばね22は、それがこの縦孔20の
中にあるとき、このシール本体とは独立に動くこ
とができるように、このガーターばねの各巻が縦
孔の壁に付着しないような大きさになつている。
更に、このガーターばねの直径は、これがリング
の縦孔の中にあるとき、この完成シールに、シー
ルを形成するエラストマー材料の経時弾性減を補
償するため、ガーターばねが広い温度範囲にわた
つて温度とは独立にリングに適当な圧縮力を働か
せることができるように選ばれている。
Next, this ring is attached to the power-driven rotating spindle 1.
4 and a circumferential slit 18 communicating with the vertical hole 20.
The knife 15 is pressed against the outer periphery 16 of this ring 10 until it forms (see FIGS. 3 and 4). Thereafter, the side surface of the slit 18 is opened, and a ring-shaped garter spring 22 of an appropriate shape is inserted through the open side surface of the slit 18 (see FIGS. 5 and 6).
The garter spring 22 is sized so that each turn of the garter spring does not stick to the wall of the well 20 so that it can move independently of the seal body when it is in the well 20. It's summery.
In addition, the diameter of the garter spring is such that when it is in the ring well, the completed seal has a temperature range over a wide temperature range to compensate for the loss of elasticity of the elastomeric material forming the seal over a wide temperature range. It is chosen so that an appropriate compressive force can be applied to the ring independently of the ring.

次に、部分30の金型キヤビテイに一層以上の
リング形シリコン含浸ガラス繊維布24を挿入す
る(第7図参照)。そして、縦孔20の中にガー
ターばねを可動に取付けたリング10を、このガ
ラス繊維布24がリング10の内面28に向いて
当接するように、この金型部30に取付ける。
Next, one or more layers of ring-shaped silicone-impregnated fiberglass cloth 24 are inserted into the mold cavity of section 30 (see FIG. 7). Then, the ring 10 with the garter spring movably attached in the vertical hole 20 is attached to the mold part 30 so that the glass fiber cloth 24 faces and abuts the inner surface 28 of the ring 10.

次に、スリツト18の側面とリング10の内面
に熱反応性接着剤をつける。その後、ガラス繊維
布を適当な長さに切り取り、金型部30に金型部
46をかぶせる(第7図参照)。この金型を次に
オーブンに入れ、それがスリツト18の向き合つ
た側面を互いにしつかりと接着し、ガラス繊維布
24をリングの内面28に接着してこのシールの
工作物接触面を形成する(第10図参照)。この
配列では、ガーターばね22が、リング10を構
成するゴム状物質が“硬化”状態になつてから縦
孔20内に挿入されているので、このガーターば
ねはシールの縦孔の内壁に付着しないだろう。
Next, a heat-reactive adhesive is applied to the sides of the slit 18 and the inner surface of the ring 10. Thereafter, the glass fiber cloth is cut to an appropriate length, and the mold part 46 is placed over the mold part 30 (see FIG. 7). The mold is then placed in an oven, which firmly adheres the opposing sides of the slits 18 together and adheres the fiberglass cloth 24 to the inner surface 28 of the ring to form the work-contacting surface of the seal. (See Figure 10). In this arrangement, the garter spring 22 is inserted into the well 20 after the rubber-like material that makes up the ring 10 is in a "hardened" state, so that the garter spring does not stick to the inner wall of the seal well. right.

第7図に見られるように。各金型は、二つの合
せ部品で作られている。最初のものは、全体が円
筒形のベース部31と、このベース部から上に伸
びる、中央に配置された円筒形部33とを有する
金型部30から成る(第7図及び第8図参照)。
この上に伸びる円筒形部は、この特定の実施例で
は、直径がベース部31より小さいが、逆が真で
ある他の構成も意図している。この上に伸びる円
筒形部33の外周35は、一般に凹で、この実施
例では、究極的にダクト又はコネクタのシール面
と係合する、このシールの内面を完全に形造る役
目をする。この配列は、シール10の全内部工作
物接触面が金型部30の面35から作られるの
で、重要である。これは、このシールの内部工作
物接触面に“ばり”ができるのを防ぐ。
As seen in Figure 7. Each mold is made of two mating parts. The first consists of a mold part 30 having a generally cylindrical base part 31 and a centrally arranged cylindrical part 33 extending upward from this base part (see FIGS. 7 and 8). ).
Although this overlying cylindrical portion has a smaller diameter than the base portion 31 in this particular example, other configurations are also contemplated where the reverse is true. The outer periphery 35 of the overlying cylindrical portion 33 is generally concave and in this embodiment serves to completely define the inner surface of the seal that ultimately engages the sealing surface of the duct or connector. This arrangement is important because the entire internal workpiece contacting surface of the seal 10 is made from the face 35 of the mold section 30. This prevents "burrs" from forming on the internal workpiece contacting surfaces of the seal.

