IP Library Granted Patent US 10,288,399
Granted Patent B2
US 10,288,399 · App. 15/323,591 · Granted May 14, 2019

Blade geometry characterization tool

Inventors: Robert D. Higbie (Haslet, TX); Jose DeAnda (Dallas, TX); Sven Roy Lofstrom (Irving, TX)
Assignee: SIKORSKY AIRCRAFT CORPORATION
G01B3/004G01B3/02G01B3/20G01B5/02G01B5/24G01B11/24
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Quick Facts
Patent No.
US 10,288,399
App. No.
15/323,591
Granted
May 14, 2019
Kind
B2
Abstract

A tool is provided for characterizing a blade geometry. The tool includes a first component attachable to a blade root of a blade and a second component attachable to leading and trailing edges of the blade at a blade tip and at multiple stations defined along a span-wise dimension of the blade. The second component is configured for characterization of a chord length of the blade at the blade tip and at the multiple stations. The first and second components are respectively configured for cooperative optical characterization of a sweep and a twist angle of the blade at the blade tip and at the multiple stations.

Claims (22)

1. A tool for characterizing a blade geometry, the tool comprising:

a first component attachable to a blade root of a blade, the first component including an optical element; and

a second component attachable to leading and trailing edges of the blade at a blade tip and at multiple stations defined along a span-wise dimension of the blade,

the second component having a measuring device configured for characterization of a chord length of the blade at the blade tip and at the multiple stations, the second component further including a scale toward which the optical element is aimed, and

the first and second components being respectively configured for cooperative optical characterization of a sweep and a twist angle of the blade at the blade tip and at the multiple stations.

2. The tool according to claim 1 , wherein the optical element comprises at least one of a laser and a sight.

3. The tool according to claim 1 , wherein the optical element is aimed at the scale for sweep characterization at the blade tip and at the multiple stations.

4. The tool according to claim 1 , wherein the first component comprises a first planar surface defining a plane to establish a twist reference angle.

5. The tool according to claim 4 , wherein the plane is substantially parallel with a chord of the blade.

6. The tool according to claim 4 , wherein the second component comprises a second planar surface which is comparable with the first planar surface for twist angle characterization at the blade tip and at the multiple stations.

7. The tool according to claim 1 , wherein the measuring device comprises a gage indicator.

8. The tool according to claim 1 , wherein the second component comprises a plurality of locating features configured to constrain an orientation of the second component relative to the blade.

9. The tool according to claim 1 , wherein the second component comprises a first end and a second end, the measuring device disposed at the first end of the second component.

10. The tool according to claim 9 , wherein the second component is disposable on the blade such that the first end of the second component corresponds to the leading edge of the blade, and the second end of the second component corresponds to the trailing edge of the blade.

11. A method of characterizing a geometry of a blade, the method comprising:

attaching a first component to a blade root of the blade, the first component including an optical element;

attaching a second component to leading and trailing edges of the blade at a blade tip and at multiple stations defined along a span-wise dimension of the blade, the second component further having a measuring device and a scale;

operating the measuring device of the second component to characterize a chord length of the blade at the blade tip and at the multiple stations; and

cooperatively operating the first and second components to characterize a sweep and a twist angle of the blade at the blade tip and at the multiple stations, wherein the cooperative operating of the first and second components comprises aiming the optical element of the first component at the scale of the second component for sweep characterization at the blade tip and at the multiple stations.

12. The method according to claim 11 , wherein the cooperative operating of the first and second components comprises comparing first and second planar surfaces of the first and second components for twist angle characterization at the blade tip and at the multiple stations.

13. The method according to claim 11 , further comprising disposing a plurality of locating features on the second component to constrain an orientation of the second component relative to the blade.

14. The method according to claim 11 , wherein the second component comprises a first end and a second end, the measuring device disposed at the first end of the second component, and attaching the first end of the second component to the leading edge of the blade, and the second end of the second component to the trailing edge of the blade.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 3, 2017
From: HIGBIE, ROBERT D.; DEANDA, JOSE; LOFSTROM, SVEN ROY
To: SIKORSKY AIRCRAFT CORPORATION
Reel/Frame 040828/0619 →
Continuity (2)
Provisional Application 62019617 · Jul 1, 2014
Related Publication 20170138715A1 · May 18, 2017