Fuel saving aircraft descent calculator

• US 4,346,288 A
• Filed: 10/31/1980
• Issued: 08/24/1982
• Est. Priority Date: 10/31/1980
• Status: Expired due to Term

• Current Assignee: Edward T. Foster
• Original Assignee: Edward T. Foster
• Inventors: Foster, Edward T.
• Primary Examiner(s): Hix, L. T.
• Assistant Examiner(s): Fuller, Benjamin R.
• Application Number:
  US06/202,601
• Time in Patent Office: 662 Days
• Field of Search: 235/61 NV, 235/61 FA, 235/70 R, 235/70 A, 235/78 N, 235/88 N, 235/89 R
• US Class Current: 235/70.00A
• CPC Class Codes: G06G 1/0063 for calculating fuel consumption

Abstract

A manually operable calculator for optimizing aircraft fuel consumption during descent from an actual altitude to a target altitude/distance. Altitude and distance scales are provided which are alignable to determine an uncorrected fuel efficient distance to commence a descent from a given altitude to a target location, with separate scales being provided for different airspeeds. Wind and weight correction scales are also provided which give a distance correction based upon the aircraft'"'"'s weight, prevailing wind conditions, and the difference between beginning and target altitudes. In the preferred embodiment a plurality of altitude scales are employed, each scale having thereon an altitude display which is proportioned in accordance with a respective air speed and given in terms of mach speed for altitudes above a mach speed/I.A.S. transition point, and in terms of I.A.S. below that point. In this embodiment a single, linear distance scale is employed.

Claims

1. A manually operable calculator for calculating a beginning of descent position to optimize aircraft fuel consumption during descent from an actual altitude and distance to a target altitude and distance, comprising:

a first member having a distance scale displayed thereon,

a second member having a first altitude scale displayed thereon, said first altitude scale being proportional in terms of indicated air speed below a predetermined altitude,

said first and second members being mutually alignable and said distance and first altitude scales being proportioned so that, when a target distance on the distance scale is aligned with a target altitude on the first altitude scale, the actual altitude on the first altitude scale is aligned with a desired fuel efficient distance on the distance scale for commencing the descent, for a given aircraft weight and speed and a given wind condition,

an aircraft weight and wind correction scale means, said correction scale means providing a correction factor to adjust the indicated distance for commencing a descent based upon the aircraft weight and prevailing wind conditions, and

means mutually securing said first and second members for relative aligned movement.

2. The calculator of claim 1, said correction scale means including means for determining a gross correction factor, and a correction scale display proportioning the gross correction factor in accordance with the actual aircraft altitude to be lost during the descent.

3. The calculator of claim 2, further comprising means having a second altitude scale displayed thereon, said second altitude scale being proportioned in terms of indicated air speed below a predetermined altitude, said first and second altitude scales being proportioned to correspond respectively to first and second aircraft speeds, said distance and second altitude scales being mutually alignable and proportioned so that, when a target distance on the distance scale is aligned with a target altitude on the second altitude scale, the actual altitude on the second altitude scale is aligned with a desired fuel efficient distance on the distance scale for commencing a descent to the target altitude and distance, for a given aircraft weight and speed and a given wind condition.

4. The calculator of claim 3, said second altitude scale being displayed on a third member which is mutually secured and alignable with said first member.

5. The calculator of claim 4, said correction scale being displayed on a fourth member which is mutually secured to said second and third members, said correction scale being alignable with either one of said first and second altitude scales.

6. The calculator of claim 1 or 2, said correction scale means including means for determining separate weight and wind correction factors, said separate correction factors being aggregable to a single correction factor.

7. A manually operable calculator for calculating a beginning of descent position to optimize aircraft fuel consumption during descent from an actual altitude and distance to a target altitude and distance, comprising:

a first member having a distance scale displayed thereon,

a plurality of additional members, each of said additional members being alignable with said first member, and having respective altitude scales displayed thereon extending over substantially equal altitude ranges, each of said altitude scales being proportioned in terms of indicated air speed below respective predetermined altitudes to correspond to respective predetermined aircraft speeds,

said distance and each of said altitude scales being respectively proportioned so that, when a target distance on the distance scale is aligned with a target altitude on a respective altitude scale, the actual altitude on said respective altitude scale is aligned with a desired fuel efficient distance on the distance scale for commencing the descent, and

means mutually securing said first and additional members for relative aligned movement.

8. The calculator of claim 7, wherein each of said altitude scales are proportioned to correspond to mach speed above respective predetermined transition altitudes, and to indicated air speed below said transition altitudes.

9. The calculator of claim 8, wherein said transition altitudes correspond substantially to the altitudes above which mach speed exceeds indicated air speed, and below which indicated air speed exceeds mach speed, for each respective altitude scale.

10. The calculator of claims 7, 8, or 9, wherein said distance scale is substantially linear.

11. The calculator of claim 7, wherein each of said altitude scales extend over approximately equal altitude ranges.

12. A manually operable calculator for calculating a beginning of descent position to optimize aircraft fuel consumption during descent from an actual altitude and distance to a target altitude and distance, comprising:

a first member having a distance scale displayed thereon,

display means having a plurality of altitude scales displayed thereon extending over substantially equal altitude ranges, each of said altitude scales being proportioned in terms of indicated air speed below respective predetermined altitudes to correspond to respective predetermined aircraft speeds and respectively alignable with said distance scale, each of said altitude scales extending over approximately equal altitude ranges,

said distance scale and each of said altitude scales being respectively proportioned so that, when a target distance on the distance scale is aligned with a target altitude on a respective altitude scale, the actual altitude on said respective altitude scale is aligned with a desired fuel efficient distance on the distance scale for commencing the descent, and

means mutually securing said first member and said display means for relative aligned movement.

13. The calculator of claim 12, said display means comprising a plurality of members, each of said members having a respective altitude scale displayed thereon, and secured for relative aligned movement with respect to said first member.

14. The calculator of claim 7 or 12, further comprising an aircraft weight and wind correction scale means, said correction scale means providing a correction factor to adjust the indicated distance for commencing a descent based upon the aircraft weight and prevailing wind conditions.