金型の第二の部分は、穴47と穴ぐり48とを
含むリング形金型部46から成る(第7図及び第
9図参照)。部分30と46は、組立てた関係で、
一つのシール用の完全な金型を形成する(第8図
参照)。
The second part of the mold consists of a ring-shaped mold section 46 containing a hole 47 and a borehole 48 (see FIGS. 7 and 9). Portions 30 and 46 are in assembled relationship;
Form a complete mold for one seal (see Figure 8).

金型部30と46を組合せるため、金型部30
は一つの円の外周上に配置された位置ぎめ面54
及び56を備える(第7図参照)。面54は、金
型部46に対する位置ぎめ面として機能する外
に、この金型キヤビテイのベースとしても役立つ
(第7図参照)。金型部46は金型部30の上に載
り、それと共同して金型キヤビテイ61を形成す
る(第9図参照)。金型部46の穴ぐり48は、
一つの円の直径上にあり且つ金型部30の面54
及び56と係合してこれらの部分30と46の結
合を保つ位置ぎめ面50及び52を有する。
In order to combine the mold parts 30 and 46, the mold part 30
is a positioning surface 54 arranged on the outer periphery of one circle.
and 56 (see FIG. 7). In addition to serving as a locating surface for mold section 46, surface 54 also serves as the base of this mold cavity (see FIG. 7). The mold part 46 rests on the mold part 30 and together forms a mold cavity 61 (see FIG. 9). The hole 48 of the mold part 46 is
on the diameter of one circle and on the surface 54 of the mold part 30
and 56 to maintain the connection of the portions 30 and 46.

積み重ねた関係で、金型部30の下面58は、
金型部46の上面59上に位置する。これは金型
キヤビテイ61を閉じ、それでこれらの金型がオ
ーブンに入れられたときシールを形成することが
できる(第8図参照)。金型部46の穴47の外
周49は、この実施例では、凹で、シールの内部
工作物接触面から遠い全外面13を完全に定める
(第8図参照)。従つて、ばりがこの外部工作物接
触面に形成される筈がない。このばりの形成除去
は、シールを仕上げるに要する労力を軽減する。
金型部46が金型部30の上に位置する組立てた
関係で、凹面35と49は互いに向き合つてこの
金型キヤビテイ61の外周限界を定める(第8図
参照)。
In stacked relationship, the lower surface 58 of the mold section 30 is
It is located on the upper surface 59 of the mold part 46. This closes the mold cavity 61 so that a seal can be formed when these molds are placed in an oven (see Figure 8). The outer periphery 49 of the hole 47 in the mold section 46 is concave in this embodiment and completely defines the entire outer surface 13 remote from the internal workpiece contacting surface of the seal (see FIG. 8). Therefore, no burrs can form on this external workpiece contact surface. This removal of burr formation reduces the effort required to finish the seal.
In assembled relation, with mold section 46 overlying mold section 30, concave surfaces 35 and 49 face each other to define the outer circumferential limits of mold cavity 61 (see FIG. 8).

各々金型部46と金型部30を含む多数の金型
を直立支持体44上に積み重ねることができ(第
9図参照)、それで多数のシールを同時に形成す
ることができる。中央に支持体受孔62が配置さ
れた閉鎖部材60は、この金型の山の上にある。
この部分は、金型部30の面58に似た形状で、
この金型の山の一番上の金型キヤビテイ61を閉
鎖する下面64を有する。
Multiple molds, each including mold section 46 and mold section 30, can be stacked on upright support 44 (see FIG. 9) so that multiple seals can be formed simultaneously. A closure member 60 with a support receiving hole 62 arranged in the center rests on this mold mound.
This part has a shape similar to the surface 58 of the mold part 30,
The mold has a lower surface 64 that closes the mold cavity 61 at the top of the mold pile.

