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10.6 The Matching Principle

283

10.6 THE MATCHING PRINCIPLE

If we wish to design an aplanatic lens of such a high aperture that a single doublet is impossible, we resort to the use of two achromats in succession. We now have four degrees of freedom. The subdivision of power between the two components and the air space between them is arbitrary, while the two bendings can be used for the correction of spherical aberration and OSC. Any reasonable types of glass can be used, and by achromatizing each component separately we automatically correct both the chromatic aberration and the lateral color.

The design of lenses of this type has been described in detail by Conrady,5 in particular when used as a microscope objective of medium power. Having decided on suitable values for the two arbitrary quantities, we trace a marginal ray through the system from front to back, solving r3 and r6 by the D – d method, and we then add two paraxial rays, one through the front component from left to right using l1 ¼ L1 and u1 ¼ sin U10 , and the other through the rear component from right to left, taking u60 ¼ sin U60 and l60 ¼ L60 as starting data.

If we can now find such a pair of bendings that the two paraxial rays match in the air space between the lenses, the system will be corrected for both spherical aberration and OSC. This is what is meant by the matching principle.

To make the required trial bendings, we have no problem with the front component, but we must adopt standard entry data for the rear component. We can easily adopt a fixed value for L4 by always choosing a suitable air space between the lenses, but any standard value of U4 that we may adopt will never agree exactly with the emerging slope U30 from the front component. Consequently it becomes necessary to match actual aberrations in the air space rather than trying to match lengths and angles.6 So far as lengths are concerned, we have always L4 ¼ L30 – d, and we require that l4 ¼ l30 – d. Subtracting these tells us that we must select bendings such that

LA4 ¼ LA30

(10-1)

To match the slope angles of the paraxial rays in the air space, we have approximately sin U4 ¼ sin U30 , and we require that u4 should also be equal to u30 . Dividing these gives

OSC4 ¼ OSC 30

(10-2)

where the OSC is defined as

 

OSC ¼ ðu= sin UÞ 1

(10-3)

Since this kind of OSC does not contain the usual correcting factor for spherical aberration and exit-pupil position (see Sections 4.3.4 and 9.3), we

284

Design of Aplanatic Objectives

refer to it as uncorrected OSC in the present context. Recall that we are trying to match the ray slope angles in the space between the front and rear components; hence the uncorrected OSC is just a convenient gauge of the relation linking the paraxial and marginal rays. To reiterate, should the matching principle concept of requiring Eqs. (10-1) and (10-2) to be satisfied not be fulfilled, it is certain that the lens system suffers imperfect correction of its aberrations.

As an example to illustrate the matching principle, we will design a 10 microscope objective of numerical aperture 0.25, so that the entering ray slope at the long conjugate end is 0.025. Assuming an object distance of 170 mm, we can trace any desired rays into the front component of the system. It should be noted that, as always, we calculate a microscope objective from the long conjugate to the short, because the long conjugate distance is fixed while the short is not, so that the long-conjugate end becomes the “front” of our system. This conflicts with ordinary microscope parlance, which regards the front of a microscope objective as the short conjugate end; this is a unique exception and we shall ignore it here.

Our first problem is to deal with the two arbitrary degrees of freedom, namely, the subdivision of refracting power between the two components, and the air space between them. For this, it is common to require that the paraxial ray suffers equal deviation at each component, and to place the rear component approximately midway between the front component and its image. This makes the object distance for all rear-element bendings about 20 mm, and we shall adopt that value here.7

As the overall paraxial deviation is 0.25 þ 0.025 ¼ 0.275, we must allow each component to deviate the paraxial ray by 0.1375, which makes the ray slope between the components equal to 0.1125. We shall therefore adopt this value of sin U4 in making all trial bendings of the rear component. For both lenses we use the following common types of glass:

(a)Crown: ne ¼ 1.52520, nF – nC ¼ 0.00893, Ve ¼ 58.81

(b)Flint: ne ¼ 1.62115, nF – nC ¼ 0.01686, Ve ¼ 36.84

with Va – Vb ¼ 21.97. The thin-lens data of the two components (Figure 10.9) are as shown in Table 10.4.

After determining the last radius by the D – d method in every case, the results of several bendings of each component are found to be as shown in Table 10.5. These results are plotted side by side on one graph in Figure 10.10.

0.025

–170

Front

Rear –0.1125 d –0.25

Figure 10.9 A Lister-type microscope design.

10.6 The Matching Principle

 

 

 

 

285

 

 

 

Table 10.4

 

 

 

 

Thin-Lens Data for Lister-type Microscope Shown in Figure 10.9

 

 

 

 

 

 

 

 

Object

Image

Focal

Clear

 

 

Suitable

distance

distance

length

aperture

 

 

thicknesses

(mm)

(mm)

(mm)

(mm)

ca

cb

(mm)

170

37.77

30.90

8.5

0.1649

0.0874

3.2, 1.0

20.0

9.00

16.36

4.5

0.3116

0.1650

2.0, 0.8

Table 10.5

Aberrations Versus Bendings for Lister-type Microscope

Front component

 

 

 

 

 

 

L1 ¼ l1 ¼ 170.0

 

sin U1 ¼ u1 ¼ 0.025

 

