Engine test stand mounting apparatus and method

Patent metadata

Field	Value
Publication number	US-10260376-B2
Application number	US-201715611312-A
Country	US
Kind code	B2
Filing date	Jun 1, 2017
Priority date	Jun 1, 2017
Publication date	Apr 16, 2019
Grant date	Apr 16, 2019

Abstract

A compliant mounting adapter for mounting an engine to a test stand includes: a body having: a first mounting interface configured for being coupled to the test stand; a second mounting interface configured for being coupled to the engine, the second mounting interface spaced-away from the first mounting interface; and a spanning element interconnecting the first and second mounting interfaces. The body is sufficiently flexible so as to permit movement relative movement of the two mounting interfaces, in response to forces generated by engine operation, in at least two degrees of freedom, and has a predetermined stiffness in each of the at least two degrees of freedom, with the predetermined stiffness of each degree of freedom being substantially independent from the stiffness of the other degrees of freedom.

First claim

What is claimed is:

1. A compliant mounting adapter for mounting an engine to a test stand, comprising:
a body having:
a first mounting interface configured for being coupled to the test stand;
a second mounting interface configured for being coupled to the engine, the second mounting interface spaced-away from the first mounting interface;
a spanning element interconnecting the first and second mounting interfaces; and
wherein the body is sufficiently flexible so as to permit relative movement of the two mounting interfaces, in response to forces generated by engine operation, in at least two degrees of freedom, and has a predetermined stiffness in each of the at least two degrees of freedom, with the predetermined stiffness of each degree of freedom being substantially independent from the stiffness of the other degrees of freedom.

2. The adapter of claim 1 wherein the first and second interfaces and the spanning element are part of a monolithic whole.

3. The adapter of claim 1 wherein the body is in the form of a closed hollow shape having a perimeter wall.

4. The adapter of claim 1 wherein the perimeter wall has as least one portion with a tapered wall thickness.

5. The adapter of claim 1 wherein each of the first and second interfaces comprises a plate having fastener holes formed therein.

6. The adapter of claim 1 wherein the body has a predetermined stiffness in four degrees of freedom, the predetermined stiffness of each degree of freedom being substantially independent from the stiffness of the other degrees of freedom.

7. The adapter of claim 1 wherein the stiffness in each of the at least two degrees of freedom is substantially equal to a corresponding stiffness of a pre-selected aircraft structure.

8. An engine testing apparatus, comprising:
a test stand having a rigid vertical support column with a first end fixedly joined to a stationary foundation, and a second end having a rigid head frame fixedly joined thereto;
one or more rigid mounting components configured to mechanically couple an engine to the head frame; and
a compliant mounting adapter mechanically coupled to one of the rigid mounting components, the compliant mounting adapter having:
a body including:
a first mounting interface mechanically coupled to the test stand;
a second mounting interface spaced-away from the first mounting interface;
a spanning element interconnecting the first and second mounting interfaces; and
wherein the body is sufficiently flexible so as to permit relative movement of the two mounting interfaces, in response to forces generated by engine operation, in at least two degrees of freedom, and has a predetermined stiffness in each of the at least two degrees of freedom, with the predetermined stiffness of each degree of freedom being substantially independent from the stiffness of the other degrees of freedom.

9. The apparatus of claim 8 further comprising an engine mechanically coupled to the head frame through directly or indirectly through the compliant mounting adapter.

10. The apparatus of claim 8 wherein the stiffness of the compliant mounting adapter in every degree of freedom is one-fifth or less of a stiffness of the test stand and the mounting components.

11. The apparatus of claim 8 wherein the mounting component comprises a rigid test stand adapter.

12. The apparatus of claim 8 wherein the first and second interfaces and the spanning element are part of a monolithic whole.

13. The apparatus of claim 8 wherein the body is in the form of a closed hollow shape having a perimeter wall.

14. The apparatus of claim 13 wherein the perimeter wall has as least one portion with a tapered wall thickness.

15. The apparatus of claim 8 wherein each of the first and second interfaces comprises a plate having fastener holes formed therein.

16. The apparatus of claim 8 wherein the body has a predetermined stiffness in four degrees of freedom, the predetermined stiffness of each degree of freedom being independent from the stiffness of the other degrees of freedom.

17. A method of testing an engine, comprising:
mounting the engine to a rigid test stand through one or more rigid mounting components, wherein the engine is coupled to the test stand directly or indirectly through a compliant mounting adapter,
wherein the compliant mounting adapter is sufficiently flexible so as to permit relative movement of the interconnected components, in response to applied forces generated by operation of the engine, in at least two degrees of freedom, and has a predetermined stiffness in each of the at least two degrees of freedom, with the predetermined stiffness of each degree of freedom being substantially independent from the stiffness of the other degrees of freedom; and
operating the engine while it is mounted to the test stand.

18. The method of claim 17 wherein the rigid mounting components include a rigid test stand adapter, and the compliant mounting adapter is disposed between the test stand adapter and the engine.

19. The method of claim 17 wherein the stiffness of the compliant mounting adapter in every degree of freedom is one-fifth or less of a stiffness of the test stand and the mounting components.

20. The method of claim 17 wherein the compliant mounting adapter has a predetermined stiffness in four degrees of freedom, the predetermined stiffness of each degree of freedom being substantially independent from the stiffness of the other degrees of freedom.

Assignees

• Gen Electric

Inventors

• Schmidt Richard

Classifications

• G01H1/003

  of rotating machines (G01H1/10 takes precedence) · CPC title

• F01D25/285 Primary

  Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures · CPC title

• G01L5/133

  for measuring thrust of propulsive devices, e.g. of propellers (aeroplanes B64C; marine propulsion B63H; jet-engines F02K) · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title

• G01M15/04

  Testing internal-combustion engines · CPC title