本発明の一般的原理を使つた別のシール形成方
法は、小さな直径のシールにより適しているかも
しれない。この方法では、金型は、中央に縦孔の
あいた管状リングを形成しそのリングがその縦孔
に通じる円周スリツトをこの金型によつて形成さ
れるように設計される。リングがこの第一金型を
離れるとき、この管状ゴムリングは硬化状態にあ
る。この点で、適当な形をしたガーターばねがこ
のスリツトの開かれた側面を通してこの管状リン
グ10の縦孔の中へ挿入される。このガーターば
ね22は、それがこのシール10の縦孔20の中
にあるとき、このガーターばねの各巻が縦孔の面
に付着しないような大きさになつていて、それに
よつてこのガーターばねはシールの縦孔の中に可
動に取付けられ、且つこのシールにシールを形成
するエラストマー材料の経時弾性減を補償するた
め、広い温度範囲にわたつて温度とは独立に航空
機ダクトの表面とシール係合するのに適した圧縮
力をシールに働かせることができる。
Alternative methods of seal formation using the general principles of the present invention may be more suitable for small diameter seals. In this method, the mold is designed to form a tubular ring with a central longitudinal hole, which ring defines a circumferential slit communicating with the longitudinal hole. When the ring leaves the first mold, the tubular rubber ring is in a cured state. At this point, a suitably shaped garter spring is inserted into the longitudinal bore of the tubular ring 10 through the open side of the slit. The garter spring 22 is sized such that when it is in the well 20 of the seal 10, each turn of the garter spring does not adhere to the face of the well, so that the garter spring The seal is movably mounted within the longitudinal bore of the seal and provides temperature-independent sealing engagement with the surface of the aircraft duct over a wide temperature range to compensate for the aging loss of elasticity of the elastomeric material forming the seal. A compressive force suitable for the seal can be applied to the seal.

次に、この管状リングのスリツトの向き合つた
面とこのリングの内面に接着剤をつける。そして
このリングを第二金型に入れ、その金型はこの金
型に配置された適当な形のリング形ガラス繊維布
層を有するので、それらがリングの内面に接触す
る。この金型が閉じられ、オーブンの中に挿入さ
れるとき、熱がスリツトの向き合つた面を接合し
且つガラス繊維布をリングの内面に接着して完成
したシールを作る。
Adhesive is then applied to the faces of the tubular ring facing the slits and to the inner surface of the ring. The ring is then placed in a second mold having appropriately shaped ring-shaped fiberglass cloth layers disposed in the mold so that they contact the inner surface of the ring. When the mold is closed and inserted into an oven, heat joins the opposing sides of the slit and bonds the fiberglass cloth to the inner surface of the ring to create the finished seal.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は、このシールを作るゴム状管状材料が
押出機を出た後に適当な長さに切られた透視図
で、その材料に作られた中央の縦孔を示す。第2
図は、“Oリング”を形成するため両端が接合さ
れたゴム状管を示す。第3図は、回転スピンドル
に取付けられたリング形シールとこのシールの縦
孔に通じる円周スリツトをこのシールに切るため
に前進するナイフ刃を示す。第4図は、このシー
ルの拡大断面図で、このシールの縦孔に通じるス
リツトを示す。第5図は、このシールのスリツト
側面を開き、この縦孔にリング形ガーターばねを
挿入した後の、第4図に示したシールを示す。第
6図は、第5図に示したシールの線6−6による
断面図である。第7図は、金型キヤビテイの中に
一つ以上のガラス繊維布層の上にシールを取付け
た金型の分解断面図である。第8図は、第7図に
示した金型の二つの部品を組立てた関係にし、シ
ールをその金型キヤビテイに入れた図である。第
9図は、多数のシールが同時に作れるように金型
を互いに積み重ねた図である。第10図及び第1
1図は、完成したシールの拡大断面図で、第11
図は、適当な形の金型で作られた変形断面のシー
ルを示す。 10……管状リング、12……端、18……ス
リツト、20……縦孔、22……ガーターばね、
24……ガラス繊維布、28……内面。
FIG. 1 is a perspective view of the rubber tubular material from which the seal is made, cut to length after it exits the extruder, showing the central longitudinal hole made in the material. Second
The figure shows a rubber tube joined at both ends to form an "O-ring". FIG. 3 shows a ring-shaped seal mounted on a rotating spindle and a knife blade advanced to cut a circumferential slit in the seal leading to a longitudinal hole in the seal. FIG. 4 is an enlarged cross-sectional view of the seal showing the slit leading to the vertical hole in the seal. FIG. 5 shows the seal shown in FIG. 4 after the slit sides of the seal have been opened and a ring-shaped garter spring has been inserted into the longitudinal hole. FIG. 6 is a cross-sectional view of the seal shown in FIG. 5 taken along line 6--6. FIG. 7 is an exploded cross-sectional view of a mold with a seal installed over one or more layers of fiberglass fabric within the mold cavity. FIG. 8 is a view of the two parts of the mold shown in FIG. 7 in assembled relation and the seal placed in the mold cavity. FIG. 9 shows the molds stacked on top of each other so that multiple seals can be made simultaneously. Figure 10 and 1
Figure 1 is an enlarged cross-sectional view of the completed seal.
The figure shows a modified cross-section seal made with a suitably shaped mold. 10... Tubular ring, 12... End, 18... Slit, 20... Vertical hole, 22... Garter spring,
24...Glass fiber cloth, 28...Inner surface.

