Research article

On some new frames along a space curve and integral curves with Darboux q-vector fields in E3

  • Received: 20 February 2024 Revised: 30 April 2024 Accepted: 16 May 2024 Published: 24 May 2024
  • MSC : 53A04

  • In this paper, to start we defined osculating q-frame, normal q-frame, and rectifying q-frame along a space curve in Euclidean 3-space E3 by using the Darboux vector field of the q-frame. We obtained the derivative equations of these new frames. Later, we defined some new integral curves of a space curve and called them ¯do-direction curve, ¯dn-direction curve and ¯dr-direction curve. Finally, we gave some theorems and results related with these curves.

    Citation: Bahar UYAR DÜLDÜL. On some new frames along a space curve and integral curves with Darboux q-vector fields in E3[J]. AIMS Mathematics, 2024, 9(7): 17871-17885. doi: 10.3934/math.2024869

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  • In this paper, to start we defined osculating q-frame, normal q-frame, and rectifying q-frame along a space curve in Euclidean 3-space E3 by using the Darboux vector field of the q-frame. We obtained the derivative equations of these new frames. Later, we defined some new integral curves of a space curve and called them ¯do-direction curve, ¯dn-direction curve and ¯dr-direction curve. Finally, we gave some theorems and results related with these curves.



    The Frenet frame is the best known and the most used frame for characterizing curves in differential geometry. However, there exist other frames for characterizing curves. Some of these alternative frames are the Bishop frame (rotation minimizing frame), the Flc (Frenet-like curve) frame, the {N,C,W} frame, etc. The Bishop frame [2] is also very suitable for engineering applications [10] because of being defined at points where even curvatures vanish. That's why many studies have been done by using this frame. On the other hand, the Bishop frame cannot be calculated analytically [6]. Therefore, Dede [5] recently introduced a new moving frame called the Flc frame. This frame has much easier calculations and a more analytical form that the Bishop frame does not have. The other alternative frame, {N,C,W}, has been defined by Scofield [14], providing a different approach. Uzunoğlu et al. [15] showed that the {N,C,W} frame has an important advantage according to the Frenet frame since the expression of slant helix characterization is more short with the new curvatures. As an alternative to the Frenet frame, Dede et al. [4] defined a new adapted frame along a space curve. They called this new frame as q-frame and obtained the relations between the Frenet frame and the q-frame.

    By using the Darboux frame {T,V,U} along a regular curve α lying on an oriented surface M in E3, Hananoi et al. [9] defined the osculating Darboux vector field Do, the normal Darboux vector field Dn, and the rectifying Darboux vector field Dr, where T is the unit tangent vector field of α, U is the unit normal vector field of M restricted to α, and V=U×T. Considering these vector fields, Önder [13] defined three special curves on a surface as Di-Darboux slant helices, where i{o,n,r}. In recent days, Alkan et al. [1] defined osculator Darboux frame, normal Darboux frame, and rectifying Darboux frame.

    Recently, many researchers [3,7,8,11,12,16] have studied associated curves and have revealed the relationships between the main curve and the associated curves. The spherical indicators, the involute-evolute curve couple, the Bertrand curve couple, the Mannheim curve couple, and the integral curves are the most familiar ones among these associated curves. Integral curves are one of the interesting curves among these curves since they are tangent to the vector field at every point.

    In this study, considering the Darboux vector field of the q-frame, we first define some new frames called the osculating q-frame, the normal q-frame, and the rectifying q-frame along a space curve in E3 and obtain their derivative equations. Second, by using some vector fields of these new q-frames, we define new integral curves called ¯do-direction curve, ¯dn-direction curve, and ¯dr-direction curve of a space curve.

    Let α=α(t) be a regular space curve with nondegenerate condition α×α0. Then, the Frenet frame vector fields are defined as

    t=α||α||,n=b×t,b=α×α||α×α||,

    where t, n, and b denote the tangent, the principal normal, and the binormal vector fields of the curve α and the prime denotes the derivative with respect to t. Then, we have the following Frenet equations:

    {t=vκn,n=v(κt+τb),b=vτn,

    where v=||α(t)||, and the curvature and the torsion functions are

    κ=||α×α||||α||3,τ=α×α,α||α×α||2,

    respectively.

