Fairing for pipes

Claim 2

A fairing for pipes and other substantially rigid structures immersed in a fluid medium, for reducing the coefficient of drag on said pipe due to relative flow thereof with respect to said fluid medium, said fairing comprising a shell of substantially rigid material forming a symmetrical structure having a nose portion and a tail portion; where (a) said nose portion has an opening along its axis to accommodate said pipe; and (b) at least said tail portion has a plurality of upstanding rib portions spaced axially along each side of said fairing and extending rearwardly from the front of said fairing, and a plurality of alternating tail portions at least between said upstanding rib portions; where aspect ratios taken at a cross-section through any of said upstanding rib portions and a cross-section through any of said alternating tail portions are similar; said aspect ratios being the ratio of length to breadth of the fairing, the breadth being the greatest width of each respective cross-section and the length of each respective cross-section being taken along the chord length thereof to the rearmost point of the cross-section where a rearward taper thereof terminates; the length and breadth, respectively, of any cross-section taken through any of said upstanding rib portions being different, in absolute terms, than the length and breadth respectively of any cross-section taken through any of said alternating tail portions of said fairing; and where each of said alternating tail portions terminates at a trailing fin portion of said fairing which extends rearwardly of said respective alternating tail portion to substantially the same distance behind the front of said fairing as said upstanding rib portions extend.

Claim 3

The fairing of claim 1 where the aspect ratio of any cross-section taken through any of said upstanding rib portions is at least equal to the aspect ratio of any cross-section taken through any of said alternating tail portions.

Claim 4

The fairing of claim 1 where said upstanding rib portions of said fairing are extended forwardly of said tail portion to enwrap at least a part of said nose portion of said fairing.

Claim 5

The fairing of claim 1 where the axial length of each of said upstanding rib portions, in the forward portion of each, is 0.5 to 1.5 times the axial length of each of said alternating tail portions in the forward portion thereof.

Claim 6

The fairing of claim 4 where the axial length of each of said upstanding rib portions, in the rearward portion of each, decreases as the distance away from the front of the fairing increases.

Claim 7

The fairing of claim 1, further comprising a pair of stabilizer plates extending between at least two adjacent upstanding rib portions near the rearward end of each, on each side of said fairing.

Claim 8

The fairing of claim 6 where said stabilizer plates extend from the endmost upstanding rib portion of said fairing at one end thereof to the endmost upstanding rib portion at the other end thereof and across the outer surfaces of said rib portions.

Claim 9

The fairing of claim 7 where said stabilizer plates overlie the places where all of said alternating tail portions between said two endmost upstanding rib portions terminate, so as to overlie the rearmost portions of each of said alternating tail portions and the foremost portions of each of said trailing fin portions.

Claim 10

The fairing of claim 8 where at least one aperture is formed through each of said trailing fin portions over which said stabilizer plates overlie.

Claim 11

The fairing of claim 9 where the rearmost edge of each of said apertures is further from the front of said fairing than the rearmost edges of said stabilizer plates.

Claim 12

The fairing of claim 9 where said shell comprises a pair of substantially identical shell halves facing each other, and having a hinge formed between the shell halves at the parting line in the nose portion thereof; and where one plate of a two-plate hinged fastener is secured to one shell half at the leading edge of each of said apertures in said trailing fin portions, and at least one pin means is secured to one of said plates and passes through said respective trailing fin portion where it may be captured by pin capturing means secured to the other of said plates.

Claim 13

The fairing of claim 11 where said shell halves are closed at each end except for the axial opening in the nose portion, and form axially extending flanges; where at least one aperture is formed through the flange at each end of said fairing and a two-plate hinged fastener is secured to one of said shell halves at each of said apertures in said flanges.

Claim 14

The fairing of claim 1, further comprising a collar fitted in the axial opening of said nose portion at at least one end of said fairing and adapted to accommodate a pipe in a central opening of said collar, where said pipe has an overall diameter less than that of said axial opening in the nose portion of said fairing.

Claim 15

The fairing of claim 13 where said collar has at least one further opening through its thickness adapted to accommodate the passage therethrough of a further pipe or the like having a dimension radially outwardly from the axis of the pipe accommodated in the central opening which is less than the difference of radii of said central opening of said collar and said axial opening in the nose portion of said fairing.

Claim 16

The fairing of claim 1 where said shell comprises a pair of substantially identical shell halves facing each other, and having a hinge formed between the shell halves at the parting line in the nose portion thereof.

Claim 17

The fairing of claim 15 where said shell halves are secured at the trailing edges thereof by removable fasteners accommodated thereby.

Claim 18

The fairing of claim 15 where the material of said shell halves is acrylonitrile butadiene styrene.

Claim 19

The fairing of claim 1, where the material of said shell is a plastic material.

Claim 20

The fairing of claim 18, further comprising sufficient buoyancy material installed in the tail portion of said shell so as to give the fairing substantially neutral buoyancy in water.

Claim 21

The fairing of claim 1, further comprising a second axial opening formed in the tail portion of said fairing to accommodate a cable or the like passed therethrough along the length of said fairing.

Claim 22

An assembly of fairings according to claim 1, with the nose portions thereof axially aligned and a collar mounted between each adjacent pair of fairings at the axial openings of said nose portions thereof.

Claim 23

The combination of claim 21, further comprising a pair of collars mounted at the endmost axial openings of the nose portions of the endmost fairings of said assembly.

Claim 24

The fairing of claim 1 where the fluidynamic aspect ratio of a cross-section thereof taken through any of said upstanding rib portions is approximately 2.1:1 and the fluidynamic aspect ratio of a cross-section thereof taken through any of said alternating tail portions is approximately 2:1.