Claims (1)

【特許請求の範囲】 1 “硬化した”エラストマー材料の管を所定の
大きさに切断し、それから材料のこの長さの両端
12に接着剤をつけ、そしてそれらを互いに接合
して中央に縦孔20のある管状リング10を形成
し、次にこのリングの外周にこのリングの縦孔に
通ずるに十分な深さの円周スリツト18を切り、
それからガーターばね22を選び、そしてリング
のスリツトの側面を、このリングの縦孔にガータ
ーばねを挿入できるように十分広げ、ガーターば
ねの各巻の大きさは、このガーターばねの各巻が
縦孔の壁に付着せずそれでこの縦孔の中にあるガ
ーターばねがリングとは無関係に収縮できるよう
に選ばれ、そしてこのガーターばねの直径は、そ
れがこのリングの縦孔の中に可動に取付けられた
とき、ガーターばねが長期間広い温度範囲にわた
つて温度と独立にリングに圧縮力を働かせること
ができるように選ばれ、それからスリツトの向い
合う側面を互いに接着し、そしてリングの内面2
8に接着剤をつけ、最後にガラス繊維布24をリ
ングの該内面に接着してこのシールの工作物接触
面を形成するそれぞれの工程を含むシールの形成
方法。 2 管状の“硬化した”ゴム状材料から管状リン
グ10を形成し、そのリングはこの管状リングの
縦孔20に通じるリング外周の円周スリツト18
を通し、次にガーターばね22をこのリングの縦
孔に挿入できるように十分このスリツトの側面を
押し開け、このガーターばねの各巻の大きさは、
このガーターばねの各巻が管状リングの縦孔の壁
に付着しないように選ばれ、それでこのガーター
ばねはリングと無関係に収縮でき、そしてこのガ
ーターばねの直径は、それがこのリングの縦孔の
中に可動に取付けられたとき、このガーターばね
が長期間広い温度範囲にわたつて温度と独立にリ
ングに圧縮力を働かせることができるように選ば
れ、それからスリツトの向い合う側面にとリング
の内面28に接着剤をつけてスリツトの向い合う
側面を互いに接着し、最後に適当な形のガラス繊
維布24をリングのこの内面に当てそれによつて
このガラス繊維布がリングの該内面に接着されて
完成したシールの工作物接触面を形成するそれぞ
れの工程を含むシール形成方法。 3 “硬化した”シリコン含浸ゴムの管状の長さ
を選択し、それからこの管状ゴムの両端12に接
着剤をつけそしてこの管状ゴムの両端を互いに接
着して中央に縦孔20のあるリング10を作り、
それからこのリングの外周にこのリングの縦孔に
通じるように十分な深さの円周スリツト18を切
り、次にこのスリツトの側面を押し開いて縦孔の
中にガーターばね22を挿入し、このガーターば
ねの各巻の大きさは、このガーターばねの各巻が
管状リングの縦孔の壁に付着しないように選ば
れ、それでこのガーターばねはリングと無関係に
収縮でき、そしてこのガーターばねの直径は、そ
れがこのリングの縦孔の中に可動に取付けられた
とき、このガーターばねが長期間広い温度範囲に
わたつて温度と独立にリングに圧縮力を働かせる
ことができるように選ばれ、次にスリツトの向い
合う面にとリングの内面28に接着剤をつけ、そ
れからこの金型の中でリングの内面と接触する一
つ以上のガラス繊維布層24を有する金型の中へ
このリングを挿入し、その後この金型を閉じそし
てスリツトの側面が互いに接着し且つリングの内
面を覆うガラス繊維布がこのリングの内面と接着
するようにリングをオーブンの中で硬化させてこ
のシールの工作物接触面を形成する、それぞれの
工程を含むシール形成方法。
Claims: 1. Cut a tube of "cured" elastomeric material to size, then apply adhesive to each end 12 of this length of material and join them together with a longitudinal hole in the center. forming a tubular ring 10 with 20 and then cutting a circumferential slit 18 in the outer periphery of this ring of sufficient depth to pass through the longitudinal hole in the ring;
A garter spring 22 is then selected, and the sides of the slit in the ring are widened sufficiently to allow the garter spring to be inserted into the well of the ring, and each turn of the garter spring is sized so that each turn of the garter spring is against the wall of the well. The diameter of this garter spring was chosen such that it could be retracted independently of the ring so that it could be retracted independently of the ring so that it could be movably mounted in the well of this ring. When the garter spring is selected to be able to exert a temperature-independent compressive force on the ring over a wide temperature range for an extended period of time, the opposite sides of the slits are then glued together and the inner surface 2 of the ring is
A method of forming a seal comprising the steps of applying adhesive to ring 8 and finally adhering a glass fiber cloth 24 to the inner surface of the ring to form the workpiece contacting surface of the seal. 2. A tubular ring 10 is formed from a tubular "hardened" rubber-like material, which ring has a circumferential slit 18 on the outer circumference of the ring leading to a longitudinal hole 20 in the tubular ring.