    The q-frame {t,nq,bq,k}, which is an alternative to the Frenet frame along a space curve α=α(t), is given by Dede et al. [4], and its vector fields are defined as

    t=α||α||,nq=t×k||t×k||,bq=t×nq,

    where the vector k=(0,0,1) is the projection vector and the vectors nq and bq are the quasi-normal and the quasi-binormal vector, respectively. The relation matrix between the Frenet frame and the q-frame is given by

    (tnb)=(1000cosθsinθ0sinθcosθ)(tnqbq),

    where θ is the angle between the vectors n and nq.

    Let α=α(s) be a space curve with arc length parameter s. Then, the q-frame equations are given by

    (tnqbq)=(0k1k2k10k3k2k30)(tnqbq), (2.1)

    where k1,k2,k3 denote the q-curvatures of α [4]. The relations between the curvatures are

    k1=κcosθ,k2=κsinθ,k3=θ+τ,

    where κ, τ are the Frenet curvatures. The Darboux vector dq of the q-frame {t,nq,bq,k} is given by

    dq=k3tk2nq+k1bq.

    Thus, the instantaneous angular speed of the q-frame is calculated as

    ||dq||=k21+k22+k23.

    Let us consider the vector fields do, dn, and dr which are called the osculating q-vector field, the normal q-vector field, and the rectifying q-vector field along α, respectively:

    do=k3tk2nq,
    dn=k2nq+k1bq,
    dr=k3t+k1bq.

    Then, the unit osculating q-vector field, the unit normal q-vector field, and the unit rectifying q-vector field along α are given by, respectively:

    ¯do=k3k22+k23tk2k22+k23nq, (2.2)
    ¯dn=k2k21+k22nq+k1k21+k22bq, (2.3)
    ¯dr=k3k21+k23t+k1k21+k23bq. (2.4)

    In this section, let us define some new frames along a space curve using the Darboux vector field of the q-frame and give some theorems related with these frames.

    Definition 3.1. Let α be a space curve in E3, {t,nq,bq,k} be its q-frame, and ¯do be the unit osculating q-vector field along the curve α. Then, the orthonormal frame {¯do,bq,eo} is called the osculating q-frame along α, where eo=¯do×bq.

    Theorem 3.2. Let {¯do,bq,eo} be the osculating q-frame along the curve α. Then, the derivative equations according to this frame can be found as

    {¯do=ρoeo,bq=ηoeo,eo=ρo¯doηobq, (3.1)

    where ρo=(k3k2k2k3)+k1(k22+k23)k22+k23 and ηo=k22+k23 are the curvatures of α according to the osculating q-frame.

    Proof. Since ¯do is the unit osculating q-vector field along the curve α, we get ¯doSp{t,nq}. So, ¯dobq, and, thus, {¯do,bq,eo} is an orthonormal frame along α, where eo=¯do×bq. Since ¯doSp{¯do,bq,eo}, we can write

    ¯do=a1¯do+a2bq+a3eo.

    Taking the inner product of both sides of this equation with ¯do yields a1=¯do,¯do=0 because of ||¯do||=1. So, we get

    ¯do=a2bq+a3eo. (3.2)

    If we take the inner product of both sides of Eq (3.2) with bq and eo, respectively, we obtain a2=¯do,bq and a3=¯do,eo. Substituting

    sinϕ=k3k22+k23,cosϕ=k2k22+k23 (3.3)

    into Eq (2.2) gives

    ¯do=sinϕtcosϕnq. (3.4)

    If we differentiate this equation with respect to s and use Eq (2.1), we have

    ¯do=(ϕ+k1)cosϕt+(ϕ+k1)sinϕnq+(k2sinϕk3cosϕ)bq.

    If we use Eq (3.3), we get a2=0. So,

    ¯do=(ϕ+k1)[cosϕt+sinϕnq]. (3.5)

    Moreover, using Eq (3.4), we obtain

    eo=cosϕtsinϕnq. (3.6)

    If we use Eqs (3.5) and (3.6), we obtain a3=(ϕ+k1). Also, Eq.(3.3) gives tanϕ=k3k2, and by doing some calculations, we find

    a3=[(k3k2k2k3)+k1(k22+k23)k22+k23].