Claim 25

A fairing for pipes and other substantially rigid structures immersed in a fluid medium, for reducing the coefficient of drag on said pipe due to relative flow thereof with respect to said fluid medium, said fairing comprising a shell of substantially rigid material forming a symmetrical structure having a nose portion and a tail portion; where (a) said nose portion has an opening along its axis to accommodate said pipe; and (b) at least said tail portion has a plurality of upstanding rib portions spaced axially along each side of said fairing and extending rearwardly from the front of said fairing, and a plurality of alternating tail portions at least between said upstanding rib portions; where aspect ratios taken at a cross-section through any of said upstanding rib portions and a cross-section through any of said alternating tail portions are similar; said aspect ratios being the ratio of length to breadth of the fairing, the breadth being the greatest width of each respective cross-section and the length of each respective cross-section being taken along the chord length thereof to the rearmost point of the cross-section where a rearward taper thereof terminates; the length and breadth, respectively, of any cross-section taken through any of said upstanding rib portions being different, in absolute terms, than the length and breadth respectively of any cross-section taken through any of said alternating tail portions of said fairing; and where said alternating tail portions and said upstanding rib portions terminate at a trailing fin portion of said fairing which extends rearwardly therefrom.

Claim 26

A fairing for pipes and other substantially rigid structures immersed in a fluid medium, for reducing the coefficient of drag on said pipe due to relative flow thereof with respect to said fluid medium, said fairing comprising a shell of substantially rigid material forming a symmetrical structure having a nose portion and a tail portion; where (a) said nose portion has an opening along its axis to accommodate said pipe; and (b) at least said tail portion has a plurality of upstanding rib portions spaced axially along each side of said fairing and extending rearwardly from the front of said fairing, and a plurality of alternating tail portions at least between said upstanding rib portions; where aspect ratios taken at a cross-section through any of said upstanding rib portions and a cross-section through any of said alternating tail portions are similar; said aspect ratios being the ratio of length to breadth of the fairing, the breadth being the greatest width of each respective cross-section and the length of each respective cross-section being taken along the chord length thereof to the rearmost point of the cross-section where a rearward taper thereof terminates; the length and breadth, respectively, of any cross-section taken through any of said upstanding rib portions being different, in absolute terms, than the length and breadth respectively of any cross-section taken through any of said alternating tail portions of said fairing; and where said alternating tail portions and said upstanding rib portions terminate at a trailing fin portion of said fairing which extends rearwardly therefrom.

Claim 27

The fairing of claim 24, further comprising a pair of stabilizer plates extending between at least two adjacent upstanding rib portions near the rearward end of each, on each side of said fairing.

Claim 28

A fairing for pipes and other substantially rigid structures immersed in a fluid medium, for reducing the coefficient of drag on said pipe due to relative flow thereof with respect to said fluid medium, said fairing comprising a shell of substantially rigid material forming a symmetrical structure having a nose portion and a tail portion; where (a) said nose portion has an opening along its axis to accommodate said pipe; and (b) at least said tail portion has a plurality of upstanding rib portions spaced axially along each side of said fairing and extending rearwardly from the front of said fairing, and a plurality of alternating tail portions at least between said upstanding rib portions; where aspect ratios taken at a cross-section through any of said upstanding rib portions and a cross-section through any of said aternating tail portions are similar; said aspect ratios being the ratio of length to breadth of the fairing, the breadth being the greatest width of each respective cross-section and the length of each respective cross-section being taken along the chord length thereof to the rearmost point of the cross-section where a rearward taper thereof terminates; the length and breadth, respectively, of any cross-section taken through any of said upstanding rib portions being different, in absolute terms, than the length and breadth respectively of any cross-section taken through any of said alternating tail portions of said fairing; and where each of said aternating tail portions terminates at a trailing fin portion of said fairing which extends rearwardly of said respective alternating tail portion to substantially the same distance behind the front of said as said upstanding rib portions extend; and further comprising a pair of stabilizer plates extending between at least two adjacent upstanding rib portions near the rearward end of each, on each side of said fairing.

Claim 29

A fairing for pipes and other substantially rigid structures immersed in a fluid medium, for reducing the coefficient of drag on said pipe due to relative flow thereof with respect to said fluid medium, said fairing comprising a shell of substantially rigid material forming a symmetrical structure having a nose portion and a tail portion; where (a) said nose portion has an opening along its axis to accommodate said pipe; and (b) at least said tail portion has a plurality of upstanding rib portions spaced axially along each side of said fairing and extending rearwardly from the front of said fairing, and a plurality of alternating tail portions at least between said upstanding rib portions; where aspect ratios taken at a cross-section through any of said upstanding rib portions and a cross-section through any of said aternating tail portions are similar; said aspect ratios being the ratio of length to breadth of the fairing, the breadth being the greatest width of each respective cross-section and the length of each respective cross-section being taken along the chord length thereof to the rearmost point of the cross-section where a rearward taper thereof terminates; the length and breadth, respectively, of any cross-section taken through any of said upstanding rib portions being different, in absolute terms, than the length and breadth respectively of any cross-section taken through any of said alternating tail portions of said fairing; and where each of said aternating tail portions terminates at a trailing fin portion of said fairing which extends rearwardly of said respective alternating tail portion to substantially the same distance behind the front of said as said upstanding rib portions extend; and further comprising a pair of stabilizer plates extending between at least two adjacent upstanding rib portions near the rearward end of each, on each side of said fairing.