, and then push the sides of this slit open enough to allow the garter spring 22 to be inserted into the longitudinal hole of this ring, the size of each turn of this garter spring being:
Each turn of this garter spring is chosen so that it does not stick to the wall of the well of the tubular ring, so that this garter spring can be contracted independently of the ring, and the diameter of this garter spring is such that it is inside the well of this ring. The garter spring is chosen so that it can exert a temperature-independent compressive force on the ring over a wide temperature range over an extended period of time, when movably mounted on the opposite sides of the slit and on the inner surface 28 of the ring. The opposite sides of the slits are glued to each other with adhesive, and finally a suitably shaped glass fiber cloth 24 is applied to this inner surface of the ring, whereby the glass fiber cloth is glued to the inner surface of the ring and the ring is completed. A method for forming a seal including steps of forming a workpiece contacting surface of the seal. 3 Select a tubular length of "cured" silicone-impregnated rubber, then apply adhesive to both ends 12 of the tubular rubber and glue the ends of the tubular rubber together to form a ring 10 with a longitudinal hole 20 in the center. Making,
Then cut a circumferential slit 18 deep enough on the outer circumference of this ring to communicate with the vertical hole of this ring, then press open the sides of this slit and insert the garter spring 22 into the vertical hole. The size of each turn of the garter spring is chosen such that each turn of the garter spring does not stick to the wall of the well of the tubular ring, so that the garter spring can be contracted independently of the ring, and the diameter of the garter spring is The garter spring is chosen so that, when it is movably mounted within the well of this ring, it can exert a compressive force on the ring over a wide temperature range for long periods of time, independent of temperature, and then the slit and the inner surface 28 of the ring, and then inserting the ring into a mold having one or more fiberglass fabric layers 24 in contact with the inner surface of the ring within the mold. , the mold is then closed and the ring is cured in an oven so that the sides of the slits adhere to each other and the fiberglass cloth covering the inner surface of the ring adheres to the inner surface of the ring to seal the workpiece contacting surface of the seal. A seal forming method including each step of forming a seal.
JP60203207A 1985-03-12 1985-09-13 Method of forming seal Granted JPS61211572A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US71085085A 1985-03-12 1985-03-12
US710850 1985-03-12

Publications (2)

Publication Number Publication Date
JPS61211572A JPS61211572A (en) 1986-09-19
JPH0228033B2 true JPH0228033B2 (en) 1990-06-21

Family

ID=24855800

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60203207A Granted JPS61211572A (en) 1985-03-12 1985-09-13 Method of forming seal

Country Status (4)