    So, from Eq (3.2), we obtain

    ¯do=[(k3k2k2k3)+k1(k22+k23)k22+k23]eo. (3.7)

    In a similar way, we may write bq as a linear combination of the vectors ¯do, bq, and eo, i.e.,

    bq=b1¯do+b2bq+b3eo. (3.8)

    Taking the inner product of both sides of Eq (3.8) with ¯do yields b1=bq,¯do. If we use Eqs (2.1), (3.3), and (3.4), we find b1=0. Also, since ||bq||=1, we get b2=0. Then, we have

    bq=b3eo. (3.9)

    If we take the inner product of both sides of Eq (3.9) with eo and use Eqs (2.1), (3.3), and (3.6), we obtain

    bq=k22+k23eo. (3.10)

    Moreover, since eoSp{¯do,bq,eo}, it can be written as

    eo=c1¯do+c2bq+c3eo. (3.11)

    Taking the inner product of both sides of Eq (3.11) with ¯do gives c1=eo,¯do. Using Eqs (2.1) and (3.6) yields

    eo=(ϕ+k1)sinϕt(ϕ+k1)cosϕnq(k2cosϕ+k3sinϕ)bq. (3.12)

    If we use Eqs (3.3), (3.4), and (3.12), we obtain

    c1=(k3k2k2k3)+k1(k22+k23)k22+k23.

    From Eqs (3.3), (3.11), and (3.12), we get c2=k22+k23. Also, since ||eo||=1, we have c3=0. Then, from Eq (3.11), we find

    eo=[(k3k2k2k3)+k1(k22+k23)k22+k23]¯dok22+k23bq. (3.13)

    If we denote ρo=(k3k2k2k3)+k1(k22+k23)k22+k23 and ηo=k22+k23, Eqs (3.7), (3.10), and (3.13) give the desired equations. Here, ρo and ηo are called the curvatures of α according to the osculating q-frame.

    Definition 3.3. Let {¯do,bq,eo} be the osculating q-frame along the space curve α. The curve α is called a bq-slant helix relative to the osculating q-frame if the vector field bq makes a constant angle with a fixed direction, i.e., bq,u=cosψ, where u is a constant unit vector and ψ is a constant angle.

    Theorem 3.4. Let {¯do,bq,eo} be the osculating q-frame along the space curve α. The curve α is a bq-slant helix relative to the osculating q-frame if, and only if, the expression ηoρo is constant (for ηo0 and ρo0).

    Proof. Let α be a bq-slant helix relative to the osculating q-frame. Then, bq,u=cosψ=c0, where u is a unit constant direction. So, it can be written as

    u=λ1¯do+cbq+λ2eo,(λ1,λ2R).

    If we differentiate this equation, we obtain

    u=λ1¯do+λ1¯do+cbq+λ2eo+λ2eo.

    If we use Eq (3.1), we find

    {λ1+λ2ρo=0,λ2ηo=0,λ2λ1ρo+cηo=0.

    Since ηo0 and ρo0, we have λ2=0 and λ1=constant. Thus, we get ηoρo=constant.

    Conversely, let ηoρo be constant. Choosing ηoρo=cosψsinψ and taking u=cosψ¯do+sinψbq gives u=0 by using Eq (3.1). So, the vector u is constant. Also, by taking the inner product of both sides of u=cosψ¯do+sinψbq with bq yields to u,bq=sinψ. Then, the constant vector u and the vector bq make a constant angle, i.e., the curve α is a bq-slant helix.

    Corollary 3.5. A space curve α with (k2(s),k3(s))(0,0) is a bq-slant helix if, and only if,

    ρ1(s)=(k3k2k2k3)+k1(k22+k23)(k22+k23)3/2

    is a constant function.

    Definition 3.6. Let α be a space curve in E3, {t,nq,bq,k} be its q-frame, and ¯dn be the unit normal q-vector field along the curve α. Then, the orthonormal frame {¯dn,t,en} is called the normal q-frame along α, where en=¯dn×t.

