Composite tube structure

• US 5,318,374 A
• Filed: 09/23/1992
• Issued: 06/07/1994
• Est. Priority Date: 09/23/1992
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Rumberger, William E.
• Primary Examiner(s): Reese, Randolph A.
• Assistant Examiner(s): KIM, HARRY CHONG HYUN
• Application Number:
  US07/948,588
• Time in Patent Office: 622 Days
• Field of Search: 403/370, 403/374, 403/43, 403/157, 403/158, 403/291, 403/404, 403/277, 464/181, 464/182, 29/446, 29/451, 29/456, 29/525.1, 285/149, 285/249, 285/255
• US Class Current: 403/277
• CPC Class Codes: F16B 4/006 Shrinkage connections, e.g. assembled with the parts being at different temperature
• CPC Class Codes: F16B 7/00 Connections of rods or tubes, e.g. of non-circular section, mutually, including resilient connections F16B11/008, F16B17/00 take precedence; umbrella frames A45B25/02; welding or soldering of connections B23K; vehicle connections in general B60D; railway couplings B61G; bicycle frames B62K; couplings for transmitting rotation F16D; couplings for tubes conveying fluids F16L
• CPC Class Codes: F16C 7/026 made of fibre reinforced resin
• CPC Class Codes: Y10T 403/4924 Inner member is expanded by longitudinally inserted element
• CPC Class Codes: Y10T 403/7056 Threaded actuator
• CPC Class Codes: Y10T 403/7069 Axially oriented

Abstract

A composite tube structure is disclosed in which the end of the composite tube is either flared out at the end or is tapered in at the end and the flared or tapered portion is accurately formed to its final dimension so as to require no machining to size. An end assembly is applied to the end of the tube which has inner and outer portions fitting precisely into the inner and outer surfaces of the end of the tube. The inner and outer end pieces are drawn axially together to secure the tube in the end assembly between the inner and outer portions under a predetermined radial stress. The tube is secured to the end assembly without the use of pins or other fasteners which require severing the fiber strands of the tube.

Claims

1. A composite tube assembly comprising:

a hollow tube of cured composite material having at least one flared end, said tube having an external flared surface and an internal flared surface, said flared end of said tube having a tapered wall thickness which tapers to a thinner wall at the end of the flared end of the tube;

a cylindrical internal end member slideably inserted in the flared end of said tube and having an externally flared surface at one end of approximately the same geometry and dimension as the internal surface of the flared end of said tube;

a hollow cylindrical external end member assembled over the flared end of said tube and the internal end member and having an internal tapered surface at one end of approximately the same geometry and dimension as the external surface of the flared end of said tube;

means for drawing said external end member and said internal end member axially together along the internal and external surfaces of the flared end of said tube for securing the flared end of said tube therebetween under a predetermined pressure; and

means for fastening said internal end member to said external end member and said tube when their axial relationship establishes a predetermined stress on the flared end of said tube.

2. The composite tube assembly according to claim 1 wherein the means for fastening and drawing said internal and external end members together axially comprises external threads on the distal end of the internal end member and matching internal threads on the distal end of the external end member, whereby threading the external end member on to the internal end member causes relative axial motion of the two end members.

3. The composite tube assembly according to claim 1 wherein the means for fastening the internal end member to the external end member comprises a plurality of pins inserted into matching holes drilled in the internal and external end members after the end members have been axially positioned.

4. The composite tube assembly according to claim 1 wherein the means for drawing the internal and external end members together axially comprises at least two semi-circular threaded holes extending axially through an internal surface of the external end member diametrically opposite each other and two matching unthreaded semicircular holes in an outer surface of the internal end member, said unthreaded holes extending only part way through said outer surface, and threaded screw members assembled in the unthreaded semicircular holes abutting the end thereof and threaded into the threaded semi-circular holes in the external end member whereby turning the screws in the threaded holes moves the end members axially relative to each other.

5. A composite tube assembly comprising:

a hollow tube of cured composite material having at least one tapered end, said tube having an external tapered surface and an internal tapered surface, said tapered end of said tube having a tapered wall thickness which tapers to a thinner wall at the end of the tapered end of the tube;

a cylindrical internal end member slideably inserted in the tapered end of said tube and having an externally tapered surface at one end of approximately the same geometry and dimension as the internal surface of the tapered end of said tube;

a hollow cylindrical external end member assembled over the tapered end of said tube and the internal end member and having an internal flared surface at one end of approximately the same geometry and dimension as the external surface of the tapered end of said tube;

means for drawing said external end member and said internal end member axially together along the internal and external surfaces of the tapered end of said tube for securing the tapered end of said tube therebetween under a predetermined pressure;

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means for fastening said internal end member to said external end member and said tube when their axial relationship establishes a predetermined stress on the tapered end of said tube.

6. The composite tube assembly according to claim 5 wherein the means for fastening and drawing said internal and external end members together axially comprises external threads on the distal end of the internal end member and matching internal threads on the distal end of the external end member, whereby threading the external end member on to the internal end member causes relative axial motion of the two end members.

7. The composite tube assembly according to claim 5 wherein the means for fastening the internal end member to the external end member comprises a plurality of pins inserted into matching holes drilled in the internal and external end members after the end members have been axially positioned.

8. The composite tube assembly according to claim 5 wherein the means for drawing the internal and external end members together axially comprises at least two semi-circular threaded holes extending axially through an internal surface of the external end member diametrically opposite each other and two matching unthreaded semicircular holes in an outer surface of the internal end member, said unthreaded holes extending only part way through said outer surface, and threaded screw members assembled in the unthreaded semicircular holes abutting the end thereof and threaded into the threaded semi-circular holes in the external end member whereby turning the screws in the threaded holes moves the end members axially relative to each other.