Country Link
JP (1) JPS61211572A (en)
DE (1) DE3532440A1 (en)
FR (1) FR2578940B1 (en)
GB (1) GB2172347B (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2236809B (en) * 1989-09-22 1994-03-16 Rolls Royce Plc Improvements in or relating to gas turbine engines
US5622372A (en) * 1995-10-17 1997-04-22 Nippon Reinz Co., Ltd. Metal seal ring and a method of producing the same
JP4943669B2 (en) * 2005-06-08 2012-05-30 東京エレクトロン株式会社 Vacuum device seal structure
KR102296414B1 (en) * 2014-02-07 2021-09-02 싱글 뷰이 무어링스 인크. Method for forming a sealing element from extruded thermoplastic rods
DE102016117544B4 (en) 2016-09-17 2018-07-19 Tim Chyla Device for the production of sealing rings, control device and their use in this device, use of at least one rotatably mounted disc in this device, and method for the production of sealing rings
DE202016105199U1 (en) 2016-09-17 2017-12-21 Tim Chyla Device and its use for the production of sealing rings
DE202020101533U1 (en) 2020-03-20 2020-04-22 GLAMAtronic Schweiß- und Anlagentechnik GmbH Device and its use for the production of sealing rings
FR3128504A1 (en) * 2021-10-27 2023-04-28 Safran Nacelles Propulsion assembly seal

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB948459A (en) * 1960-09-08 1964-02-05 Aerox Ltd Improvements in or relating to sealing means for filter apparatus
DE1855957U (en) * 1962-05-18 1962-08-02 Skf Kugellagerfabriken Gmbh SEAL RING.
CH425378A (en) * 1963-06-28 1966-11-30 Denso Chemie Gmbh Rolling ring seal made of expanded elastomeric plastics for sealing pipelines with bell socket pipes
FR1460993A (en) * 1965-02-13 1966-12-02 Pipe connection
GB1170766A (en) * 1965-10-21 1969-11-19 Chesterton A W Co Process of Encapsulating O-Rings
GB1103979A (en) * 1965-10-21 1968-02-21 Chesterton A W Co Composite "o" ring
FR1496536A (en) * 1966-10-13 1967-09-29 A W Cherteston Company Composite O-ring and method and apparatus for its manufacture
CH592827A5 (en) * 1974-06-26 1977-11-15 Joint Francais
FR2489463B1 (en) * 1980-08-26 1987-05-15 Gen Connector Corp ANNULAR SEAL, JOINT CONSTRUCTION METHOD, MOLDS AND DEVICE FOR CARRYING OUT SAID APPLICATION, JOINT FOR CONNECTING TWO DUCTS
US4453723A (en) * 1980-12-02 1984-06-12 General Connectors Corp. Seal
JPS588868A (en) * 1981-07-09 1983-01-19 Nichirin Gomme Kogyo Kk Hollow o-ring and manufacture thereof

Also Published As

Publication number Publication date
DE3532440A1 (en) 1986-09-25
GB2172347A (en) 1986-09-17
GB2172347B (en) 1988-03-16
JPS61211572A (en) 1986-09-19
FR2578940B1 (en) 1989-09-15
FR2578940A1 (en) 1986-09-19
GB8521477D0 (en) 1985-10-02

Similar Documents

Publication Publication Date Title
JPH0228033B2 (en)
US4755244A (en) Method of forming a seal
US2604362A (en) Process of making brushes
US5943758A (en) Fabrication of a hollow composite-material shaft having an integral collar
US2450727A (en) Method of resiliently mounting a roll on a shaft
US3647589A (en) Method of manufacturing rubber wear cover for rollers and method of applying same
US2348287A (en) Method of forming composite articles
CA2421701C (en) Method of molding a helicopter rotor blade
US3570790A (en) Method of making a kite and kite structure
US1388123A (en) Method of making hollow rubber articles
ATE43996T1 (en) PROCESS FOR MAKING A THERMOPLASTIC COMPOSITE.
US3580765A (en) Resilient o-ring and method of manufacture
ATE58333T1 (en) METHOD OF BUILDING TIRES.
US966873A (en) Method of manufacturing gaskets.
JPH0374175B2 (en)
JPS629412B2 (en)
US2734011A (en) robinson
SU1608078A1 (en) Method of joining tubes from composite materials
JPH01178001A (en) Manufacture of tube for vehicle tire
JPS61132315A (en) Manufacture of molding for vehicle
JPS58163636A (en) Manufacture of weatherstrip for use with automobile
JP2860809B2 (en) Core for manufacturing electric fusion joints
US842217A (en) Method of forming inner tubes for tires.
JPS6311578Y2 (en)
GB897222A (en) Pipe sections made of plastics and a method of making them