    Theorem 3.7. Let {¯dn,t,en} be the normal q-frame along the curve α. Then, the derivative equations according to this frame can be obtained as

    {¯dn=ρnen,t=ηnen,en=ρn¯dnηnt, (3.14)

    where ρn=(k2k1k1k2)+k3(k21+k22)k21+k22 and ηn=k21+k22 are the curvatures of α according to the normal q-frame.

    Proof. Since ¯dn is the unit normal q-vector field along α, from Eq (2.3), we have ¯dnSp{nq,bq}. Hence, ¯dnt. Let en=¯dn×t. Then, we obtain the orthonormal frame {¯dn,t,en} along α. Since ¯dnSp{¯dn,t,en}, it can be written as

    ¯dn=a1¯dn+a2t+a3en. (3.15)

    If we take the inner product of both sides of Eq (3.15) with ¯dn and take into consideration ||¯dn||=1, we get a1=0. So, we have

    ¯dn=a2t+a3en. (3.16)

    Taking the inner product of both sides of Eq (3.16) with t and en, respectively, yields a2=¯dn,t and a3=¯dn,en. In Eq (2.3), if we take

    sinϕ=k2k21+k22,cosϕ=k1k21+k22, (3.17)

    we obtain

    ¯dn=sinϕnq+cosϕbq. (3.18)

    Differentiating this equation with respect to s and using Eq (2.1) gives

    ¯dn=(k1sinϕk2cosϕ)t(ϕ+k3)cosϕnq(ϕ+k3)sinϕbq.

    If we use Eq (3.17), we get a2=0. So, we have

    ¯dn=(ϕ+k3)[cosϕnq+sinϕbq]. (3.19)

    Also, using Eq (3.18) yields

    en=cosϕnq+sinϕbq. (3.20)

    Moreover, from Eqs (3.19) and (3.20), we have a3=(ϕ+k3). By doing some calculations, we find

    a3=[(k2k1k1k2)+k3(k21+k22)k21+k22].

    If we use Eq (3.16), we have

    ¯dn=[(k2k1k1k2)+k3(k21+k22)k21+k22]en. (3.21)

    Similarly, since tSp{¯dn,t,en}, we can write

    t=b1¯dn+b2t+b3en. (3.22)

    If we take the inner product of both sides of Eq (3.22) with ¯dn, we obtain b1=t,¯dn. Eqs (2.1), (3.17), and (3.18) give b1=0. Also, since ||t||=1, we have b2=0. So, we get

    t=b3en. (3.23)

    Taking the inner product of both sides of Eq (3.23) with en and using Eqs (2.1), (3.17), and (3.20) yields b3=k21+k22 and

    t=k21+k22en. (3.24)

    Additionally, since enSp{¯dn,t,en}, we can write

    en=c1¯dn+c2t+c3en. (3.25)

    If we take the inner product of both sides of Eq (3.25) with ¯dn, we get c1=en,¯dn. Eqs (2.1) and (3.20) give us

    en=(k1cosϕ+k2sinϕ)t(ϕ+k3)sinϕnq+(ϕ+k3)cosϕbq. (3.26)

    If we use Eqs (3.18) and (3.26), we find

    c1=(k2k1k1k2)+k3(k21+k22)k21+k22.

    Also, using Eqs (3.17), (3.25), and (3.26) yields c2=k21+k22. In addition, since ||en||=1, we have c3=0. Thus, using Eq (3.25) gives

    en=[(k2k1k1k2)+k3(k21+k22)k21+k22]¯dnk21+k22t. (3.27)

    If we denote ρn=(k2k1k1k2)+k3(k21+k22)k21+k22 and ηn=k21+k22 and use Eqs (3.21), (3.24), and (3.27), we obtain the desired equations.

    Theorem 3.8. Let {¯dn,t,en} be the normal q-frame along the space curve α. The curve α is a helix relative to the normal q-frame if, and only if, the expression ηnρn is constant, for ηn0 and ρn0.

    Proof. Let α be a helix relative to the normal q-frame. Then, t,u=cosψ=c0, where u is a unit constant direction. So, we can write

    u=λ1¯dn+ct+λ2en,(λ1,λ2R).