 

 

c1

0

0.02

0.04

0.06

 

0.08

c3 by D – d

0.08273

0.06254

0.04130

0.01870

þ0.00558

L30

33.149

34.666

35.465

35.567

35.005

LA03

 

 

 

 

 

 

0.1474

0.9529

1.3282

0.8596

 

0.6049

uncorrected OSC30

0.01164

0.03753

0.03727

0.01360

0.03567

 

Rear component

 

 

 

 

 

 

L4 ¼ 20.00

 

sin U4 ¼ 0.1125

 

 

 

c4

0.05

0.10

0.15

0.20

 

0.25

c6 by D – d

0.11360

0.05405

0.01450

0.09511

 

0.19249

L06 ¼ l60

7.3552

7.3700

7.2695

7.0888

 

6.8570

sin U60 ¼ u60

0.25862

0.24760

0.23939

0.23259

0.22588

l4

18.8706

20.2829

20.7971

20.4545

19.3870

LA4

1.1294

0.2829

0.7971

0.4545

 

0.6130

uncorrected OSC4

0.03222

0.03055

0.04323

0.01363

 

0.05653

LA

 

OSC

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

2

 

0.04

 

OSC

 

 

 

 

 

 

Top

 

 

 

 

 

 

 

 

 

 

 

 

OSC

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1

 

0.02

 

 

LA

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Long

 

 

 

 

 

Middle

 

 

 

 

 

 

 

 

 

 

 

 

LA

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

0

 

0

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

–1

 

–0.02

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Bottom

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

–2

 

–0.04

 

 

 

 

 

 

 

 

 

 

 

 

c1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

c4

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

0

0.02

0.04

0.06

0.08

 

0.05

0.10

0.15

0.20

0.25

 

 

 

 

Figure 10.10 The matching principle.

286

 

 

 

Design of Aplanatic Objectives

 

 

 

Table 10.6

 

 

 

 

 

Matching Solutions

 

 

 

 

 

 

 

 

 

 

Rectangle

c1

c2

c3

c4

c5

c6

 

 

 

 

 

 

 

A (top)

0.032

0.133

0.050

0.045

0.266

0.119

B (middle)

0.067

0.098

0.010

0.070

0.242

0.091

C (bottom)

0.081

0.084

0.007

0.165

0.147

0.037

D (long)

0.003

0.162

0.080

0.228

0.084

0.147

It is our aim to select such values of c1 and c4 that LA30 ¼ LA4 and simultaneously OSC30 ¼ OSC4. This is done by searching for rectangles that just fit into the four curves, with spherical aberration and coma points, respectively, each being on the same level. In this case, there are four such rectangles to be found, indicating that the curves represent quadratic expressions. The four solutions are shown in Table 10.6.

For many reasons we shall continue the design using solution C. All the other solutions contain stronger surfaces, and moreover both components of solution C contain almost equiconvex crown elements. This starting setup is as follows:

c

d

ne

0.081

3.21.52520

0.08394

1.01.62115

0.00685

14.9603 (air)

0.165

2.01.52520

0.14654

0.81.62115

0.03730

with l60 ¼ 7.2095, LA60 ¼ 0.01383, u60 ¼ 0.2361, and OSC60 ¼ 0.00297. For the final OSC60 calculation we assumed that the exit pupil is in such a position that (l0 – l0pr) is about 17.0. This puts the exit pupil about 10 mm inside the rear vertex of the objective.

Although this solution is close, we must improve both aberrations by means of a double graph. Changing c1 by 0.001 and maintaining the D – d solutions, and L4 ¼ 20.0, we find that the aberrations become

LA06 ¼ 0:000829; OSC 06 ¼ 0:002404

10.6 The Matching Principle

287

Restoring the original c1 and changing c4 by 0.001 gives

LA60 ¼ 0:001306;

OSC 60 ¼ 0:003279

Inspection of the graph suggests that we change the original c1 by 0.001 and c4 by –0.01. These changes give

LA06 ¼ 0:000403; OSC 06 ¼ þ0:000474

Unfortunately the numerical aperture of the system is now 0.2381, whereas it should be 0.25. We therefore scale all radii down by 4%, which gives

LA06 ¼ 0:001114; OSC 06 ¼ 0:000221

Further reference to the double graph suggests that we try Dc1 ¼ 0.0005 and Dc4 ¼ 0.002. This change gives the almost perfect solution drawn to scale in Figure 10.9, namely,

c

d

ne

0.08578

3.2 1.52520

0.08576

1.0 1.62115

0.009152

13.8043 (air)

0.16320

2.0 1.52520

0.16080

0.8 1.62115

0.02602

with l60 ¼ 6.8925, u60 ¼ 0.2500, LA60 ¼ 0.000004, OSC60 ¼ –0.000095, and LZA60 ¼ –0.00289. In practice, of course, we should apply trifling further bendings to both components to render the crown elements exactly equiconvex. These changes are so slight that they have no significant effect on any of the aberrations.

The zonal aberration tolerance is 6l/sin2 Um0 ¼ 0.053, so that the zonal residual of our objective is about half the Rayleigh limit. To improve it, we would have to go to a flint of somewhat higher index, but the present design would be acceptable as it stands.