    Differentiating this equation with respect to s and using Eq (3.14) gives

    {λ1+λ2ρn=0,λ2ηn=0,λ2λ1ρn+cηn=0.

    Since ηn0 and ρn0, we have λ2=0 and λ1=constant. So, we obtain ηnρn=constant.

    Conversely, let ηnρn be constant. If we choose ηnρn=cosψsinψ and take u=cosψ¯dn+sinψt, we find u=0 with the help of Eq (3.14). Then, the vector u is constant. Additionally, if we take the inner product of both sides of u=cosψ¯dn+sinψt with t, we get u,t=sinψ. Consequently, the constant vector u and the tangent vector t make a constant angle, i.e., the curve α is a helix.

    Example 3.9. Let us consider the curve α(t)=(3tt3,3t2,3t+t3) in E3. The q-frame apparatus of the curve α is

    t=12(1+t2)(1t2,2t,1+t2),nq=11+t2(2t,t21,0),bq=12(1+t2)(1t2,2t,1t2),
    k1=21+t2,k2=0,k3=21+t2,

    with the projection vector k=(0,0,1). Also, the normal q-frame apparatus of the curve α is

    ¯dn=12(1+t2)(t21,2t,1+t2),t=12(1+t2)(1t2,2t,1+t2),en=11+t2(2t,1t2,0),
    ρn=ηn=21+t2.

    Since the expression ηnρn is constant, the curve α is a helix relative to the normal q-frame.

    Corollary 3.10. A space curve α with (k1(s),k2(s))(0,0) is a helix if, and only if,

    ρ2(s)=(k2k1k1k2)+k3(k21+k22)(k21+k22)3/2

    is a constant function.

    Definition 3.11. Let α be a space curve in E3, {t,nq,bq,k} be its q-frame, and ¯dr be the unit rectifying q-vector field along the curve α. Then, the orthonormal frame {¯dr,nq,er} is called the rectifying q-frame along α, where er=¯dr×nq.

    Theorem 3.12. Let {¯dr,nq,er} be the rectifying q-frame along the curve α. Then, the derivative equations according to this frame can be calculated as

    {¯dr=ρrer,nq=ηrer,er=ρr¯drηrnq,

    where ρr=(k3k1k1k3)k2(k21+k23)k21+k23 and ηr=k21+k23 are the curvatures of α according to the rectifying q-frame.

    Proof. Since ¯dr is the unit rectifying q-vector field along α, we have ¯drSp{t,bq}. So, ¯drnq and {¯dr,nq,er} is an orthonormal frame along α, where er=¯dr×nq. Since ¯drSp{¯dr,nq,er}, we can write

    ¯dr=a1¯dr+a2nq+a3er. (3.28)

    If we take the inner product of both sides of Eq (3.28) with ¯dr and consider ||¯dr||=1, we have a1=0. So, it can be written as

    ¯dr=a2nq+a3er. (3.29)

    Taking the inner product of both sides of Eq (3.29) with nq and er, respectively, yields a2=¯dr,nq and a3=¯dr,er. In Eq (2.4), denoting

    sinϕ=k3k21+k23,cosϕ=k1k21+k23, (3.30)

    gives

    ¯dr=sinϕt+cosϕbq. (3.31)

    If we differentiate Eq (3.31) with respect to s and use Eq (2.1), we obtain

    ¯dr=(ϕk2)cosϕt+(k1sinϕk3cosϕ)nq(ϕk2)sinϕbq.

    So, from Eq (3.30), we get a2=0 and

    ¯dr=(ϕk2)[cosϕtsinϕbq]. (3.32)

    Moreover, from Eq (3.31), we have

    er=cosϕt+sinϕbq. (3.33)

    Also, if we use Eqs (3.32) and (3.33), we obtain a3=(ϕk2). Doing some calculations yields

    a3=[(k3k1k1k3)k2(k21+k23)k21+k23]

    and from Eq (3.29), it follows that

    ¯dr=[(k3k1k1k3)k2(k21+k23)k21+k23]er. (3.34)

    Similarly, since nqSp{¯dr,nq,er}, we can write

    nq=b1¯dr+b2nq+b3er. (3.35)

    If we take the inner product of both sides of Eq (3.35) with ¯dr, we get b1=nq,¯dr. Using Eqs (2.1), (3.30), and (3.31) yields b1=0. Also, since ||nq||=1, we have b2=0. Then, we get

    nq=b3er. (3.36)

    Taking the inner product of both sides of Eq (3.36) with er gives b3=nq,er. If we use Eqs (2.1), (3.30), and (3.33), we obtain b3=k21+k23. So, we have

    nq=k21+k23er. (3.37)

    Moreover, since erSp{¯dr,nq,er}, it can be written as

    er=c1¯dr+c2nq+c3er. (3.38)

    If we take the inner product of both sides of Eq (3.38) with ¯dr, we have c1=er,¯dr. From Eqs (2.1) and (3.33), we have

    er=(ϕk2)sinϕt(k1cosϕ+k3sinϕ)nq+(ϕk2)cosϕbq. (3.39)

    If we use Eqs (3.31) and (3.39), we obtain

    c1=(k3k1k1k3)k2(k21+k23)k21+k23.

    From Eqs (3.30), (3.38), and (3.39), we find c2=k21+k23. Also, we get c3=0, since ||er||=1. So, Eq (3.38) yields

    er=[(k3k1k1k3)k2(k21+k23)k21+k23]¯drk21+k23nq. (3.40)

    Thus, if we denote

    ρr=(k3k1k1k3)k2(k21+k23)k21+k23

    and

    ηr=k21+k23,

    we obtain the desired equations from Eqs (3.34), (3.37), and (3.40).

    Definition 3.13. Let {¯dr,nq,er} be the rectifying q-frame along the space curve α. The curve α is called an nq-slant helix relative to the rectifying q-frame if the vector field nq makes a constant angle with a fixed direction, i.e., nq,u=cosψ, where u is a constant unit vector and ψ is a constant angle.

    Theorem 3.14. Let {¯dr,nq,er} be the rectifying q-frame along the space curve α. The curve α is an nq-slant helix relative to the rectifying q-frame if, and only if, the expression ηrρr is constant (for ηr0 and ρr0).

    Proof. The proof of the theorem can be done in a similar way to the proof of Theorem 3.4.

    Corollary 3.15. A space curve α with (k1(s),k3(s))(0,0) is an nq-slant helix if, and only if,

    ρ3(s)=(k3k1k1k3)k2(k21+k23)(k21+k23)3/2

    is a constant function.

    In this section, let us define some new integral curves associated with a space curve using the osculating, the normal, and the rectifying q-frame vector fields.

    Definition 4.1. Let α be a space curve in E3, {t,nq,bq,k} be the q-frame along α, and ¯do be the unit osculating q-frame vector field of α. The integral curve of the vector field ¯do is called the ¯do-direction curve of α. Namely, if γ(s) is the ¯do-direction curve of α, then γ(s)=¯do(s) or ¯do(s)=γ(s).

    Now, let us find the Frenet apparatus {tγ,nγ,bγ,κγ,τγ} of γ. Since γ is the ¯do-direction curve of α, it can be written γ=¯do. So, the tangent vector tγ of γ is

    tγ=¯do=1k22+k23(k3tk2nq).

    If we differentiate this equation with respect to s and use Eq (2.1), we obtain

    ¯do=(k3k2k2k3)+k1(k22+k23)(k22+k23)3/2(k2t+k3nq). (4.1)

    Since ρo=(k3k2k2k3)+k1(k22+k23)k22+k23, Eq (4.1) can be rewritten as

    ¯do=ρobq||bq||.

    So, we have ||¯do||=ερo, where ε=±1. Since nγ=¯do||¯do||, we get

    nγ=εbq||bq||.

    Additionally, since bγ=tγ×nγ, the binormal vector is obtained as bγ=εbq. Moreover, the curvature and the torsion of γ can be found as

    κγ=||tγ||=ερo,τγ=bγ,nγ=ηo.

    Then, the following corollary can be given.

    Corollary 4.2. Let γ be the ¯do-direction curve of a space curve α. Then, the Frenet apparatus {tγ,nγ,bγ,κγ,τγ} of γ can be obtained as

    tγ=¯do,nγ=εbq||bq||,bγ=εbq,κγ=ερo,τγ=ηo,

    where ε=±1.

    Corollary 4.3. γ is a general helix if, and only if, α is a bq-slant helix.

    Definition 4.4. Let α be a space curve in E3, {t,nq,bq,k} be the q-frame along α, and ¯dn be the unit normal q-frame vector field of α. The integral curve of the vector field ¯dn is called the ¯dn-direction curve of α. Namely, if ζ(s) is the ¯dn-direction curve of α, then ζ(s)=¯dn(s) or ¯dn(s)=ζ(s).

    Similarly, let us obtain the Frenet apparatus {tζ,nζ,bζ,κζ,τζ} of the curve ζ. Taking into account the definition of the ¯dn-direction curve gives

    tζ=¯dn=1k21+k22(k2nq+k1bq).

    Differentiating this equation with respect to s and applying Eq (2.1) yields

    ¯dn=(k1k2k2k1)k3(k21+k22)(k21+k22)3/2(k1nq+k2bq). (4.2)

    Since ρn=(k2k1k1k2)+k3(k21+k22)k21+k22, Eq (4.2) can be rewritten as

    ¯dn=ρnt||t||.

    Then, we get ||¯dn||=ερn, where ε=±1. Thus, since nζ=¯dn||¯dn||, we obtain

    nζ=εt||t||.

    Also, the binormal vector bζ is given by bζ=εt. Besides, the curvatures of the ¯dn-direction curve ζ can be obtained as

    κζ=||tζ||=ερn,τζ=bζ,nζ=ηn.

    Then, we can give the following corollary.

    Corollary 4.5. Let ζ be the ¯dn-direction curve of a space curve α. Then, the Frenet apparatus {tζ,nζ,bζ,κζ,τζ} of ζ can be found as

    tζ=¯dn,nζ=εt||t||,bζ=εt,κζ=ερn,τζ=ηn,

    where ε=±1.

    Corollary 4.6. ζ is a general helix if, and only if, α is a general helix.

    Definition 4.7. Let α be a space curve in E3, {t,nq,bq,k} be the q-frame along α, and ¯dr be the unit rectifying q-frame vector field of α. The integral curve of the vector field ¯dr is called the ¯dr-direction curve of α. Namely, if φ(s) is the ¯dr-direction curve of α, then φ(s)=¯dr(s) or ¯dr(s)=φ(s).

    In a similar way, let us calculate the Frenet apparatus {tφ,nφ,bφ,κφ,τφ} of φ. From the definition of the ¯dr-direction curve, we have

    tφ=¯dr=1k21+k23(k3t+k1bq).

    If we differentiate this equation with respect to s, we find

    ¯dr=(k3k1k1k3)k2(k21+k23)(k21+k23)3/2(k1tk3bq). (4.3)

    Since ρr=(k3k1k1k3)k2(k21+k23)k21+k23, from Eq (4.3) we obtain

    ¯dr=ρrnq||nq||.

    Then, we have ||¯dr||=ερr, where ε=±1. Since nφ=¯dr||¯dr||, we get

    nφ=εnq||nq||.

    Also, the binormal vector bφ of the curve φ is found as bφ=εnq. In addition, the curvature and the torsion of the ¯dr-direction curve φ can be obtained as

    κφ=||tφ||=ερr,τφ=bφ,nφ=ηr.

    Then, the following corollary can be given.

    Corollary 4.8. Let φ be the ¯dr-direction curve of a space curve α. Then, the Frenet apparatus {tφ,nφ,bφ,κφ,τφ} of φ can be obtained as

    tφ=¯dr,nφ=εnq||nq||,bφ=εnq,κφ=ερr,τφ=ηr,

    where ε=±1.

    Corollary 4.9. φ is a general helix if, and only if, α is an nq-slant helix.

    In this study, we obtained the derivative equations of the osculating q-frame, the normal q-frame, and the rectifying q-frame which have been defined along a space curve by using the Darboux vector field of the q-frame in Euclidean 3-space. Then, we defined some new slant helices and new integral curves and gave their characterizations.

    The author declares she has not used Artificial Intelligence (AI) tools in the creation of this article.

    The author declares no conflicts of interest.



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